mirror of
https://github.com/FlightControl-Master/MOOSE_MISSIONS.git
synced 2025-08-15 10:37:46 +00:00
MOOSE demonstration missions [skip ci]
This commit is contained in:
Applevangelist
Binary file not shown.
@@ -1,189 +0,0 @@
|
||||
-- View scripts
|
||||
-- Copyright (C) 2004, Eagle Dynamics.
|
||||
DisableCombatViews = false -- F5 & Ctrl-F5
|
||||
ExternalObjectsLockDistance = 10000.0
|
||||
ShowTargetInfo = false
|
||||
CameraTerrainRestriction = true
|
||||
hAngleRearDefault = 180
|
||||
vAngleRearDefault = -8.0
|
||||
vAngleRearMin = -90 -- -8.0
|
||||
vAngleRearMax = 90.0
|
||||
|
||||
dbg_shell = "weapons.shells.PKT_7_62_T" -- 23mm shell
|
||||
--dbg_shell = "weapons.shells.2A42_30_AP"
|
||||
--dbg_shell = "weapons.nurs.WGr21"
|
||||
--dbg_shell = "weapons.shells.2A64_152" -- 152mm shell
|
||||
dbg_shell_v0 = -1 -- Muzzle speed m/s (-1 - speed from shall database)
|
||||
dbg_shell_fire_rate = 120
|
||||
--reformatted per-unit data to be mod system friendly
|
||||
--this file is no longer should be edited for adding new flyable aircraft , DCS automatically check core database (i.e. where you define your aircraft in aircraft table just define ViewSettings and SnapViews tables)
|
||||
|
||||
function default_fighter_player(t)
|
||||
local res = {
|
||||
CameraViewAngleLimits = {20.000000,140.000000},
|
||||
CameraAngleRestriction = {false ,90.000000,0.500000},
|
||||
EyePoint = {0.05 ,0.000000 ,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.4500000},y ={-0.300000,0.100000},z = {-0.220000,0.220000},roll = 90.000000},
|
||||
Allow360rotation = false,
|
||||
CameraAngleLimits = {200,-80.000000,110.000000},
|
||||
ShoulderSize = 0.2, -- move body when azimuth value more then 90 degrees
|
||||
}
|
||||
if t then
|
||||
for i,o in pairs(t) do
|
||||
res[i] = o
|
||||
end
|
||||
end
|
||||
return res
|
||||
end
|
||||
|
||||
function fulcrum()
|
||||
return {
|
||||
Cockpit = {
|
||||
default_fighter_player({CockpitLocalPoint = {4.71,1.28,0.000000}})
|
||||
},
|
||||
Chase = {
|
||||
LocalPoint = {1.220000,3.750000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-15.080000,6.350000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
end
|
||||
|
||||
ViewSettings = {}
|
||||
ViewSettings["A-10A"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.600000},
|
||||
y = {-0.300000,0.100000},
|
||||
z = {-0.250000,0.250000},
|
||||
roll = 90.000000}}),
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {0.600000,3.682000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-27.000000,12.000000,0.000000},
|
||||
AnglesDefault = {0.000000,-12.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["A-10C"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.600000},
|
||||
y = {-0.300000,0.100000},
|
||||
z = {-0.250000,0.250000},
|
||||
roll = 90.000000}}),
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {0.600000,3.682000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-27.000000,12.000000,0.000000},
|
||||
AnglesDefault = {0.000000,-12.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["F-15C"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {6.210000,1.204000,0.000000}})-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {2.510000,3.604000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-13.790000,6.204000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Ka-50"] = {
|
||||
Cockpit = {
|
||||
[1] = {-- player slot 1
|
||||
CockpitLocalPoint = {3.188000,0.390000,0.000000},
|
||||
CameraViewAngleLimits = {20.000000,120.000000},
|
||||
CameraAngleRestriction = {false,60.000000,0.400000},
|
||||
CameraAngleLimits = {140.000000,-65.000000,90.000000},
|
||||
EyePoint = {0.090000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.020000,0.350000},y ={-0.150000,0.165000},z = {-0.170000,0.170000},roll = 90.000000},
|
||||
},
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.512000,2.790000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.812000,5.390000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["MiG-29A"] = fulcrum()
|
||||
ViewSettings["MiG-29G"] = fulcrum()
|
||||
ViewSettings["MiG-29S"] = fulcrum()
|
||||
|
||||
ViewSettings["Su-25"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {3.352000,0.506000,0.000000}}),-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.348000,2.906000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.648001,5.506000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-25T"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {3.406000,0.466000,0.000000}}),-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.294000,2.866000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.594000,5.466000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-25TM"] = {
|
||||
Cockpit = {
|
||||
[1] = {-- player slot 1
|
||||
CockpitLocalPoint = {4.000000,1.000000,0.000000},
|
||||
CameraViewAngleLimits = {20.000000,140.000000},
|
||||
CameraAngleRestriction = {true,90.000000,0.400000},
|
||||
CameraAngleLimits = {160.000000,-70.000000,90.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.200000,0.200000},y ={-0.200000,0.200000},z = {-0.200000,0.200000},roll = 60.000000},
|
||||
},
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {4.000000,2.000000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {4.000000,2.000000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-27"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {7.959000,1.419000,0.000000}})-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {4.259000,3.819000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-12.041000,6.419000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
|
||||
ViewSettings["Su-33"] = ViewSettings["Su-27"]
|
||||
File diff suppressed because it is too large
Load Diff
@@ -1,128 +0,0 @@
|
||||
-- View scripts
|
||||
-- Copyright (C) 2004, Eagle Dynamics.
|
||||
|
||||
CockpitMouse = true --false
|
||||
CockpitMouseSpeedSlow = 1.0
|
||||
CockpitMouseSpeedNormal = 10.0
|
||||
CockpitMouseSpeedFast = 20.0
|
||||
CockpitKeyboardAccelerationSlow = 5.0
|
||||
CockpitKeyboardAccelerationNormal = 30.0
|
||||
CockpitKeyboardAccelerationFast = 80.0
|
||||
CockpitKeyboardZoomAcceleration = 300.0
|
||||
DisableSnapViewsSaving = false
|
||||
UseDefaultSnapViews = true
|
||||
CockpitPanStepHor = 45.0
|
||||
CockpitPanStepVert = 30.0
|
||||
CockpitNyMove = true
|
||||
|
||||
CockpitHAngleAccelerateTimeMax = 0.15
|
||||
CockpitVAngleAccelerateTimeMax = 0.15
|
||||
CockpitZoomAccelerateTimeMax = 0.2
|
||||
|
||||
function NaturalHeadMoving(tang, roll, omz)
|
||||
local r = roll
|
||||
if r > 90.0 then
|
||||
r = 180.0 - r
|
||||
elseif roll < -90.0 then
|
||||
r = -180.0 - r
|
||||
end
|
||||
local hAngle = -0.25 * r
|
||||
local vAngle = math.min(math.max(0.0, 0.4 * tang + 45.0 * omz), 90.0)
|
||||
return hAngle, vAngle
|
||||
end
|
||||
|
||||
ExternalMouse = true
|
||||
ExternalMouseSpeedSlow = 1.0
|
||||
ExternalMouseSpeedNormal = 5.0
|
||||
ExternalMouseSpeedFast = 20.0
|
||||
ExternalViewAngleMin = 3.0
|
||||
ExternalViewAngleMax = 140.0
|
||||
ExternalViewAngleDefault = 60.0
|
||||
ExternalKeyboardZoomAcceleration = 30.0
|
||||
ExternalKeyboardZoomAccelerateTimeMax = 1.0
|
||||
ExplosionExpoTime = 4.0
|
||||
ExternalKeyboardAccelerationSlow = 1.0
|
||||
ExternalKeyboardAccelerationNormal = 10.0
|
||||
ExternalKeyboardAccelerationFast = 30.0
|
||||
ExternalHAngleAccelerateTimeMax = 3.0
|
||||
ExternalVAngleAccelerateTimeMax = 3.0
|
||||
ExternalDistAccelerateTimeMax = 3.0
|
||||
ExternalHAngleLocalAccelerateTimeMax = 3.0
|
||||
ExternalVAngleLocalAccelerateTimeMax = 3.0
|
||||
ExternalAngleNormalDiscreteStep = 15.0/ExternalKeyboardAccelerationNormal -- When 'S' is pressed only
|
||||
ChaseCameraNyMove = true
|
||||
FreeCameraAngleIncrement = 3.0
|
||||
FreeCameraDistanceIncrement = 200.0
|
||||
FreeCameraLeftRightIncrement = 2.0
|
||||
FreeCameraAltitudeIncrement = 2.0
|
||||
FreeCameraScalarSpeedAcceleration = 0.1
|
||||
xMinMap = -300000
|
||||
xMaxMap = 500000
|
||||
yMinMap = -400000
|
||||
yMaxMap = 200000
|
||||
dxMap = 150000
|
||||
dyMap = 100000
|
||||
|
||||
head_roll_shaking = true
|
||||
head_roll_shaking_max = 30.0
|
||||
head_roll_shaking_compensation_gain = 0.3
|
||||
|
||||
-- CameraJiggle() and CameraFloat() functions make camera position
|
||||
-- dependent on FPS so be careful in using the Shift-J command with tracks, please.
|
||||
-- uncomment to use custom jiggle functions
|
||||
--[[
|
||||
function CameraJiggle(t,rnd1,rnd2,rnd3)
|
||||
local rotX, rotY, rotZ
|
||||
rotX = 0.05 * rnd1 * math.sin(37.0 * (t - 0.0))
|
||||
rotY = 0.05 * rnd2 * math.sin(41.0 * (t - 1.0))
|
||||
rotZ = 0.05 * rnd3 * math.sin(53.0 * (t - 2.0))
|
||||
return rotX, rotY, rotZ
|
||||
end
|
||||
|
||||
function CameraFloat(t)
|
||||
local dX, dY, dZ
|
||||
dX = 0.61 * math.sin(0.7 * t) + 0.047 * math.sin(1.6 * t);
|
||||
dY = 0.43 * math.sin(0.6 * t) + 0.067 * math.sin(1.7 * t);
|
||||
dZ = 0.53 * math.sin(1.0 * t) + 0.083 * math.sin(1.9 * t);
|
||||
return dX, dY, dZ
|
||||
end
|
||||
--]]
|
||||
--Debug keys
|
||||
|
||||
DEBUG_TEXT = 1
|
||||
DEBUG_GEOMETRY = 2
|
||||
|
||||
debug_keys = {
|
||||
[DEBUG_TEXT] = 1,
|
||||
[DEBUG_GEOMETRY] = 1
|
||||
}
|
||||
|
||||
function onDebugCommand(command)
|
||||
if command == 10000 then
|
||||
if debug_keys[DEBUG_TEXT] ~= 0 or debug_keys[DEBUG_GEOMETRY] ~= 0 then
|
||||
debug_keys[DEBUG_GEOMETRY] = 0
|
||||
debug_keys[DEBUG_TEXT] = 0
|
||||
else
|
||||
debug_keys[DEBUG_GEOMETRY] = 1
|
||||
debug_keys[DEBUG_TEXT] = 1
|
||||
end
|
||||
elseif command == 10001 then
|
||||
if debug_keys[DEBUG_TEXT] ~= 0 then
|
||||
debug_keys[DEBUG_TEXT] = 0
|
||||
else
|
||||
debug_keys[DEBUG_TEXT] = 1
|
||||
end
|
||||
elseif command == 10002 then
|
||||
if debug_keys[DEBUG_GEOMETRY] ~= 0 then
|
||||
debug_keys[DEBUG_GEOMETRY] = 0
|
||||
else
|
||||
debug_keys[DEBUG_GEOMETRY] = 1
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
-- gain values for TrackIR , to unify responce on diffrent types of aircraft
|
||||
TrackIR_gain_x = -0.6
|
||||
TrackIR_gain_y = 0.3
|
||||
TrackIR_gain_z = -0.25
|
||||
TrackIR_gain_roll = -90
|
||||
@@ -1,880 +0,0 @@
|
||||
SAT_SYS_GLONASS = 0
|
||||
SAT_SYS_GPS = 1
|
||||
|
||||
almanac = {}
|
||||
--GPS
|
||||
almanac[0] = {}
|
||||
almanac[0]["System"] = SAT_SYS_GPS
|
||||
almanac[0]["Number"] = 1
|
||||
almanac[0]["Orbital"] = "F"
|
||||
almanac[0]["Eccentricity"] = 6.294000e-003
|
||||
almanac[0]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[0]["Orbital_Inclination"] = 9.885676e-001
|
||||
almanac[0]["Rate_of_Right_Ascen"] = -7.862702e-009
|
||||
almanac[0]["SQRT_A"] = 5.153700e+003
|
||||
almanac[0]["Right_Ascen_at_Week"] = 8.096750e-001
|
||||
almanac[0]["Argument_of_Perigee"] = -1.777773e+000
|
||||
almanac[0]["Mean_Anom"] = -5.315745e-001
|
||||
almanac[0]["week"] = 1390
|
||||
|
||||
almanac[1] = {}
|
||||
almanac[1]["System"] = SAT_SYS_GPS
|
||||
almanac[1]["Number"] = 2
|
||||
almanac[1]["Orbital"] = "C"
|
||||
almanac[1]["Eccentricity"] = 8.794000e-003
|
||||
almanac[1]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[1]["Orbital_Inclination"] = 9.487811e-001
|
||||
almanac[1]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[1]["SQRT_A"] = 5.153700e+003
|
||||
almanac[1]["Right_Ascen_at_Week"] = -1.329172e+000
|
||||
almanac[1]["Argument_of_Perigee"] = 2.138637e+000
|
||||
almanac[1]["Mean_Anom"] = 7.311702e-001
|
||||
almanac[1]["week"] = 1390
|
||||
|
||||
almanac[2] = {}
|
||||
almanac[2]["System"] = SAT_SYS_GPS
|
||||
almanac[2]["Number"] = 3
|
||||
almanac[2]["Orbital"] = "F"
|
||||
almanac[2]["Eccentricity"] = 8.424000e-003
|
||||
almanac[2]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[2]["Orbital_Inclination"] = 9.262804e-001
|
||||
almanac[2]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[2]["SQRT_A"] = 5.153600e+003
|
||||
almanac[2]["Right_Ascen_at_Week"] = -2.341514e+000
|
||||
almanac[2]["Argument_of_Perigee"] = 6.749357e-001
|
||||
almanac[2]["Mean_Anom"] = -2.296153e-001
|
||||
almanac[2]["week"] = 1389
|
||||
|
||||
almanac[3] = {}
|
||||
almanac[3]["System"] = SAT_SYS_GPS
|
||||
almanac[3]["Number"] = 4
|
||||
almanac[3]["Orbital"] = "D"
|
||||
almanac[3]["Eccentricity"] = 7.413000e-003
|
||||
almanac[3]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[3]["Orbital_Inclination"] = 9.482889e-001
|
||||
almanac[3]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[3]["SQRT_A"] = 5.153600e+003
|
||||
almanac[3]["Right_Ascen_at_Week"] = -1.309589e+000
|
||||
almanac[3]["Argument_of_Perigee"] = 1.623504e-001
|
||||
almanac[3]["Mean_Anom"] = -3.022943e+000
|
||||
almanac[3]["week"] = 1390
|
||||
|
||||
almanac[4] = {}
|
||||
almanac[4]["System"] = SAT_SYS_GPS
|
||||
almanac[4]["Number"] = 5
|
||||
almanac[4]["Orbital"] = "B"
|
||||
almanac[4]["Eccentricity"] = 7.432000e-003
|
||||
almanac[4]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[4]["Orbital_Inclination"] = 9.387437e-001
|
||||
almanac[4]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[4]["SQRT_A"] = 5.153700e+003
|
||||
almanac[4]["Right_Ascen_at_Week"] = 2.779487e+000
|
||||
almanac[4]["Argument_of_Perigee"] = 1.099033e+000
|
||||
almanac[4]["Mean_Anom"] = 2.970984e+000
|
||||
almanac[4]["week"] = 1390
|
||||
|
||||
almanac[5] = {}
|
||||
almanac[5]["System"] = SAT_SYS_GPS
|
||||
almanac[5]["Number"] = 6
|
||||
almanac[5]["Orbital"] = "C"
|
||||
almanac[5]["Eccentricity"] = 6.020000e-003
|
||||
almanac[5]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[5]["Orbital_Inclination"] = 9.337591e-001
|
||||
almanac[5]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[5]["SQRT_A"] = 5.153600e+003
|
||||
almanac[5]["Right_Ascen_at_Week"] = -2.407627e+000
|
||||
almanac[5]["Argument_of_Perigee"] = -1.788263e+000
|
||||
almanac[5]["Mean_Anom"] = -2.149877e+000
|
||||
almanac[5]["week"] = 1390
|
||||
|
||||
almanac[6] = {}
|
||||
almanac[6]["System"] = SAT_SYS_GPS
|
||||
almanac[6]["Number"] = 7
|
||||
almanac[6]["Orbital"] = "C"
|
||||
almanac[6]["Eccentricity"] = 1.052400e-002
|
||||
almanac[6]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[6]["Orbital_Inclination"] = 9.353229e-001
|
||||
almanac[6]["Rate_of_Right_Ascen"] = -8.080868e-009
|
||||
almanac[6]["SQRT_A"] = 5.153700e+003
|
||||
almanac[6]["Right_Ascen_at_Week"] = -2.433580e+000
|
||||
almanac[6]["Argument_of_Perigee"] = -1.767301e+000
|
||||
almanac[6]["Mean_Anom"] = -3.141503e+000
|
||||
almanac[6]["week"] = 1390
|
||||
|
||||
almanac[7] = {}
|
||||
almanac[7]["System"] = SAT_SYS_GPS
|
||||
almanac[7]["Number"] = 8
|
||||
almanac[7]["Orbital"] = "A"
|
||||
almanac[7]["Eccentricity"] = 9.822000e-003
|
||||
almanac[7]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[7]["Orbital_Inclination"] = 9.741390e-001
|
||||
almanac[7]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[7]["SQRT_A"] = 5.153600e+003
|
||||
almanac[7]["Right_Ascen_at_Week"] = 1.857849e+000
|
||||
almanac[7]["Argument_of_Perigee"] = 2.674034e+000
|
||||
almanac[7]["Mean_Anom"] = -2.009745e+000
|
||||
almanac[7]["week"] = 1390
|
||||
|
||||
almanac[8] = {}
|
||||
almanac[8]["System"] = SAT_SYS_GPS
|
||||
almanac[8]["Number"] = 9
|
||||
almanac[8]["Orbital"] = "A"
|
||||
almanac[8]["Eccentricity"] = 1.839300e-002
|
||||
almanac[8]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[8]["Orbital_Inclination"] = 9.617541e-001
|
||||
almanac[8]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[8]["SQRT_A"] = 5.153600e+003
|
||||
almanac[8]["Right_Ascen_at_Week"] = 1.777005e+000
|
||||
almanac[8]["Argument_of_Perigee"] = 1.274962e+000
|
||||
almanac[8]["Mean_Anom"] = -2.349578e+000
|
||||
almanac[8]["week"] = 1390
|
||||
|
||||
almanac[9] = {}
|
||||
almanac[9]["System"] = SAT_SYS_GPS
|
||||
almanac[9]["Number"] = 10
|
||||
almanac[9]["Orbital"] = "E"
|
||||
almanac[9]["Eccentricity"] = 7.061000e-003
|
||||
almanac[9]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[9]["Orbital_Inclination"] = 9.728876e-001
|
||||
almanac[9]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[9]["SQRT_A"] = 5.153600e+003
|
||||
almanac[9]["Right_Ascen_at_Week"] = -2.563014e-001
|
||||
almanac[9]["Argument_of_Perigee"] = 4.377980e-001
|
||||
almanac[9]["Mean_Anom"] = 1.210716e+000
|
||||
almanac[9]["week"] = 1390
|
||||
|
||||
almanac[10] = {}
|
||||
almanac[10]["System"] = SAT_SYS_GPS
|
||||
almanac[10]["Number"] = 11
|
||||
almanac[10]["Orbital"] = "D"
|
||||
almanac[10]["Eccentricity"] = 5.744000e-003
|
||||
almanac[10]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[10]["Orbital_Inclination"] = 8.959309e-001
|
||||
almanac[10]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[10]["SQRT_A"] = 5.153600e+003
|
||||
almanac[10]["Right_Ascen_at_Week"] = -1.478816e+000
|
||||
almanac[10]["Argument_of_Perigee"] = 3.750011e-001
|
||||
almanac[10]["Mean_Anom"] = -1.522048e+000
|
||||
almanac[10]["week"] = 1390
|
||||
|
||||
almanac[11] = {}
|
||||
almanac[11]["System"] = SAT_SYS_GPS
|
||||
almanac[11]["Number"] = 13
|
||||
almanac[11]["Orbital"] = "F"
|
||||
almanac[11]["Eccentricity"] = 3.088000e-003
|
||||
almanac[11]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[11]["Orbital_Inclination"] = 9.927564e-001
|
||||
almanac[11]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[11]["SQRT_A"] = 5.153700e+003
|
||||
almanac[11]["Right_Ascen_at_Week"] = 7.956600e-001
|
||||
almanac[11]["Argument_of_Perigee"] = 1.279395e+000
|
||||
almanac[11]["Mean_Anom"] = 1.004349e+000
|
||||
almanac[11]["week"] = 1390
|
||||
|
||||
almanac[12] = {}
|
||||
almanac[12]["System"] = SAT_SYS_GPS
|
||||
almanac[12]["Number"] = 14
|
||||
almanac[12]["Orbital"] = "F"
|
||||
almanac[12]["Eccentricity"] = 2.591000e-003
|
||||
almanac[12]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[12]["Orbital_Inclination"] = 9.868729e-001
|
||||
almanac[12]["Rate_of_Right_Ascen"] = -7.885391e-009
|
||||
almanac[12]["SQRT_A"] = 5.153600e+003
|
||||
almanac[12]["Right_Ascen_at_Week"] = 7.819592e-001
|
||||
almanac[12]["Argument_of_Perigee"] = -2.158621e+000
|
||||
almanac[12]["Mean_Anom"] = 5.412611e-001
|
||||
almanac[12]["week"] = 1390
|
||||
|
||||
almanac[13] = {}
|
||||
almanac[13]["System"] = SAT_SYS_GPS
|
||||
almanac[13]["Number"] = 15
|
||||
almanac[13]["Orbital"] = "D"
|
||||
almanac[13]["Eccentricity"] = 9.828000e-003
|
||||
almanac[13]["Time_of_Applicability"] = 3.194880e+005
|
||||
almanac[13]["Orbital_Inclination"] = 9.554204e-001
|
||||
almanac[13]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[13]["SQRT_A"] = 5.153600e+003
|
||||
almanac[13]["Right_Ascen_at_Week"] = -1.123869e+000
|
||||
almanac[13]["Argument_of_Perigee"] = 2.690266e+000
|
||||
almanac[13]["Mean_Anom"] = 2.220476e+000
|
||||
almanac[13]["week"] = 1389
|
||||
|
||||
almanac[14] = {}
|
||||
almanac[14]["System"] = SAT_SYS_GPS
|
||||
almanac[14]["Number"] = 16
|
||||
almanac[14]["Orbital"] = "B"
|
||||
almanac[14]["Eccentricity"] = 3.494000e-003
|
||||
almanac[14]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[14]["Orbital_Inclination"] = 9.629340e-001
|
||||
almanac[14]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[14]["SQRT_A"] = 5.153700e+003
|
||||
almanac[14]["Right_Ascen_at_Week"] = 2.873124e+000
|
||||
almanac[14]["Argument_of_Perigee"] = -7.819243e-001
|
||||
almanac[14]["Mean_Anom"] = 2.623629e+000
|
||||
almanac[14]["week"] = 1390
|
||||
|
||||
almanac[15] = {}
|
||||
almanac[15]["System"] = SAT_SYS_GPS
|
||||
almanac[15]["Number"] = 17
|
||||
almanac[15]["Orbital"] = "C"
|
||||
almanac[15]["Eccentricity"] = 2.141000e-003
|
||||
almanac[15]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[15]["Orbital_Inclination"] = 9.601170e-001
|
||||
almanac[15]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[15]["SQRT_A"] = 5.153700e+003
|
||||
almanac[15]["Right_Ascen_at_Week"] = -2.371499e+000
|
||||
almanac[15]["Argument_of_Perigee"] = 3.087694e+000
|
||||
almanac[15]["Mean_Anom"] = 1.611217e+000
|
||||
almanac[15]["week"] = 1390
|
||||
|
||||
almanac[16] = {}
|
||||
almanac[16]["System"] = SAT_SYS_GPS
|
||||
almanac[16]["Number"] = 18
|
||||
almanac[16]["Orbital"] = "E"
|
||||
almanac[16]["Eccentricity"] = 7.636000e-003
|
||||
almanac[16]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[16]["Orbital_Inclination"] = 9.569597e-001
|
||||
almanac[16]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[16]["SQRT_A"] = 5.153700e+003
|
||||
almanac[16]["Right_Ascen_at_Week"] = -2.359858e-001
|
||||
almanac[16]["Argument_of_Perigee"] = -2.649216e+000
|
||||
almanac[16]["Mean_Anom"] = 2.675029e+000
|
||||
almanac[16]["week"] = 1390
|
||||
|
||||
almanac[17] = {}
|
||||
almanac[17]["System"] = SAT_SYS_GPS
|
||||
almanac[17]["Number"] = 19
|
||||
almanac[17]["Orbital"] = "C"
|
||||
almanac[17]["Eccentricity"] = 3.602000e-003
|
||||
almanac[17]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[17]["Orbital_Inclination"] = 9.580209e-001
|
||||
almanac[17]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[17]["SQRT_A"] = 5.153600e+003
|
||||
almanac[17]["Right_Ascen_at_Week"] = -2.312385e+000
|
||||
almanac[17]["Argument_of_Perigee"] = -1.161079e+000
|
||||
almanac[17]["Mean_Anom"] = 1.310619e+000
|
||||
almanac[17]["week"] = 1390
|
||||
|
||||
almanac[18] = {}
|
||||
almanac[18]["System"] = SAT_SYS_GPS
|
||||
almanac[18]["Number"] = 20
|
||||
almanac[18]["Orbital"] = "E"
|
||||
almanac[18]["Eccentricity"] = 2.796000e-003
|
||||
almanac[18]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[18]["Orbital_Inclination"] = 9.564693e-001
|
||||
almanac[18]["Rate_of_Right_Ascen"] = -7.908080e-009
|
||||
almanac[18]["SQRT_A"] = 5.153600e+003
|
||||
almanac[18]["Right_Ascen_at_Week"] = -2.889565e-001
|
||||
almanac[18]["Argument_of_Perigee"] = 1.379612e+000
|
||||
almanac[18]["Mean_Anom"] = 2.461750e+000
|
||||
almanac[18]["week"] = 1390
|
||||
|
||||
almanac[19] = {}
|
||||
almanac[19]["System"] = SAT_SYS_GPS
|
||||
almanac[19]["Number"] = 21
|
||||
almanac[19]["Orbital"] = "D"
|
||||
almanac[19]["Eccentricity"] = 1.162900e-002
|
||||
almanac[19]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[19]["Orbital_Inclination"] = 9.418592e-001
|
||||
almanac[19]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[19]["SQRT_A"] = 5.153600e+003
|
||||
almanac[19]["Right_Ascen_at_Week"] = -1.289972e+000
|
||||
almanac[19]["Argument_of_Perigee"] = -2.923686e+000
|
||||
almanac[19]["Mean_Anom"] = -2.349194e+000
|
||||
almanac[19]["week"] = 1390
|
||||
|
||||
almanac[20] = {}
|
||||
almanac[20]["System"] = SAT_SYS_GPS
|
||||
almanac[20]["Number"] = 22
|
||||
almanac[20]["Orbital"] = "E"
|
||||
almanac[20]["Eccentricity"] = 4.893000e-003
|
||||
almanac[20]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[20]["Orbital_Inclination"] = 9.545093e-001
|
||||
almanac[20]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[20]["SQRT_A"] = 5.153600e+003
|
||||
almanac[20]["Right_Ascen_at_Week"] = -2.280969e-001
|
||||
almanac[20]["Argument_of_Perigee"] = -1.674502e+000
|
||||
almanac[20]["Mean_Anom"] = 1.106852e+000
|
||||
almanac[20]["week"] = 1390
|
||||
|
||||
almanac[21] = {}
|
||||
almanac[21]["System"] = SAT_SYS_GPS
|
||||
almanac[21]["Number"] = 23
|
||||
almanac[21]["Orbital"] = "F"
|
||||
almanac[21]["Eccentricity"] = 4.822000e-003
|
||||
almanac[21]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[21]["Orbital_Inclination"] = 9.691247e-001
|
||||
almanac[21]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[21]["SQRT_A"] = 5.153700e+003
|
||||
almanac[21]["Right_Ascen_at_Week"] = 7.667399e-001
|
||||
almanac[21]["Argument_of_Perigee"] = 2.497634e+000
|
||||
almanac[21]["Mean_Anom"] = 3.184700e-001
|
||||
almanac[21]["week"] = 1390
|
||||
|
||||
almanac[22] = {}
|
||||
almanac[22]["System"] = SAT_SYS_GPS
|
||||
almanac[22]["Number"] = 24
|
||||
almanac[22]["Orbital"] = "D"
|
||||
almanac[22]["Eccentricity"] = 9.277000e-003
|
||||
almanac[22]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[22]["Orbital_Inclination"] = 9.585183e-001
|
||||
almanac[22]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[22]["SQRT_A"] = 5.153900e+003
|
||||
almanac[22]["Right_Ascen_at_Week"] = -1.274840e+000
|
||||
almanac[22]["Argument_of_Perigee"] = -8.815651e-001
|
||||
almanac[22]["Mean_Anom"] = -1.695551e+000
|
||||
almanac[22]["week"] = 1390
|
||||
|
||||
almanac[23] = {}
|
||||
almanac[23]["System"] = SAT_SYS_GPS
|
||||
almanac[23]["Number"] = 25
|
||||
almanac[23]["Orbital"] = "A"
|
||||
almanac[23]["Eccentricity"] = 1.257400e-002
|
||||
almanac[23]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[23]["Orbital_Inclination"] = 9.551027e-001
|
||||
almanac[23]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[23]["SQRT_A"] = 5.153600e+003
|
||||
almanac[23]["Right_Ascen_at_Week"] = 1.721853e+000
|
||||
almanac[23]["Argument_of_Perigee"] = -1.329870e+000
|
||||
almanac[23]["Mean_Anom"] = -1.769623e+000
|
||||
almanac[23]["week"] = 1390
|
||||
|
||||
almanac[24] = {}
|
||||
almanac[24]["System"] = SAT_SYS_GPS
|
||||
almanac[24]["Number"] = 26
|
||||
almanac[24]["Orbital"] = "F"
|
||||
almanac[24]["Eccentricity"] = 1.745700e-002
|
||||
almanac[24]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[24]["Orbital_Inclination"] = 9.908749e-001
|
||||
almanac[24]["Rate_of_Right_Ascen"] = -7.840012e-009
|
||||
almanac[24]["SQRT_A"] = 5.153700e+003
|
||||
almanac[24]["Right_Ascen_at_Week"] = 7.961836e-001
|
||||
almanac[24]["Argument_of_Perigee"] = 8.161502e-001
|
||||
almanac[24]["Mean_Anom"] = -5.841961e-001
|
||||
almanac[24]["week"] = 1390
|
||||
|
||||
almanac[25] = {}
|
||||
almanac[25]["System"] = SAT_SYS_GPS
|
||||
almanac[25]["Number"] = 27
|
||||
almanac[25]["Orbital"] = "A"
|
||||
almanac[25]["Eccentricity"] = 1.991000e-002
|
||||
almanac[25]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[25]["Orbital_Inclination"] = 9.596563e-001
|
||||
almanac[25]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[25]["SQRT_A"] = 5.153600e+003
|
||||
almanac[25]["Right_Ascen_at_Week"] = 1.754124e+000
|
||||
almanac[25]["Argument_of_Perigee"] = -1.900854e+000
|
||||
almanac[25]["Mean_Anom"] = 3.046487e+000
|
||||
almanac[25]["week"] = 1390
|
||||
|
||||
almanac[26] = {}
|
||||
almanac[26]["System"] = SAT_SYS_GPS
|
||||
almanac[26]["Number"] = 28
|
||||
almanac[26]["Orbital"] = "B"
|
||||
almanac[26]["Eccentricity"] = 1.162800e-002
|
||||
almanac[26]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[26]["Orbital_Inclination"] = 9.610106e-001
|
||||
almanac[26]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[26]["SQRT_A"] = 5.153600e+003
|
||||
almanac[26]["Right_Ascen_at_Week"] = 2.882583e+000
|
||||
almanac[26]["Argument_of_Perigee"] = -2.242868e+000
|
||||
almanac[26]["Mean_Anom"] = 1.860642e+000
|
||||
almanac[26]["week"] = 1390
|
||||
|
||||
almanac[27] = {}
|
||||
almanac[27]["System"] = SAT_SYS_GPS
|
||||
almanac[27]["Number"] = 29
|
||||
almanac[27]["Orbital"] = "F"
|
||||
almanac[27]["Eccentricity"] = 9.462000e-003
|
||||
almanac[27]["Time_of_Applicability"] = 1.474560e+005
|
||||
almanac[27]["Orbital_Inclination"] = 9.874838e-001
|
||||
almanac[27]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[27]["SQRT_A"] = 5.153700e+003
|
||||
almanac[27]["Right_Ascen_at_Week"] = 7.647503e-001
|
||||
almanac[27]["Argument_of_Perigee"] = -8.614589e-001
|
||||
almanac[27]["Mean_Anom"] = -4.488983e-001
|
||||
almanac[27]["week"] = 1390
|
||||
|
||||
almanac[28] = {}
|
||||
almanac[28]["System"] = SAT_SYS_GPS
|
||||
almanac[28]["Number"] = 30
|
||||
almanac[28]["Orbital"] = "B"
|
||||
almanac[28]["Eccentricity"] = 9.296000e-003
|
||||
almanac[28]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[28]["Orbital_Inclination"] = 9.452992e-001
|
||||
almanac[28]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[28]["SQRT_A"] = 5.153600e+003
|
||||
almanac[28]["Right_Ascen_at_Week"] = 2.826698e+000
|
||||
almanac[28]["Argument_of_Perigee"] = 1.306413e+000
|
||||
almanac[28]["Mean_Anom"] = 2.148725e+000
|
||||
almanac[28]["week"] = 1390
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
--GLONASS
|
||||
--1 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 1-8
|
||||
almanac[29] = {}
|
||||
almanac[29]["System"] = SAT_SYS_GLONASS
|
||||
almanac[29]["Number"] = 1
|
||||
almanac[29]["Orbital"] = 1
|
||||
almanac[29]["GLONASS_Data"] = {}
|
||||
almanac[29]["GLONASS_Data"]["NKU_Number"] = 796
|
||||
almanac[29]["GLONASS_Data"]["Cosmos_Number"] = 2411
|
||||
almanac[29]["Eccentricity"] = 1.184000e-003
|
||||
almanac[29]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[29]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[29]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[29]["SQRT_A"] = 5.050500e+003
|
||||
almanac[29]["Right_Ascen_at_Week"] = 5.979807e+000
|
||||
almanac[29]["Argument_of_Perigee"] = 2.622634e+000
|
||||
almanac[29]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[29]["week"] = 1390
|
||||
almanac[29]["Commit_date"] = "06.02.2005"
|
||||
almanac[29]["Life_dates"] = {}
|
||||
|
||||
almanac[30] = {}
|
||||
almanac[30]["System"] = SAT_SYS_GLONASS
|
||||
almanac[30]["Number"] = 2
|
||||
almanac[30]["Orbital"] = 1
|
||||
almanac[30]["GLONASS_Data"] = {}
|
||||
almanac[30]["GLONASS_Data"]["NKU_Number"] = 794
|
||||
almanac[30]["GLONASS_Data"]["Cosmos_Number"] = 2401
|
||||
almanac[30]["Eccentricity"] = 4.486000e-003
|
||||
almanac[30]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[30]["Orbital_Inclination"] = 1.128459e+000
|
||||
almanac[30]["Rate_of_Right_Ascen"] = -6.759654e-009
|
||||
almanac[30]["SQRT_A"] = 5.050500e+003
|
||||
almanac[30]["Right_Ascen_at_Week"] = 5.997871e+000
|
||||
almanac[30]["Argument_of_Perigee"] = 1.709531e+000
|
||||
almanac[30]["Mean_Anom"] = -5.367633e+000
|
||||
almanac[30]["week"] = 1390
|
||||
almanac[30]["Commit_date"] = "02.02.2004"
|
||||
almanac[30]["Life_dates"] = {}
|
||||
|
||||
almanac[31] = {}
|
||||
almanac[31]["System"] = SAT_SYS_GLONASS
|
||||
almanac[31]["Number"] = 3
|
||||
almanac[31]["Orbital"] = 1
|
||||
almanac[31]["GLONASS_Data"] = {}
|
||||
almanac[31]["GLONASS_Data"]["NKU_Number"] = 789
|
||||
almanac[31]["GLONASS_Data"]["Cosmos_Number"] = 2381
|
||||
almanac[31]["Eccentricity"] = 2.459000e-003
|
||||
almanac[31]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[31]["Orbital_Inclination"] = 1.122958e+000
|
||||
almanac[31]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[31]["SQRT_A"] = 5.050500e+003
|
||||
almanac[31]["Right_Ascen_at_Week"] = 5.960713e+000
|
||||
almanac[31]["Argument_of_Perigee"] = -2.683407e+000
|
||||
almanac[31]["Mean_Anom"] = -1.791788e+000
|
||||
almanac[31]["week"] = 1390
|
||||
almanac[31]["Commit_date"] = "04.01.2002"
|
||||
almanac[31]["Life_dates"] = {}
|
||||
|
||||
almanac[32] = {}
|
||||
almanac[32]["System"] = SAT_SYS_GLONASS
|
||||
almanac[32]["Number"] = 4
|
||||
almanac[32]["Orbital"] = 1
|
||||
almanac[32]["GLONASS_Data"] = {}
|
||||
almanac[32]["GLONASS_Data"]["NKU_Number"] = 795
|
||||
almanac[29]["GLONASS_Data"]["Cosmos_Number"] = 2403
|
||||
almanac[32]["Eccentricity"] = 4.054000e-003
|
||||
almanac[32]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[32]["Orbital_Inclination"] = 1.128543e+000
|
||||
almanac[32]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[32]["SQRT_A"] = 5.050500e+003
|
||||
almanac[32]["Right_Ascen_at_Week"] = 5.998081e+000
|
||||
almanac[32]["Argument_of_Perigee"] = 1.497160e+000
|
||||
almanac[32]["Mean_Anom"] = -4.293681e-001
|
||||
almanac[32]["week"] = 1390
|
||||
almanac[32]["Commit_date"] = "29.01.2004"
|
||||
almanac[32]["Life_dates"] = {}
|
||||
|
||||
almanac[33] = {}
|
||||
almanac[33]["System"] = SAT_SYS_GLONASS
|
||||
almanac[33]["Number"] = 5
|
||||
almanac[33]["Orbital"] = 1
|
||||
almanac[33]["GLONASS_Data"] = {}
|
||||
almanac[33]["GLONASS_Data"]["NKU_Number"] = 711
|
||||
almanac[33]["GLONASS_Data"]["Cosmos_Number"] = 2382
|
||||
almanac[33]["Eccentricity"] = 7.040000e-004
|
||||
almanac[33]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[33]["Orbital_Inclination"] = 1.122886e+000
|
||||
almanac[33]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[33]["SQRT_A"] = 5.050600e+003
|
||||
almanac[33]["Right_Ascen_at_Week"] = 5.960713e+000
|
||||
almanac[33]["Argument_of_Perigee"] = 2.740933e+000
|
||||
almanac[33]["Mean_Anom"] = -2.523604e+000
|
||||
almanac[33]["week"] = 1390
|
||||
almanac[33]["Commit_date"] = "13.02.2003"
|
||||
almanac[33]["Life_dates"] = {}
|
||||
|
||||
almanac[34] = {}
|
||||
almanac[34]["System"] = SAT_SYS_GLONASS
|
||||
almanac[34]["Number"] = 6
|
||||
almanac[34]["Orbital"] = 1
|
||||
almanac[34]["GLONASS_Data"] = {}
|
||||
almanac[34]["GLONASS_Data"]["NKU_Number"] = 701
|
||||
almanac[34]["GLONASS_Data"]["Cosmos_Number"] = 2404
|
||||
almanac[34]["Eccentricity"] = 4.766000e-003
|
||||
almanac[34]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[34]["Orbital_Inclination"] = 1.128276e+000
|
||||
almanac[34]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[34]["SQRT_A"] = 5.050500e+003
|
||||
almanac[34]["Right_Ascen_at_Week"] = 5.997906e+000
|
||||
almanac[34]["Argument_of_Perigee"] = 1.802417e+000
|
||||
almanac[34]["Mean_Anom"] = -2.426512e+000
|
||||
almanac[34]["week"] = 1390
|
||||
almanac[34]["Commit_date"] = "08.12.2004"
|
||||
almanac[34]["Life_dates"] = {}
|
||||
|
||||
almanac[35] = {}
|
||||
almanac[35]["System"] = SAT_SYS_GLONASS
|
||||
almanac[35]["Number"] = 7
|
||||
almanac[35]["Orbital"] = 1
|
||||
almanac[35]["GLONASS_Data"] = {}
|
||||
almanac[35]["GLONASS_Data"]["NKU_Number"] = 712
|
||||
almanac[35]["GLONASS_Data"]["Cosmos_Number"] = 2413
|
||||
almanac[35]["Eccentricity"] = 7.570000e-004
|
||||
almanac[35]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[35]["Orbital_Inclination"] = 1.126344e+000
|
||||
almanac[35]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[35]["SQRT_A"] = 5.050500e+003
|
||||
almanac[35]["Right_Ascen_at_Week"] = 5.979388e+000
|
||||
almanac[35]["Argument_of_Perigee"] = 2.566068e+000
|
||||
almanac[35]["Mean_Anom"] = -3.921228e+000
|
||||
almanac[35]["week"] = 1390
|
||||
almanac[35]["Commit_date"] = "07.10.2005"
|
||||
almanac[35]["Life_dates"] = {}
|
||||
|
||||
almanac[36] = {}
|
||||
almanac[36]["System"] = SAT_SYS_GLONASS
|
||||
almanac[36]["GLONASS_Data"] = {}
|
||||
almanac[36]["Number"] = 8
|
||||
almanac[36]["Orbital"] = 1
|
||||
almanac[36]["GLONASS_Data"] = {}
|
||||
almanac[36]["GLONASS_Data"]["NKU_Number"] = 797
|
||||
almanac[36]["GLONASS_Data"]["Cosmos_Number"] = 2412
|
||||
almanac[36]["Eccentricity"] = 4.060000e-004
|
||||
almanac[36]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[36]["Orbital_Inclination"] = 1.126564e+000
|
||||
almanac[36]["Rate_of_Right_Ascen"] = -6.785834e-009
|
||||
almanac[36]["SQRT_A"] = 5.050600e+003
|
||||
almanac[36]["Right_Ascen_at_Week"] = 5.980069e+000
|
||||
almanac[36]["Argument_of_Perigee"] = 2.673633e+000
|
||||
almanac[36]["Mean_Anom"] = -4.812026e+000
|
||||
almanac[36]["week"] = 1390
|
||||
almanac[36]["Commit_date"] = "06.02.2005"
|
||||
almanac[36]["Life_dates"] = {}
|
||||
|
||||
--3 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 17-24
|
||||
almanac[37] = {}
|
||||
almanac[37]["System"] = SAT_SYS_GLONASS
|
||||
almanac[37]["Number"] = 17
|
||||
almanac[37]["Orbital"] = 3
|
||||
almanac[37]["GLONASS_Data"] = {}
|
||||
almanac[37]["GLONASS_Data"]["NKU_Number"] = 787
|
||||
almanac[37]["GLONASS_Data"]["Cosmos_Number"] = 2375
|
||||
almanac[37]["Eccentricity"] = 5.670000e-004
|
||||
almanac[37]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[37]["Orbital_Inclination"] = 1.126524e+000
|
||||
almanac[37]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[37]["SQRT_A"] = 5.050500e+003
|
||||
almanac[37]["Right_Ascen_at_Week"] = 3.895554e+000
|
||||
almanac[37]["Argument_of_Perigee"] = 6.085085e-001
|
||||
almanac[37]["Mean_Anom"] = -2.977407e+000
|
||||
almanac[37]["week"] = 1390
|
||||
almanac[37]["Commit_date"] = "04.11.2000"
|
||||
almanac[37]["Life_dates"] = {}
|
||||
|
||||
|
||||
almanac[38] = {}
|
||||
almanac[38]["System"] = SAT_SYS_GLONASS
|
||||
almanac[38]["Number"] = 18
|
||||
almanac[38]["Orbital"] = 3
|
||||
almanac[38]["GLONASS_Data"] = {}
|
||||
almanac[38]["GLONASS_Data"]["NKU_Number"] = 783
|
||||
almanac[38]["GLONASS_Data"]["Cosmos_Number"] = 2374
|
||||
almanac[38]["Eccentricity"] = 4.520000e-003
|
||||
almanac[38]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[38]["Orbital_Inclination"] = 1.126239e+000
|
||||
almanac[38]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[38]["SQRT_A"] = 5.050600e+003
|
||||
almanac[38]["Right_Ascen_at_Week"] = 3.894071e+000
|
||||
almanac[38]["Argument_of_Perigee"] = -2.509589e+000
|
||||
almanac[38]["Mean_Anom"] = -1.020057e+000
|
||||
almanac[38]["week"] = 1390
|
||||
almanac[38]["Commit_date"] = "05.01.2001"
|
||||
almanac[38]["Life_dates"] = {}
|
||||
|
||||
almanac[39] = {}
|
||||
almanac[39]["System"] = SAT_SYS_GLONASS
|
||||
almanac[39]["Number"] = 19
|
||||
almanac[39]["Orbital"] = 3
|
||||
almanac[39]["GLONASS_Data"] = {}
|
||||
almanac[39]["GLONASS_Data"]["NKU_Number"] = 798
|
||||
almanac[39]["GLONASS_Data"]["Cosmos_Number"] = 2417
|
||||
almanac[39]["Eccentricity"] = 2.023000e-003
|
||||
almanac[39]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[39]["Orbital_Inclination"] = 1.132205e+000
|
||||
almanac[39]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[39]["SQRT_A"] = 5.050500e+003
|
||||
almanac[39]["Right_Ascen_at_Week"] = 3.884018e+000
|
||||
almanac[39]["Argument_of_Perigee"] = 2.718313e+000
|
||||
almanac[39]["Mean_Anom"] = -3.933620e-001
|
||||
almanac[39]["week"] = 1390
|
||||
almanac[39]["Commit_date"] = "22.01.2006"
|
||||
almanac[39]["Life_dates"] = {}
|
||||
|
||||
almanac[40] = {}
|
||||
almanac[40]["System"] = SAT_SYS_GLONASS
|
||||
almanac[40]["Number"] = 20
|
||||
almanac[40]["Orbital"] = 3
|
||||
almanac[40]["GLONASS_Data"] = {}
|
||||
almanac[40]["GLONASS_Data"]["NKU_Number"] = 793
|
||||
almanac[40]["GLONASS_Data"]["Cosmos_Number"] = 2396
|
||||
almanac[40]["Eccentricity"] = 1.822000e-003
|
||||
almanac[40]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[40]["Orbital_Inclination"] = 1.129789e+000
|
||||
almanac[40]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[40]["SQRT_A"] = 5.050500e+003
|
||||
almanac[40]["Right_Ascen_at_Week"] = 3.896863e+000
|
||||
almanac[40]["Argument_of_Perigee"] = 2.723776e+000
|
||||
almanac[40]["Mean_Anom"] = -1.193647e+000
|
||||
almanac[40]["week"] = 1390
|
||||
almanac[40]["Commit_date"] = "31.01.2003"
|
||||
almanac[40]["Life_dates"] = {}
|
||||
|
||||
almanac[41] = {}
|
||||
almanac[41]["System"] = SAT_SYS_GLONASS
|
||||
almanac[41]["Number"] = 21
|
||||
almanac[41]["Orbital"] = 3
|
||||
almanac[41]["GLONASS_Data"] = {}
|
||||
almanac[41]["GLONASS_Data"]["NKU_Number"] = 792
|
||||
almanac[41]["GLONASS_Data"]["Cosmos_Number"] = 2395
|
||||
almanac[41]["Eccentricity"] = 5.290000e-004
|
||||
almanac[41]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[41]["Orbital_Inclination"] = 1.129957e+000
|
||||
almanac[41]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[41]["SQRT_A"] = 5.050500e+003
|
||||
almanac[41]["Right_Ascen_at_Week"] = 3.897806e+000
|
||||
almanac[41]["Argument_of_Perigee"] = -9.519367e-001
|
||||
almanac[41]["Mean_Anom"] = -4.578920e+000
|
||||
almanac[41]["week"] = 1390
|
||||
almanac[41]["Commit_date"] = "31.01.2003"
|
||||
almanac[41]["Life_dates"] = {}
|
||||
|
||||
almanac[42] = {}
|
||||
almanac[42]["System"] = SAT_SYS_GLONASS
|
||||
almanac[42]["Number"] = 22
|
||||
almanac[42]["Orbital"] = 3
|
||||
almanac[42]["GLONASS_Data"] = {}
|
||||
almanac[42]["GLONASS_Data"]["NKU_Number"] = 791
|
||||
almanac[42]["GLONASS_Data"]["Cosmos_Number"] = 2394
|
||||
almanac[42]["Eccentricity"] = 9.200000e-005
|
||||
almanac[42]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[42]["Orbital_Inclination"] = 1.129742e+000
|
||||
almanac[42]["Rate_of_Right_Ascen"] = -6.740456e-009
|
||||
almanac[42]["SQRT_A"] = 5.050500e+003
|
||||
almanac[42]["Right_Ascen_at_Week"] = 3.897404e+000
|
||||
almanac[42]["Argument_of_Perigee"] = 2.518211e+000
|
||||
almanac[42]["Mean_Anom"] = -2.530167e+000
|
||||
almanac[42]["week"] = 1390
|
||||
almanac[42]["Commit_date"] = "21.01.2003"
|
||||
almanac[42]["Life_dates"] = {}
|
||||
|
||||
almanac[43] = {}
|
||||
almanac[43]["System"] = SAT_SYS_GLONASS
|
||||
almanac[43]["Number"] = 23
|
||||
almanac[43]["Orbital"] = 3
|
||||
almanac[43]["GLONASS_Data"] = {}
|
||||
almanac[43]["GLONASS_Data"]["NKU_Number"] = 714
|
||||
almanac[43]["GLONASS_Data"]["Cosmos_Number"] = 2419
|
||||
almanac[43]["Eccentricity"] = 8.730000e-004
|
||||
almanac[43]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[43]["Orbital_Inclination"] = 1.132105e+000
|
||||
almanac[43]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[43]["SQRT_A"] = 5.050500e+003
|
||||
almanac[43]["Right_Ascen_at_Week"] = 3.883808e+000
|
||||
almanac[43]["Argument_of_Perigee"] = -3.039139e-001
|
||||
almanac[43]["Mean_Anom"] = -5.228304e-001
|
||||
almanac[43]["week"] = 1390
|
||||
almanac[43]["Commit_date"] = "31.08.2006"
|
||||
almanac[43]["Life_dates"] = {}
|
||||
|
||||
almanac[44] = {}
|
||||
almanac[44]["System"] = SAT_SYS_GLONASS
|
||||
almanac[44]["Number"] = 24
|
||||
almanac[44]["Orbital"] = 3
|
||||
almanac[44]["GLONASS_Data"] = {}
|
||||
almanac[44]["GLONASS_Data"]["NKU_Number"] = 713
|
||||
almanac[44]["GLONASS_Data"]["Cosmos_Number"] = 2418
|
||||
almanac[44]["Eccentricity"] = 2.044000e-003
|
||||
almanac[44]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[44]["Orbital_Inclination"] = 1.132430e+000
|
||||
almanac[44]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[44]["SQRT_A"] = 5.050500e+003
|
||||
almanac[44]["Right_Ascen_at_Week"] = 3.883983e+000
|
||||
almanac[44]["Argument_of_Perigee"] = -3.722784e-001
|
||||
almanac[44]["Mean_Anom"] = -1.240457e+000
|
||||
almanac[44]["week"] = 1390
|
||||
almanac[44]["Commit_date"] = "31.08.2006"
|
||||
almanac[44]["Life_dates"] = {}
|
||||
|
||||
--2 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 9-16
|
||||
almanac[45] = {}
|
||||
almanac[45]["System"] = SAT_SYS_GLONASS
|
||||
almanac[45]["Number"] = 9
|
||||
almanac[45]["Orbital"] = 2
|
||||
almanac[45]["GLONASS_Data"] = {}
|
||||
almanac[45]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[45]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[45]["Eccentricity"] = 1.184000e-003
|
||||
almanac[45]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[45]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[45]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[45]["SQRT_A"] = 5.050500e+003
|
||||
almanac[45]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[45]["Argument_of_Perigee"] = 2.88430067
|
||||
almanac[45]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[45]["week"] = 1390
|
||||
almanac[45]["Commit_date"] = "N/A"
|
||||
almanac[45]["Life_dates"] = {}
|
||||
|
||||
almanac[46] = {}
|
||||
almanac[46]["System"] = SAT_SYS_GLONASS
|
||||
almanac[46]["Number"] = 10
|
||||
almanac[46]["Orbital"] = 2
|
||||
almanac[46]["GLONASS_Data"] = {}
|
||||
almanac[46]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[46]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[46]["Eccentricity"] = 1.184000e-003
|
||||
almanac[46]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[46]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[46]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[46]["SQRT_A"] = 5.050500e+003
|
||||
almanac[46]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[46]["Argument_of_Perigee"] = 3.66930067
|
||||
almanac[46]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[46]["week"] = 1390
|
||||
almanac[46]["Commit_date"] = "N/A"
|
||||
almanac[46]["Life_dates"] = {}
|
||||
|
||||
almanac[47] = {}
|
||||
almanac[47]["System"] = SAT_SYS_GLONASS
|
||||
almanac[47]["Number"] = 11
|
||||
almanac[47]["Orbital"] = 2
|
||||
almanac[47]["GLONASS_Data"] = {}
|
||||
almanac[47]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[47]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[47]["Eccentricity"] = 1.184000e-003
|
||||
almanac[47]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[47]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[47]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[47]["SQRT_A"] = 5.050500e+003
|
||||
almanac[47]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[47]["Argument_of_Perigee"] = 4.45430067
|
||||
almanac[47]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[47]["week"] = 1390
|
||||
almanac[47]["Commit_date"] = "N/A"
|
||||
almanac[47]["Life_dates"] = {}
|
||||
|
||||
almanac[48] = {}
|
||||
almanac[48]["System"] = SAT_SYS_GLONASS
|
||||
almanac[48]["Number"] = 12
|
||||
almanac[48]["Orbital"] = 2
|
||||
almanac[48]["GLONASS_Data"] = {}
|
||||
almanac[48]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[48]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[48]["Eccentricity"] = 1.184000e-003
|
||||
almanac[48]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[48]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[48]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[48]["SQRT_A"] = 5.050500e+003
|
||||
almanac[48]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[48]["Argument_of_Perigee"] = 5.23930067
|
||||
almanac[48]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[48]["week"] = 1390
|
||||
almanac[48]["Commit_date"] = "N/A"
|
||||
almanac[48]["Life_dates"] = {}
|
||||
|
||||
almanac[49] = {}
|
||||
almanac[49]["System"] = SAT_SYS_GLONASS
|
||||
almanac[49]["Number"] = 13
|
||||
almanac[49]["Orbital"] = 2
|
||||
almanac[49]["GLONASS_Data"] = {}
|
||||
almanac[49]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[49]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[49]["Eccentricity"] = 1.184000e-003
|
||||
almanac[49]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[49]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[49]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[49]["SQRT_A"] = 5.050500e+003
|
||||
almanac[49]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[49]["Argument_of_Perigee"] = 6.02430067
|
||||
almanac[49]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[49]["week"] = 1390
|
||||
almanac[49]["Commit_date"] = "N/A"
|
||||
almanac[49]["Life_dates"] = {}
|
||||
|
||||
almanac[50] = {}
|
||||
almanac[50]["System"] = SAT_SYS_GLONASS
|
||||
almanac[50]["Number"] = 14
|
||||
almanac[50]["Orbital"] = 2
|
||||
almanac[50]["GLONASS_Data"] = {}
|
||||
almanac[50]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[50]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[50]["Eccentricity"] = 1.184000e-003
|
||||
almanac[50]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[50]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[50]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[50]["SQRT_A"] = 5.050500e+003
|
||||
almanac[50]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[50]["Argument_of_Perigee"] = 0.52930067
|
||||
almanac[50]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[50]["week"] = 1390
|
||||
almanac[50]["Commit_date"] = "N/A"
|
||||
almanac[50]["Life_dates"] = {}
|
||||
|
||||
almanac[51] = {}
|
||||
almanac[51]["System"] = SAT_SYS_GLONASS
|
||||
almanac[51]["Number"] = 15
|
||||
almanac[51]["Orbital"] = 2
|
||||
almanac[51]["GLONASS_Data"] = {}
|
||||
almanac[51]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[51]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[51]["Eccentricity"] = 1.184000e-003
|
||||
almanac[51]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[51]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[51]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[51]["SQRT_A"] = 5.050500e+003
|
||||
almanac[51]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[51]["Argument_of_Perigee"] = 1.31430067
|
||||
almanac[51]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[51]["week"] = 1390
|
||||
almanac[51]["Commit_date"] = "N/A"
|
||||
almanac[51]["Life_dates"] = {}
|
||||
|
||||
almanac[52] = {}
|
||||
almanac[52]["System"] = SAT_SYS_GLONASS
|
||||
almanac[52]["Number"] = 16
|
||||
almanac[52]["Orbital"] = 2
|
||||
almanac[52]["GLONASS_Data"] = {}
|
||||
almanac[52]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[52]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[52]["Eccentricity"] = 1.184000e-003
|
||||
almanac[52]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[52]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[52]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[52]["SQRT_A"] = 5.050500e+003
|
||||
almanac[52]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[52]["Argument_of_Perigee"] = 2.09930067
|
||||
almanac[52]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[52]["week"] = 1390
|
||||
almanac[52]["Commit_date"] = "N/A"
|
||||
almanac[52]["Life_dates"] = {}
|
||||
|
||||
SA_mode = false
|
||||
AS_mode = false
|
||||
@@ -1,27 +0,0 @@
|
||||
birds_avail = true --Birds availability. false - there is no birds
|
||||
birds_maximum_hrad = 200 --Maximum altitude above ground al sea level bird could be met
|
||||
birds_maximum_absolute_height = 8000 --Maximum absolute altitude bird could be met
|
||||
birds_minimum_velocity = 40 --Minimum velocity bird could be met
|
||||
birds_delta_time = 3.55
|
||||
birds_probability = {0.006333333*150,
|
||||
0.004166667*150,
|
||||
0.001966667*150,
|
||||
0.001090909*150,
|
||||
0.000741818*150,
|
||||
0.0006*150,
|
||||
0.000510545*150,
|
||||
0.000447273*150,
|
||||
0.000389455*150,
|
||||
0.000349091*150,
|
||||
0.000310909*150,
|
||||
0.000282545*150,
|
||||
0.000250909*150,
|
||||
0.000220364*150,
|
||||
0.000196364*150,
|
||||
0.000174545*150,
|
||||
0.000152727*150,
|
||||
0.000128727*150,
|
||||
0.000103636*150,
|
||||
7.63636E-05*150,
|
||||
0*150
|
||||
}
|
||||
@@ -1,150 +0,0 @@
|
||||
----------------------------------------------------------------------------------------
|
||||
---
|
||||
-- Name: BOS-100 - Stennis Hornet and Tomcat
|
||||
-- Author: funkyfranky
|
||||
-- Date Created: 17 August 2019
|
||||
--
|
||||
-- # Situation:
|
||||
--
|
||||
-- Practice Case I/II/III recovery using the F/A-18C Hornet or F-14B Tomcat.
|
||||
--
|
||||
-- See mission briefing for further details.
|
||||
--
|
||||
-- *** IMPORTANT ***
|
||||
-- If you run the mission in single player, hit ESC twice before entering a slot!
|
||||
-- Otherwise the script will not load due to a long standing DCS bug.
|
||||
--
|
||||
----------------------------------------------------------------------------------------
|
||||
|
||||
-- No MOOSE settings menu. Comment out this line if required.
|
||||
_SETTINGS:SetPlayerMenuOff()
|
||||
|
||||
-- S-3B Recovery Tanker spawning in air.
|
||||
local tanker=RECOVERYTANKER:New("USS Stennis", "Texaco Group")
|
||||
tanker:SetTakeoffAir()
|
||||
tanker:SetRadio(250)
|
||||
tanker:SetModex(511)
|
||||
tanker:SetTACAN(1, "TKR")
|
||||
tanker:__Start(1)
|
||||
|
||||
-- E-2D AWACS spawning on Stennis.
|
||||
local awacs=RECOVERYTANKER:New("USS Stennis", "E-2D Wizard Group")
|
||||
awacs:SetAWACS()
|
||||
awacs:SetRadio(260)
|
||||
awacs:SetAltitude(20000)
|
||||
awacs:SetCallsign(CALLSIGN.AWACS.Wizard)
|
||||
awacs:SetRacetrackDistances(30, 15)
|
||||
awacs:SetModex(611)
|
||||
awacs:SetTACAN(2, "WIZ")
|
||||
awacs:__Start(1)
|
||||
|
||||
-- Rescue Helo with home base Lake Erie. Has to be a global object!
|
||||
rescuehelo=RESCUEHELO:New("USS Stennis", "Rescue Helo")
|
||||
rescuehelo:SetHomeBase(AIRBASE:FindByName("Lake Erie"))
|
||||
rescuehelo:SetModex(42)
|
||||
rescuehelo:__Start(1)
|
||||
|
||||
-- Create AIRBOSS object.
|
||||
local AirbossStennis=AIRBOSS:New("USS Stennis")
|
||||
|
||||
-- Add recovery windows:
|
||||
-- Case I from 9 to 10 am.
|
||||
local window1=AirbossStennis:AddRecoveryWindow( "9:00", "10:00", 1, nil, true, 25)
|
||||
-- Case II with +15 degrees holding offset from 15:00 for 60 min.
|
||||
local window2=AirbossStennis:AddRecoveryWindow("15:00", "16:00", 2, 15, true, 23)
|
||||
-- Case III with +30 degrees holding offset from 2100 to 2200.
|
||||
local window3=AirbossStennis:AddRecoveryWindow("21:00", "22:00", 3, 30, true, 21)
|
||||
|
||||
-- Set folder of airboss sound files within miz file.
|
||||
AirbossStennis:SetSoundfilesFolder("Airboss Soundfiles/")
|
||||
|
||||
-- Single carrier menu optimization.
|
||||
AirbossStennis:SetMenuSingleCarrier()
|
||||
|
||||
-- Skipper menu.
|
||||
AirbossStennis:SetMenuRecovery(30, 20, false)
|
||||
|
||||
-- Remove landed AI planes from flight deck.
|
||||
AirbossStennis:SetDespawnOnEngineShutdown()
|
||||
|
||||
-- Load all saved player grades from your "Saved Games\DCS" folder (if lfs was desanitized).
|
||||
AirbossStennis:Load()
|
||||
|
||||
-- Automatically save player results to your "Saved Games\DCS" folder each time a player get a final grade from the LSO.
|
||||
AirbossStennis:SetAutoSave()
|
||||
|
||||
-- Enable trap sheet.
|
||||
AirbossStennis:SetTrapSheet()
|
||||
|
||||
-- Start airboss class.
|
||||
AirbossStennis:Start()
|
||||
|
||||
|
||||
--- Function called when recovery tanker is started.
|
||||
function tanker:OnAfterStart(From,Event,To)
|
||||
|
||||
-- Set recovery tanker.
|
||||
AirbossStennis:SetRecoveryTanker(tanker)
|
||||
|
||||
|
||||
-- Use tanker as radio relay unit for LSO transmissions.
|
||||
AirbossStennis:SetRadioRelayLSO(self:GetUnitName())
|
||||
|
||||
end
|
||||
|
||||
--- Function called when AWACS is started.
|
||||
function awacs:OnAfterStart(From,Event,To)
|
||||
-- Set AWACS.
|
||||
AirbossStennis:SetRecoveryTanker(tanker)
|
||||
end
|
||||
|
||||
|
||||
--- Function called when rescue helo is started.
|
||||
function rescuehelo:OnAfterStart(From,Event,To)
|
||||
-- Use rescue helo as radio relay for Marshal.
|
||||
AirbossStennis:SetRadioRelayMarshal(self:GetUnitName())
|
||||
end
|
||||
|
||||
--- Function called when a player gets graded by the LSO.
|
||||
function AirbossStennis:OnAfterLSOGrade(From, Event, To, playerData, grade)
|
||||
local PlayerData=playerData --Ops.Airboss#AIRBOSS.PlayerData
|
||||
local Grade=grade --Ops.Airboss#AIRBOSS.LSOgrade
|
||||
|
||||
----------------------------------------
|
||||
--- Interface your Discord bot here! ---
|
||||
----------------------------------------
|
||||
|
||||
local score=tonumber(Grade.points)
|
||||
local name=tostring(PlayerData.name)
|
||||
|
||||
-- Report LSO grade to dcs.log file.
|
||||
env.info(string.format("Player %s scored %.1f", name, score))
|
||||
end
|
||||
|
||||
|
||||
---------------------------
|
||||
--- Generate AI Traffic ---
|
||||
---------------------------
|
||||
|
||||
-- Spawn some AI flights as additional traffic.
|
||||
local F181=SPAWN:New("FA-18C Group 1"):InitModex(111) -- Coming in from NW after ~ 6 min
|
||||
local F182=SPAWN:New("FA-18C Group 2"):InitModex(112) -- Coming in from NW after ~20 min
|
||||
local F183=SPAWN:New("FA-18C Group 3"):InitModex(113) -- Coming in from W after ~18 min
|
||||
local F14=SPAWN:New("F-14B 2ship"):InitModex(211) -- Coming in from SW after ~ 4 min
|
||||
local E2D=SPAWN:New("E-2D Group"):InitModex(311) -- Coming in from NE after ~10 min
|
||||
local S3B=SPAWN:New("S-3B Group"):InitModex(411) -- Coming in from S after ~16 min
|
||||
|
||||
-- Spawn always 9 min before the recovery window opens.
|
||||
local spawntimes={"8:51", "14:51", "20:51"}
|
||||
for _,spawntime in pairs(spawntimes) do
|
||||
local _time=UTILS.ClockToSeconds(spawntime)-timer.getAbsTime()
|
||||
if _time>0 then
|
||||
SCHEDULER:New(nil, F181.Spawn, {F181}, _time)
|
||||
SCHEDULER:New(nil, F182.Spawn, {F182}, _time)
|
||||
SCHEDULER:New(nil, F183.Spawn, {F183}, _time)
|
||||
SCHEDULER:New(nil, F14.Spawn, {F14}, _time)
|
||||
SCHEDULER:New(nil, E2D.Spawn, {E2D}, _time)
|
||||
SCHEDULER:New(nil, S3B.Spawn, {S3B}, _time)
|
||||
end
|
||||
end
|
||||
|
||||
Binary file not shown.
@@ -1,189 +0,0 @@
|
||||
-- View scripts
|
||||
-- Copyright (C) 2004, Eagle Dynamics.
|
||||
DisableCombatViews = false -- F5 & Ctrl-F5
|
||||
ExternalObjectsLockDistance = 10000.0
|
||||
ShowTargetInfo = false
|
||||
CameraTerrainRestriction = true
|
||||
hAngleRearDefault = 180
|
||||
vAngleRearDefault = -8.0
|
||||
vAngleRearMin = -90 -- -8.0
|
||||
vAngleRearMax = 90.0
|
||||
|
||||
dbg_shell = "weapons.shells.PKT_7_62_T" -- 23mm shell
|
||||
--dbg_shell = "weapons.shells.2A42_30_AP"
|
||||
--dbg_shell = "weapons.nurs.WGr21"
|
||||
--dbg_shell = "weapons.shells.2A64_152" -- 152mm shell
|
||||
dbg_shell_v0 = -1 -- Muzzle speed m/s (-1 - speed from shall database)
|
||||
dbg_shell_fire_rate = 120
|
||||
--reformatted per-unit data to be mod system friendly
|
||||
--this file is no longer should be edited for adding new flyable aircraft , DCS automatically check core database (i.e. where you define your aircraft in aircraft table just define ViewSettings and SnapViews tables)
|
||||
|
||||
function default_fighter_player(t)
|
||||
local res = {
|
||||
CameraViewAngleLimits = {20.000000,140.000000},
|
||||
CameraAngleRestriction = {false ,90.000000,0.500000},
|
||||
EyePoint = {0.05 ,0.000000 ,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.4500000},y ={-0.300000,0.100000},z = {-0.220000,0.220000},roll = 90.000000},
|
||||
Allow360rotation = false,
|
||||
CameraAngleLimits = {200,-80.000000,110.000000},
|
||||
ShoulderSize = 0.2, -- move body when azimuth value more then 90 degrees
|
||||
}
|
||||
if t then
|
||||
for i,o in pairs(t) do
|
||||
res[i] = o
|
||||
end
|
||||
end
|
||||
return res
|
||||
end
|
||||
|
||||
function fulcrum()
|
||||
return {
|
||||
Cockpit = {
|
||||
default_fighter_player({CockpitLocalPoint = {4.71,1.28,0.000000}})
|
||||
},
|
||||
Chase = {
|
||||
LocalPoint = {1.220000,3.750000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-15.080000,6.350000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
end
|
||||
|
||||
ViewSettings = {}
|
||||
ViewSettings["A-10A"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.600000},
|
||||
y = {-0.300000,0.100000},
|
||||
z = {-0.250000,0.250000},
|
||||
roll = 90.000000}}),
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {0.600000,3.682000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-27.000000,12.000000,0.000000},
|
||||
AnglesDefault = {0.000000,-12.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["A-10C"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.600000},
|
||||
y = {-0.300000,0.100000},
|
||||
z = {-0.250000,0.250000},
|
||||
roll = 90.000000}}),
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {0.600000,3.682000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-27.000000,12.000000,0.000000},
|
||||
AnglesDefault = {0.000000,-12.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["F-15C"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {6.210000,1.204000,0.000000}})-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {2.510000,3.604000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-13.790000,6.204000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Ka-50"] = {
|
||||
Cockpit = {
|
||||
[1] = {-- player slot 1
|
||||
CockpitLocalPoint = {3.188000,0.390000,0.000000},
|
||||
CameraViewAngleLimits = {20.000000,120.000000},
|
||||
CameraAngleRestriction = {false,60.000000,0.400000},
|
||||
CameraAngleLimits = {140.000000,-65.000000,90.000000},
|
||||
EyePoint = {0.090000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.020000,0.350000},y ={-0.150000,0.165000},z = {-0.170000,0.170000},roll = 90.000000},
|
||||
},
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.512000,2.790000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.812000,5.390000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["MiG-29A"] = fulcrum()
|
||||
ViewSettings["MiG-29G"] = fulcrum()
|
||||
ViewSettings["MiG-29S"] = fulcrum()
|
||||
|
||||
ViewSettings["Su-25"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {3.352000,0.506000,0.000000}}),-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.348000,2.906000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.648001,5.506000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-25T"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {3.406000,0.466000,0.000000}}),-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.294000,2.866000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.594000,5.466000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-25TM"] = {
|
||||
Cockpit = {
|
||||
[1] = {-- player slot 1
|
||||
CockpitLocalPoint = {4.000000,1.000000,0.000000},
|
||||
CameraViewAngleLimits = {20.000000,140.000000},
|
||||
CameraAngleRestriction = {true,90.000000,0.400000},
|
||||
CameraAngleLimits = {160.000000,-70.000000,90.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.200000,0.200000},y ={-0.200000,0.200000},z = {-0.200000,0.200000},roll = 60.000000},
|
||||
},
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {4.000000,2.000000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {4.000000,2.000000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-27"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {7.959000,1.419000,0.000000}})-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {4.259000,3.819000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-12.041000,6.419000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
|
||||
ViewSettings["Su-33"] = ViewSettings["Su-27"]
|
||||
File diff suppressed because it is too large
Load Diff
@@ -1,128 +0,0 @@
|
||||
-- View scripts
|
||||
-- Copyright (C) 2004, Eagle Dynamics.
|
||||
|
||||
CockpitMouse = true --false
|
||||
CockpitMouseSpeedSlow = 1.0
|
||||
CockpitMouseSpeedNormal = 10.0
|
||||
CockpitMouseSpeedFast = 20.0
|
||||
CockpitKeyboardAccelerationSlow = 5.0
|
||||
CockpitKeyboardAccelerationNormal = 30.0
|
||||
CockpitKeyboardAccelerationFast = 80.0
|
||||
CockpitKeyboardZoomAcceleration = 300.0
|
||||
DisableSnapViewsSaving = false
|
||||
UseDefaultSnapViews = true
|
||||
CockpitPanStepHor = 45.0
|
||||
CockpitPanStepVert = 30.0
|
||||
CockpitNyMove = true
|
||||
|
||||
CockpitHAngleAccelerateTimeMax = 0.15
|
||||
CockpitVAngleAccelerateTimeMax = 0.15
|
||||
CockpitZoomAccelerateTimeMax = 0.2
|
||||
|
||||
function NaturalHeadMoving(tang, roll, omz)
|
||||
local r = roll
|
||||
if r > 90.0 then
|
||||
r = 180.0 - r
|
||||
elseif roll < -90.0 then
|
||||
r = -180.0 - r
|
||||
end
|
||||
local hAngle = -0.25 * r
|
||||
local vAngle = math.min(math.max(0.0, 0.4 * tang + 45.0 * omz), 90.0)
|
||||
return hAngle, vAngle
|
||||
end
|
||||
|
||||
ExternalMouse = true
|
||||
ExternalMouseSpeedSlow = 1.0
|
||||
ExternalMouseSpeedNormal = 5.0
|
||||
ExternalMouseSpeedFast = 20.0
|
||||
ExternalViewAngleMin = 3.0
|
||||
ExternalViewAngleMax = 140.0
|
||||
ExternalViewAngleDefault = 60.0
|
||||
ExternalKeyboardZoomAcceleration = 30.0
|
||||
ExternalKeyboardZoomAccelerateTimeMax = 1.0
|
||||
ExplosionExpoTime = 4.0
|
||||
ExternalKeyboardAccelerationSlow = 1.0
|
||||
ExternalKeyboardAccelerationNormal = 10.0
|
||||
ExternalKeyboardAccelerationFast = 30.0
|
||||
ExternalHAngleAccelerateTimeMax = 3.0
|
||||
ExternalVAngleAccelerateTimeMax = 3.0
|
||||
ExternalDistAccelerateTimeMax = 3.0
|
||||
ExternalHAngleLocalAccelerateTimeMax = 3.0
|
||||
ExternalVAngleLocalAccelerateTimeMax = 3.0
|
||||
ExternalAngleNormalDiscreteStep = 15.0/ExternalKeyboardAccelerationNormal -- When 'S' is pressed only
|
||||
ChaseCameraNyMove = true
|
||||
FreeCameraAngleIncrement = 3.0
|
||||
FreeCameraDistanceIncrement = 200.0
|
||||
FreeCameraLeftRightIncrement = 2.0
|
||||
FreeCameraAltitudeIncrement = 2.0
|
||||
FreeCameraScalarSpeedAcceleration = 0.1
|
||||
xMinMap = -300000
|
||||
xMaxMap = 500000
|
||||
yMinMap = -400000
|
||||
yMaxMap = 200000
|
||||
dxMap = 150000
|
||||
dyMap = 100000
|
||||
|
||||
head_roll_shaking = true
|
||||
head_roll_shaking_max = 30.0
|
||||
head_roll_shaking_compensation_gain = 0.3
|
||||
|
||||
-- CameraJiggle() and CameraFloat() functions make camera position
|
||||
-- dependent on FPS so be careful in using the Shift-J command with tracks, please.
|
||||
-- uncomment to use custom jiggle functions
|
||||
--[[
|
||||
function CameraJiggle(t,rnd1,rnd2,rnd3)
|
||||
local rotX, rotY, rotZ
|
||||
rotX = 0.05 * rnd1 * math.sin(37.0 * (t - 0.0))
|
||||
rotY = 0.05 * rnd2 * math.sin(41.0 * (t - 1.0))
|
||||
rotZ = 0.05 * rnd3 * math.sin(53.0 * (t - 2.0))
|
||||
return rotX, rotY, rotZ
|
||||
end
|
||||
|
||||
function CameraFloat(t)
|
||||
local dX, dY, dZ
|
||||
dX = 0.61 * math.sin(0.7 * t) + 0.047 * math.sin(1.6 * t);
|
||||
dY = 0.43 * math.sin(0.6 * t) + 0.067 * math.sin(1.7 * t);
|
||||
dZ = 0.53 * math.sin(1.0 * t) + 0.083 * math.sin(1.9 * t);
|
||||
return dX, dY, dZ
|
||||
end
|
||||
--]]
|
||||
--Debug keys
|
||||
|
||||
DEBUG_TEXT = 1
|
||||
DEBUG_GEOMETRY = 2
|
||||
|
||||
debug_keys = {
|
||||
[DEBUG_TEXT] = 1,
|
||||
[DEBUG_GEOMETRY] = 1
|
||||
}
|
||||
|
||||
function onDebugCommand(command)
|
||||
if command == 10000 then
|
||||
if debug_keys[DEBUG_TEXT] ~= 0 or debug_keys[DEBUG_GEOMETRY] ~= 0 then
|
||||
debug_keys[DEBUG_GEOMETRY] = 0
|
||||
debug_keys[DEBUG_TEXT] = 0
|
||||
else
|
||||
debug_keys[DEBUG_GEOMETRY] = 1
|
||||
debug_keys[DEBUG_TEXT] = 1
|
||||
end
|
||||
elseif command == 10001 then
|
||||
if debug_keys[DEBUG_TEXT] ~= 0 then
|
||||
debug_keys[DEBUG_TEXT] = 0
|
||||
else
|
||||
debug_keys[DEBUG_TEXT] = 1
|
||||
end
|
||||
elseif command == 10002 then
|
||||
if debug_keys[DEBUG_GEOMETRY] ~= 0 then
|
||||
debug_keys[DEBUG_GEOMETRY] = 0
|
||||
else
|
||||
debug_keys[DEBUG_GEOMETRY] = 1
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
-- gain values for TrackIR , to unify responce on diffrent types of aircraft
|
||||
TrackIR_gain_x = -0.6
|
||||
TrackIR_gain_y = 0.3
|
||||
TrackIR_gain_z = -0.25
|
||||
TrackIR_gain_roll = -90
|
||||
@@ -1,880 +0,0 @@
|
||||
SAT_SYS_GLONASS = 0
|
||||
SAT_SYS_GPS = 1
|
||||
|
||||
almanac = {}
|
||||
--GPS
|
||||
almanac[0] = {}
|
||||
almanac[0]["System"] = SAT_SYS_GPS
|
||||
almanac[0]["Number"] = 1
|
||||
almanac[0]["Orbital"] = "F"
|
||||
almanac[0]["Eccentricity"] = 6.294000e-003
|
||||
almanac[0]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[0]["Orbital_Inclination"] = 9.885676e-001
|
||||
almanac[0]["Rate_of_Right_Ascen"] = -7.862702e-009
|
||||
almanac[0]["SQRT_A"] = 5.153700e+003
|
||||
almanac[0]["Right_Ascen_at_Week"] = 8.096750e-001
|
||||
almanac[0]["Argument_of_Perigee"] = -1.777773e+000
|
||||
almanac[0]["Mean_Anom"] = -5.315745e-001
|
||||
almanac[0]["week"] = 1390
|
||||
|
||||
almanac[1] = {}
|
||||
almanac[1]["System"] = SAT_SYS_GPS
|
||||
almanac[1]["Number"] = 2
|
||||
almanac[1]["Orbital"] = "C"
|
||||
almanac[1]["Eccentricity"] = 8.794000e-003
|
||||
almanac[1]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[1]["Orbital_Inclination"] = 9.487811e-001
|
||||
almanac[1]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[1]["SQRT_A"] = 5.153700e+003
|
||||
almanac[1]["Right_Ascen_at_Week"] = -1.329172e+000
|
||||
almanac[1]["Argument_of_Perigee"] = 2.138637e+000
|
||||
almanac[1]["Mean_Anom"] = 7.311702e-001
|
||||
almanac[1]["week"] = 1390
|
||||
|
||||
almanac[2] = {}
|
||||
almanac[2]["System"] = SAT_SYS_GPS
|
||||
almanac[2]["Number"] = 3
|
||||
almanac[2]["Orbital"] = "F"
|
||||
almanac[2]["Eccentricity"] = 8.424000e-003
|
||||
almanac[2]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[2]["Orbital_Inclination"] = 9.262804e-001
|
||||
almanac[2]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[2]["SQRT_A"] = 5.153600e+003
|
||||
almanac[2]["Right_Ascen_at_Week"] = -2.341514e+000
|
||||
almanac[2]["Argument_of_Perigee"] = 6.749357e-001
|
||||
almanac[2]["Mean_Anom"] = -2.296153e-001
|
||||
almanac[2]["week"] = 1389
|
||||
|
||||
almanac[3] = {}
|
||||
almanac[3]["System"] = SAT_SYS_GPS
|
||||
almanac[3]["Number"] = 4
|
||||
almanac[3]["Orbital"] = "D"
|
||||
almanac[3]["Eccentricity"] = 7.413000e-003
|
||||
almanac[3]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[3]["Orbital_Inclination"] = 9.482889e-001
|
||||
almanac[3]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[3]["SQRT_A"] = 5.153600e+003
|
||||
almanac[3]["Right_Ascen_at_Week"] = -1.309589e+000
|
||||
almanac[3]["Argument_of_Perigee"] = 1.623504e-001
|
||||
almanac[3]["Mean_Anom"] = -3.022943e+000
|
||||
almanac[3]["week"] = 1390
|
||||
|
||||
almanac[4] = {}
|
||||
almanac[4]["System"] = SAT_SYS_GPS
|
||||
almanac[4]["Number"] = 5
|
||||
almanac[4]["Orbital"] = "B"
|
||||
almanac[4]["Eccentricity"] = 7.432000e-003
|
||||
almanac[4]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[4]["Orbital_Inclination"] = 9.387437e-001
|
||||
almanac[4]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[4]["SQRT_A"] = 5.153700e+003
|
||||
almanac[4]["Right_Ascen_at_Week"] = 2.779487e+000
|
||||
almanac[4]["Argument_of_Perigee"] = 1.099033e+000
|
||||
almanac[4]["Mean_Anom"] = 2.970984e+000
|
||||
almanac[4]["week"] = 1390
|
||||
|
||||
almanac[5] = {}
|
||||
almanac[5]["System"] = SAT_SYS_GPS
|
||||
almanac[5]["Number"] = 6
|
||||
almanac[5]["Orbital"] = "C"
|
||||
almanac[5]["Eccentricity"] = 6.020000e-003
|
||||
almanac[5]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[5]["Orbital_Inclination"] = 9.337591e-001
|
||||
almanac[5]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[5]["SQRT_A"] = 5.153600e+003
|
||||
almanac[5]["Right_Ascen_at_Week"] = -2.407627e+000
|
||||
almanac[5]["Argument_of_Perigee"] = -1.788263e+000
|
||||
almanac[5]["Mean_Anom"] = -2.149877e+000
|
||||
almanac[5]["week"] = 1390
|
||||
|
||||
almanac[6] = {}
|
||||
almanac[6]["System"] = SAT_SYS_GPS
|
||||
almanac[6]["Number"] = 7
|
||||
almanac[6]["Orbital"] = "C"
|
||||
almanac[6]["Eccentricity"] = 1.052400e-002
|
||||
almanac[6]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[6]["Orbital_Inclination"] = 9.353229e-001
|
||||
almanac[6]["Rate_of_Right_Ascen"] = -8.080868e-009
|
||||
almanac[6]["SQRT_A"] = 5.153700e+003
|
||||
almanac[6]["Right_Ascen_at_Week"] = -2.433580e+000
|
||||
almanac[6]["Argument_of_Perigee"] = -1.767301e+000
|
||||
almanac[6]["Mean_Anom"] = -3.141503e+000
|
||||
almanac[6]["week"] = 1390
|
||||
|
||||
almanac[7] = {}
|
||||
almanac[7]["System"] = SAT_SYS_GPS
|
||||
almanac[7]["Number"] = 8
|
||||
almanac[7]["Orbital"] = "A"
|
||||
almanac[7]["Eccentricity"] = 9.822000e-003
|
||||
almanac[7]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[7]["Orbital_Inclination"] = 9.741390e-001
|
||||
almanac[7]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[7]["SQRT_A"] = 5.153600e+003
|
||||
almanac[7]["Right_Ascen_at_Week"] = 1.857849e+000
|
||||
almanac[7]["Argument_of_Perigee"] = 2.674034e+000
|
||||
almanac[7]["Mean_Anom"] = -2.009745e+000
|
||||
almanac[7]["week"] = 1390
|
||||
|
||||
almanac[8] = {}
|
||||
almanac[8]["System"] = SAT_SYS_GPS
|
||||
almanac[8]["Number"] = 9
|
||||
almanac[8]["Orbital"] = "A"
|
||||
almanac[8]["Eccentricity"] = 1.839300e-002
|
||||
almanac[8]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[8]["Orbital_Inclination"] = 9.617541e-001
|
||||
almanac[8]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[8]["SQRT_A"] = 5.153600e+003
|
||||
almanac[8]["Right_Ascen_at_Week"] = 1.777005e+000
|
||||
almanac[8]["Argument_of_Perigee"] = 1.274962e+000
|
||||
almanac[8]["Mean_Anom"] = -2.349578e+000
|
||||
almanac[8]["week"] = 1390
|
||||
|
||||
almanac[9] = {}
|
||||
almanac[9]["System"] = SAT_SYS_GPS
|
||||
almanac[9]["Number"] = 10
|
||||
almanac[9]["Orbital"] = "E"
|
||||
almanac[9]["Eccentricity"] = 7.061000e-003
|
||||
almanac[9]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[9]["Orbital_Inclination"] = 9.728876e-001
|
||||
almanac[9]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[9]["SQRT_A"] = 5.153600e+003
|
||||
almanac[9]["Right_Ascen_at_Week"] = -2.563014e-001
|
||||
almanac[9]["Argument_of_Perigee"] = 4.377980e-001
|
||||
almanac[9]["Mean_Anom"] = 1.210716e+000
|
||||
almanac[9]["week"] = 1390
|
||||
|
||||
almanac[10] = {}
|
||||
almanac[10]["System"] = SAT_SYS_GPS
|
||||
almanac[10]["Number"] = 11
|
||||
almanac[10]["Orbital"] = "D"
|
||||
almanac[10]["Eccentricity"] = 5.744000e-003
|
||||
almanac[10]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[10]["Orbital_Inclination"] = 8.959309e-001
|
||||
almanac[10]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[10]["SQRT_A"] = 5.153600e+003
|
||||
almanac[10]["Right_Ascen_at_Week"] = -1.478816e+000
|
||||
almanac[10]["Argument_of_Perigee"] = 3.750011e-001
|
||||
almanac[10]["Mean_Anom"] = -1.522048e+000
|
||||
almanac[10]["week"] = 1390
|
||||
|
||||
almanac[11] = {}
|
||||
almanac[11]["System"] = SAT_SYS_GPS
|
||||
almanac[11]["Number"] = 13
|
||||
almanac[11]["Orbital"] = "F"
|
||||
almanac[11]["Eccentricity"] = 3.088000e-003
|
||||
almanac[11]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[11]["Orbital_Inclination"] = 9.927564e-001
|
||||
almanac[11]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[11]["SQRT_A"] = 5.153700e+003
|
||||
almanac[11]["Right_Ascen_at_Week"] = 7.956600e-001
|
||||
almanac[11]["Argument_of_Perigee"] = 1.279395e+000
|
||||
almanac[11]["Mean_Anom"] = 1.004349e+000
|
||||
almanac[11]["week"] = 1390
|
||||
|
||||
almanac[12] = {}
|
||||
almanac[12]["System"] = SAT_SYS_GPS
|
||||
almanac[12]["Number"] = 14
|
||||
almanac[12]["Orbital"] = "F"
|
||||
almanac[12]["Eccentricity"] = 2.591000e-003
|
||||
almanac[12]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[12]["Orbital_Inclination"] = 9.868729e-001
|
||||
almanac[12]["Rate_of_Right_Ascen"] = -7.885391e-009
|
||||
almanac[12]["SQRT_A"] = 5.153600e+003
|
||||
almanac[12]["Right_Ascen_at_Week"] = 7.819592e-001
|
||||
almanac[12]["Argument_of_Perigee"] = -2.158621e+000
|
||||
almanac[12]["Mean_Anom"] = 5.412611e-001
|
||||
almanac[12]["week"] = 1390
|
||||
|
||||
almanac[13] = {}
|
||||
almanac[13]["System"] = SAT_SYS_GPS
|
||||
almanac[13]["Number"] = 15
|
||||
almanac[13]["Orbital"] = "D"
|
||||
almanac[13]["Eccentricity"] = 9.828000e-003
|
||||
almanac[13]["Time_of_Applicability"] = 3.194880e+005
|
||||
almanac[13]["Orbital_Inclination"] = 9.554204e-001
|
||||
almanac[13]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[13]["SQRT_A"] = 5.153600e+003
|
||||
almanac[13]["Right_Ascen_at_Week"] = -1.123869e+000
|
||||
almanac[13]["Argument_of_Perigee"] = 2.690266e+000
|
||||
almanac[13]["Mean_Anom"] = 2.220476e+000
|
||||
almanac[13]["week"] = 1389
|
||||
|
||||
almanac[14] = {}
|
||||
almanac[14]["System"] = SAT_SYS_GPS
|
||||
almanac[14]["Number"] = 16
|
||||
almanac[14]["Orbital"] = "B"
|
||||
almanac[14]["Eccentricity"] = 3.494000e-003
|
||||
almanac[14]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[14]["Orbital_Inclination"] = 9.629340e-001
|
||||
almanac[14]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[14]["SQRT_A"] = 5.153700e+003
|
||||
almanac[14]["Right_Ascen_at_Week"] = 2.873124e+000
|
||||
almanac[14]["Argument_of_Perigee"] = -7.819243e-001
|
||||
almanac[14]["Mean_Anom"] = 2.623629e+000
|
||||
almanac[14]["week"] = 1390
|
||||
|
||||
almanac[15] = {}
|
||||
almanac[15]["System"] = SAT_SYS_GPS
|
||||
almanac[15]["Number"] = 17
|
||||
almanac[15]["Orbital"] = "C"
|
||||
almanac[15]["Eccentricity"] = 2.141000e-003
|
||||
almanac[15]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[15]["Orbital_Inclination"] = 9.601170e-001
|
||||
almanac[15]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[15]["SQRT_A"] = 5.153700e+003
|
||||
almanac[15]["Right_Ascen_at_Week"] = -2.371499e+000
|
||||
almanac[15]["Argument_of_Perigee"] = 3.087694e+000
|
||||
almanac[15]["Mean_Anom"] = 1.611217e+000
|
||||
almanac[15]["week"] = 1390
|
||||
|
||||
almanac[16] = {}
|
||||
almanac[16]["System"] = SAT_SYS_GPS
|
||||
almanac[16]["Number"] = 18
|
||||
almanac[16]["Orbital"] = "E"
|
||||
almanac[16]["Eccentricity"] = 7.636000e-003
|
||||
almanac[16]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[16]["Orbital_Inclination"] = 9.569597e-001
|
||||
almanac[16]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[16]["SQRT_A"] = 5.153700e+003
|
||||
almanac[16]["Right_Ascen_at_Week"] = -2.359858e-001
|
||||
almanac[16]["Argument_of_Perigee"] = -2.649216e+000
|
||||
almanac[16]["Mean_Anom"] = 2.675029e+000
|
||||
almanac[16]["week"] = 1390
|
||||
|
||||
almanac[17] = {}
|
||||
almanac[17]["System"] = SAT_SYS_GPS
|
||||
almanac[17]["Number"] = 19
|
||||
almanac[17]["Orbital"] = "C"
|
||||
almanac[17]["Eccentricity"] = 3.602000e-003
|
||||
almanac[17]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[17]["Orbital_Inclination"] = 9.580209e-001
|
||||
almanac[17]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[17]["SQRT_A"] = 5.153600e+003
|
||||
almanac[17]["Right_Ascen_at_Week"] = -2.312385e+000
|
||||
almanac[17]["Argument_of_Perigee"] = -1.161079e+000
|
||||
almanac[17]["Mean_Anom"] = 1.310619e+000
|
||||
almanac[17]["week"] = 1390
|
||||
|
||||
almanac[18] = {}
|
||||
almanac[18]["System"] = SAT_SYS_GPS
|
||||
almanac[18]["Number"] = 20
|
||||
almanac[18]["Orbital"] = "E"
|
||||
almanac[18]["Eccentricity"] = 2.796000e-003
|
||||
almanac[18]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[18]["Orbital_Inclination"] = 9.564693e-001
|
||||
almanac[18]["Rate_of_Right_Ascen"] = -7.908080e-009
|
||||
almanac[18]["SQRT_A"] = 5.153600e+003
|
||||
almanac[18]["Right_Ascen_at_Week"] = -2.889565e-001
|
||||
almanac[18]["Argument_of_Perigee"] = 1.379612e+000
|
||||
almanac[18]["Mean_Anom"] = 2.461750e+000
|
||||
almanac[18]["week"] = 1390
|
||||
|
||||
almanac[19] = {}
|
||||
almanac[19]["System"] = SAT_SYS_GPS
|
||||
almanac[19]["Number"] = 21
|
||||
almanac[19]["Orbital"] = "D"
|
||||
almanac[19]["Eccentricity"] = 1.162900e-002
|
||||
almanac[19]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[19]["Orbital_Inclination"] = 9.418592e-001
|
||||
almanac[19]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[19]["SQRT_A"] = 5.153600e+003
|
||||
almanac[19]["Right_Ascen_at_Week"] = -1.289972e+000
|
||||
almanac[19]["Argument_of_Perigee"] = -2.923686e+000
|
||||
almanac[19]["Mean_Anom"] = -2.349194e+000
|
||||
almanac[19]["week"] = 1390
|
||||
|
||||
almanac[20] = {}
|
||||
almanac[20]["System"] = SAT_SYS_GPS
|
||||
almanac[20]["Number"] = 22
|
||||
almanac[20]["Orbital"] = "E"
|
||||
almanac[20]["Eccentricity"] = 4.893000e-003
|
||||
almanac[20]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[20]["Orbital_Inclination"] = 9.545093e-001
|
||||
almanac[20]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[20]["SQRT_A"] = 5.153600e+003
|
||||
almanac[20]["Right_Ascen_at_Week"] = -2.280969e-001
|
||||
almanac[20]["Argument_of_Perigee"] = -1.674502e+000
|
||||
almanac[20]["Mean_Anom"] = 1.106852e+000
|
||||
almanac[20]["week"] = 1390
|
||||
|
||||
almanac[21] = {}
|
||||
almanac[21]["System"] = SAT_SYS_GPS
|
||||
almanac[21]["Number"] = 23
|
||||
almanac[21]["Orbital"] = "F"
|
||||
almanac[21]["Eccentricity"] = 4.822000e-003
|
||||
almanac[21]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[21]["Orbital_Inclination"] = 9.691247e-001
|
||||
almanac[21]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[21]["SQRT_A"] = 5.153700e+003
|
||||
almanac[21]["Right_Ascen_at_Week"] = 7.667399e-001
|
||||
almanac[21]["Argument_of_Perigee"] = 2.497634e+000
|
||||
almanac[21]["Mean_Anom"] = 3.184700e-001
|
||||
almanac[21]["week"] = 1390
|
||||
|
||||
almanac[22] = {}
|
||||
almanac[22]["System"] = SAT_SYS_GPS
|
||||
almanac[22]["Number"] = 24
|
||||
almanac[22]["Orbital"] = "D"
|
||||
almanac[22]["Eccentricity"] = 9.277000e-003
|
||||
almanac[22]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[22]["Orbital_Inclination"] = 9.585183e-001
|
||||
almanac[22]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[22]["SQRT_A"] = 5.153900e+003
|
||||
almanac[22]["Right_Ascen_at_Week"] = -1.274840e+000
|
||||
almanac[22]["Argument_of_Perigee"] = -8.815651e-001
|
||||
almanac[22]["Mean_Anom"] = -1.695551e+000
|
||||
almanac[22]["week"] = 1390
|
||||
|
||||
almanac[23] = {}
|
||||
almanac[23]["System"] = SAT_SYS_GPS
|
||||
almanac[23]["Number"] = 25
|
||||
almanac[23]["Orbital"] = "A"
|
||||
almanac[23]["Eccentricity"] = 1.257400e-002
|
||||
almanac[23]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[23]["Orbital_Inclination"] = 9.551027e-001
|
||||
almanac[23]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[23]["SQRT_A"] = 5.153600e+003
|
||||
almanac[23]["Right_Ascen_at_Week"] = 1.721853e+000
|
||||
almanac[23]["Argument_of_Perigee"] = -1.329870e+000
|
||||
almanac[23]["Mean_Anom"] = -1.769623e+000
|
||||
almanac[23]["week"] = 1390
|
||||
|
||||
almanac[24] = {}
|
||||
almanac[24]["System"] = SAT_SYS_GPS
|
||||
almanac[24]["Number"] = 26
|
||||
almanac[24]["Orbital"] = "F"
|
||||
almanac[24]["Eccentricity"] = 1.745700e-002
|
||||
almanac[24]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[24]["Orbital_Inclination"] = 9.908749e-001
|
||||
almanac[24]["Rate_of_Right_Ascen"] = -7.840012e-009
|
||||
almanac[24]["SQRT_A"] = 5.153700e+003
|
||||
almanac[24]["Right_Ascen_at_Week"] = 7.961836e-001
|
||||
almanac[24]["Argument_of_Perigee"] = 8.161502e-001
|
||||
almanac[24]["Mean_Anom"] = -5.841961e-001
|
||||
almanac[24]["week"] = 1390
|
||||
|
||||
almanac[25] = {}
|
||||
almanac[25]["System"] = SAT_SYS_GPS
|
||||
almanac[25]["Number"] = 27
|
||||
almanac[25]["Orbital"] = "A"
|
||||
almanac[25]["Eccentricity"] = 1.991000e-002
|
||||
almanac[25]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[25]["Orbital_Inclination"] = 9.596563e-001
|
||||
almanac[25]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[25]["SQRT_A"] = 5.153600e+003
|
||||
almanac[25]["Right_Ascen_at_Week"] = 1.754124e+000
|
||||
almanac[25]["Argument_of_Perigee"] = -1.900854e+000
|
||||
almanac[25]["Mean_Anom"] = 3.046487e+000
|
||||
almanac[25]["week"] = 1390
|
||||
|
||||
almanac[26] = {}
|
||||
almanac[26]["System"] = SAT_SYS_GPS
|
||||
almanac[26]["Number"] = 28
|
||||
almanac[26]["Orbital"] = "B"
|
||||
almanac[26]["Eccentricity"] = 1.162800e-002
|
||||
almanac[26]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[26]["Orbital_Inclination"] = 9.610106e-001
|
||||
almanac[26]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[26]["SQRT_A"] = 5.153600e+003
|
||||
almanac[26]["Right_Ascen_at_Week"] = 2.882583e+000
|
||||
almanac[26]["Argument_of_Perigee"] = -2.242868e+000
|
||||
almanac[26]["Mean_Anom"] = 1.860642e+000
|
||||
almanac[26]["week"] = 1390
|
||||
|
||||
almanac[27] = {}
|
||||
almanac[27]["System"] = SAT_SYS_GPS
|
||||
almanac[27]["Number"] = 29
|
||||
almanac[27]["Orbital"] = "F"
|
||||
almanac[27]["Eccentricity"] = 9.462000e-003
|
||||
almanac[27]["Time_of_Applicability"] = 1.474560e+005
|
||||
almanac[27]["Orbital_Inclination"] = 9.874838e-001
|
||||
almanac[27]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[27]["SQRT_A"] = 5.153700e+003
|
||||
almanac[27]["Right_Ascen_at_Week"] = 7.647503e-001
|
||||
almanac[27]["Argument_of_Perigee"] = -8.614589e-001
|
||||
almanac[27]["Mean_Anom"] = -4.488983e-001
|
||||
almanac[27]["week"] = 1390
|
||||
|
||||
almanac[28] = {}
|
||||
almanac[28]["System"] = SAT_SYS_GPS
|
||||
almanac[28]["Number"] = 30
|
||||
almanac[28]["Orbital"] = "B"
|
||||
almanac[28]["Eccentricity"] = 9.296000e-003
|
||||
almanac[28]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[28]["Orbital_Inclination"] = 9.452992e-001
|
||||
almanac[28]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[28]["SQRT_A"] = 5.153600e+003
|
||||
almanac[28]["Right_Ascen_at_Week"] = 2.826698e+000
|
||||
almanac[28]["Argument_of_Perigee"] = 1.306413e+000
|
||||
almanac[28]["Mean_Anom"] = 2.148725e+000
|
||||
almanac[28]["week"] = 1390
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
--GLONASS
|
||||
--1 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 1-8
|
||||
almanac[29] = {}
|
||||
almanac[29]["System"] = SAT_SYS_GLONASS
|
||||
almanac[29]["Number"] = 1
|
||||
almanac[29]["Orbital"] = 1
|
||||
almanac[29]["GLONASS_Data"] = {}
|
||||
almanac[29]["GLONASS_Data"]["NKU_Number"] = 796
|
||||
almanac[29]["GLONASS_Data"]["Cosmos_Number"] = 2411
|
||||
almanac[29]["Eccentricity"] = 1.184000e-003
|
||||
almanac[29]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[29]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[29]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[29]["SQRT_A"] = 5.050500e+003
|
||||
almanac[29]["Right_Ascen_at_Week"] = 5.979807e+000
|
||||
almanac[29]["Argument_of_Perigee"] = 2.622634e+000
|
||||
almanac[29]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[29]["week"] = 1390
|
||||
almanac[29]["Commit_date"] = "06.02.2005"
|
||||
almanac[29]["Life_dates"] = {}
|
||||
|
||||
almanac[30] = {}
|
||||
almanac[30]["System"] = SAT_SYS_GLONASS
|
||||
almanac[30]["Number"] = 2
|
||||
almanac[30]["Orbital"] = 1
|
||||
almanac[30]["GLONASS_Data"] = {}
|
||||
almanac[30]["GLONASS_Data"]["NKU_Number"] = 794
|
||||
almanac[30]["GLONASS_Data"]["Cosmos_Number"] = 2401
|
||||
almanac[30]["Eccentricity"] = 4.486000e-003
|
||||
almanac[30]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[30]["Orbital_Inclination"] = 1.128459e+000
|
||||
almanac[30]["Rate_of_Right_Ascen"] = -6.759654e-009
|
||||
almanac[30]["SQRT_A"] = 5.050500e+003
|
||||
almanac[30]["Right_Ascen_at_Week"] = 5.997871e+000
|
||||
almanac[30]["Argument_of_Perigee"] = 1.709531e+000
|
||||
almanac[30]["Mean_Anom"] = -5.367633e+000
|
||||
almanac[30]["week"] = 1390
|
||||
almanac[30]["Commit_date"] = "02.02.2004"
|
||||
almanac[30]["Life_dates"] = {}
|
||||
|
||||
almanac[31] = {}
|
||||
almanac[31]["System"] = SAT_SYS_GLONASS
|
||||
almanac[31]["Number"] = 3
|
||||
almanac[31]["Orbital"] = 1
|
||||
almanac[31]["GLONASS_Data"] = {}
|
||||
almanac[31]["GLONASS_Data"]["NKU_Number"] = 789
|
||||
almanac[31]["GLONASS_Data"]["Cosmos_Number"] = 2381
|
||||
almanac[31]["Eccentricity"] = 2.459000e-003
|
||||
almanac[31]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[31]["Orbital_Inclination"] = 1.122958e+000
|
||||
almanac[31]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[31]["SQRT_A"] = 5.050500e+003
|
||||
almanac[31]["Right_Ascen_at_Week"] = 5.960713e+000
|
||||
almanac[31]["Argument_of_Perigee"] = -2.683407e+000
|
||||
almanac[31]["Mean_Anom"] = -1.791788e+000
|
||||
almanac[31]["week"] = 1390
|
||||
almanac[31]["Commit_date"] = "04.01.2002"
|
||||
almanac[31]["Life_dates"] = {}
|
||||
|
||||
almanac[32] = {}
|
||||
almanac[32]["System"] = SAT_SYS_GLONASS
|
||||
almanac[32]["Number"] = 4
|
||||
almanac[32]["Orbital"] = 1
|
||||
almanac[32]["GLONASS_Data"] = {}
|
||||
almanac[32]["GLONASS_Data"]["NKU_Number"] = 795
|
||||
almanac[29]["GLONASS_Data"]["Cosmos_Number"] = 2403
|
||||
almanac[32]["Eccentricity"] = 4.054000e-003
|
||||
almanac[32]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[32]["Orbital_Inclination"] = 1.128543e+000
|
||||
almanac[32]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[32]["SQRT_A"] = 5.050500e+003
|
||||
almanac[32]["Right_Ascen_at_Week"] = 5.998081e+000
|
||||
almanac[32]["Argument_of_Perigee"] = 1.497160e+000
|
||||
almanac[32]["Mean_Anom"] = -4.293681e-001
|
||||
almanac[32]["week"] = 1390
|
||||
almanac[32]["Commit_date"] = "29.01.2004"
|
||||
almanac[32]["Life_dates"] = {}
|
||||
|
||||
almanac[33] = {}
|
||||
almanac[33]["System"] = SAT_SYS_GLONASS
|
||||
almanac[33]["Number"] = 5
|
||||
almanac[33]["Orbital"] = 1
|
||||
almanac[33]["GLONASS_Data"] = {}
|
||||
almanac[33]["GLONASS_Data"]["NKU_Number"] = 711
|
||||
almanac[33]["GLONASS_Data"]["Cosmos_Number"] = 2382
|
||||
almanac[33]["Eccentricity"] = 7.040000e-004
|
||||
almanac[33]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[33]["Orbital_Inclination"] = 1.122886e+000
|
||||
almanac[33]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[33]["SQRT_A"] = 5.050600e+003
|
||||
almanac[33]["Right_Ascen_at_Week"] = 5.960713e+000
|
||||
almanac[33]["Argument_of_Perigee"] = 2.740933e+000
|
||||
almanac[33]["Mean_Anom"] = -2.523604e+000
|
||||
almanac[33]["week"] = 1390
|
||||
almanac[33]["Commit_date"] = "13.02.2003"
|
||||
almanac[33]["Life_dates"] = {}
|
||||
|
||||
almanac[34] = {}
|
||||
almanac[34]["System"] = SAT_SYS_GLONASS
|
||||
almanac[34]["Number"] = 6
|
||||
almanac[34]["Orbital"] = 1
|
||||
almanac[34]["GLONASS_Data"] = {}
|
||||
almanac[34]["GLONASS_Data"]["NKU_Number"] = 701
|
||||
almanac[34]["GLONASS_Data"]["Cosmos_Number"] = 2404
|
||||
almanac[34]["Eccentricity"] = 4.766000e-003
|
||||
almanac[34]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[34]["Orbital_Inclination"] = 1.128276e+000
|
||||
almanac[34]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[34]["SQRT_A"] = 5.050500e+003
|
||||
almanac[34]["Right_Ascen_at_Week"] = 5.997906e+000
|
||||
almanac[34]["Argument_of_Perigee"] = 1.802417e+000
|
||||
almanac[34]["Mean_Anom"] = -2.426512e+000
|
||||
almanac[34]["week"] = 1390
|
||||
almanac[34]["Commit_date"] = "08.12.2004"
|
||||
almanac[34]["Life_dates"] = {}
|
||||
|
||||
almanac[35] = {}
|
||||
almanac[35]["System"] = SAT_SYS_GLONASS
|
||||
almanac[35]["Number"] = 7
|
||||
almanac[35]["Orbital"] = 1
|
||||
almanac[35]["GLONASS_Data"] = {}
|
||||
almanac[35]["GLONASS_Data"]["NKU_Number"] = 712
|
||||
almanac[35]["GLONASS_Data"]["Cosmos_Number"] = 2413
|
||||
almanac[35]["Eccentricity"] = 7.570000e-004
|
||||
almanac[35]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[35]["Orbital_Inclination"] = 1.126344e+000
|
||||
almanac[35]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[35]["SQRT_A"] = 5.050500e+003
|
||||
almanac[35]["Right_Ascen_at_Week"] = 5.979388e+000
|
||||
almanac[35]["Argument_of_Perigee"] = 2.566068e+000
|
||||
almanac[35]["Mean_Anom"] = -3.921228e+000
|
||||
almanac[35]["week"] = 1390
|
||||
almanac[35]["Commit_date"] = "07.10.2005"
|
||||
almanac[35]["Life_dates"] = {}
|
||||
|
||||
almanac[36] = {}
|
||||
almanac[36]["System"] = SAT_SYS_GLONASS
|
||||
almanac[36]["GLONASS_Data"] = {}
|
||||
almanac[36]["Number"] = 8
|
||||
almanac[36]["Orbital"] = 1
|
||||
almanac[36]["GLONASS_Data"] = {}
|
||||
almanac[36]["GLONASS_Data"]["NKU_Number"] = 797
|
||||
almanac[36]["GLONASS_Data"]["Cosmos_Number"] = 2412
|
||||
almanac[36]["Eccentricity"] = 4.060000e-004
|
||||
almanac[36]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[36]["Orbital_Inclination"] = 1.126564e+000
|
||||
almanac[36]["Rate_of_Right_Ascen"] = -6.785834e-009
|
||||
almanac[36]["SQRT_A"] = 5.050600e+003
|
||||
almanac[36]["Right_Ascen_at_Week"] = 5.980069e+000
|
||||
almanac[36]["Argument_of_Perigee"] = 2.673633e+000
|
||||
almanac[36]["Mean_Anom"] = -4.812026e+000
|
||||
almanac[36]["week"] = 1390
|
||||
almanac[36]["Commit_date"] = "06.02.2005"
|
||||
almanac[36]["Life_dates"] = {}
|
||||
|
||||
--3 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 17-24
|
||||
almanac[37] = {}
|
||||
almanac[37]["System"] = SAT_SYS_GLONASS
|
||||
almanac[37]["Number"] = 17
|
||||
almanac[37]["Orbital"] = 3
|
||||
almanac[37]["GLONASS_Data"] = {}
|
||||
almanac[37]["GLONASS_Data"]["NKU_Number"] = 787
|
||||
almanac[37]["GLONASS_Data"]["Cosmos_Number"] = 2375
|
||||
almanac[37]["Eccentricity"] = 5.670000e-004
|
||||
almanac[37]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[37]["Orbital_Inclination"] = 1.126524e+000
|
||||
almanac[37]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[37]["SQRT_A"] = 5.050500e+003
|
||||
almanac[37]["Right_Ascen_at_Week"] = 3.895554e+000
|
||||
almanac[37]["Argument_of_Perigee"] = 6.085085e-001
|
||||
almanac[37]["Mean_Anom"] = -2.977407e+000
|
||||
almanac[37]["week"] = 1390
|
||||
almanac[37]["Commit_date"] = "04.11.2000"
|
||||
almanac[37]["Life_dates"] = {}
|
||||
|
||||
|
||||
almanac[38] = {}
|
||||
almanac[38]["System"] = SAT_SYS_GLONASS
|
||||
almanac[38]["Number"] = 18
|
||||
almanac[38]["Orbital"] = 3
|
||||
almanac[38]["GLONASS_Data"] = {}
|
||||
almanac[38]["GLONASS_Data"]["NKU_Number"] = 783
|
||||
almanac[38]["GLONASS_Data"]["Cosmos_Number"] = 2374
|
||||
almanac[38]["Eccentricity"] = 4.520000e-003
|
||||
almanac[38]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[38]["Orbital_Inclination"] = 1.126239e+000
|
||||
almanac[38]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[38]["SQRT_A"] = 5.050600e+003
|
||||
almanac[38]["Right_Ascen_at_Week"] = 3.894071e+000
|
||||
almanac[38]["Argument_of_Perigee"] = -2.509589e+000
|
||||
almanac[38]["Mean_Anom"] = -1.020057e+000
|
||||
almanac[38]["week"] = 1390
|
||||
almanac[38]["Commit_date"] = "05.01.2001"
|
||||
almanac[38]["Life_dates"] = {}
|
||||
|
||||
almanac[39] = {}
|
||||
almanac[39]["System"] = SAT_SYS_GLONASS
|
||||
almanac[39]["Number"] = 19
|
||||
almanac[39]["Orbital"] = 3
|
||||
almanac[39]["GLONASS_Data"] = {}
|
||||
almanac[39]["GLONASS_Data"]["NKU_Number"] = 798
|
||||
almanac[39]["GLONASS_Data"]["Cosmos_Number"] = 2417
|
||||
almanac[39]["Eccentricity"] = 2.023000e-003
|
||||
almanac[39]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[39]["Orbital_Inclination"] = 1.132205e+000
|
||||
almanac[39]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[39]["SQRT_A"] = 5.050500e+003
|
||||
almanac[39]["Right_Ascen_at_Week"] = 3.884018e+000
|
||||
almanac[39]["Argument_of_Perigee"] = 2.718313e+000
|
||||
almanac[39]["Mean_Anom"] = -3.933620e-001
|
||||
almanac[39]["week"] = 1390
|
||||
almanac[39]["Commit_date"] = "22.01.2006"
|
||||
almanac[39]["Life_dates"] = {}
|
||||
|
||||
almanac[40] = {}
|
||||
almanac[40]["System"] = SAT_SYS_GLONASS
|
||||
almanac[40]["Number"] = 20
|
||||
almanac[40]["Orbital"] = 3
|
||||
almanac[40]["GLONASS_Data"] = {}
|
||||
almanac[40]["GLONASS_Data"]["NKU_Number"] = 793
|
||||
almanac[40]["GLONASS_Data"]["Cosmos_Number"] = 2396
|
||||
almanac[40]["Eccentricity"] = 1.822000e-003
|
||||
almanac[40]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[40]["Orbital_Inclination"] = 1.129789e+000
|
||||
almanac[40]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[40]["SQRT_A"] = 5.050500e+003
|
||||
almanac[40]["Right_Ascen_at_Week"] = 3.896863e+000
|
||||
almanac[40]["Argument_of_Perigee"] = 2.723776e+000
|
||||
almanac[40]["Mean_Anom"] = -1.193647e+000
|
||||
almanac[40]["week"] = 1390
|
||||
almanac[40]["Commit_date"] = "31.01.2003"
|
||||
almanac[40]["Life_dates"] = {}
|
||||
|
||||
almanac[41] = {}
|
||||
almanac[41]["System"] = SAT_SYS_GLONASS
|
||||
almanac[41]["Number"] = 21
|
||||
almanac[41]["Orbital"] = 3
|
||||
almanac[41]["GLONASS_Data"] = {}
|
||||
almanac[41]["GLONASS_Data"]["NKU_Number"] = 792
|
||||
almanac[41]["GLONASS_Data"]["Cosmos_Number"] = 2395
|
||||
almanac[41]["Eccentricity"] = 5.290000e-004
|
||||
almanac[41]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[41]["Orbital_Inclination"] = 1.129957e+000
|
||||
almanac[41]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[41]["SQRT_A"] = 5.050500e+003
|
||||
almanac[41]["Right_Ascen_at_Week"] = 3.897806e+000
|
||||
almanac[41]["Argument_of_Perigee"] = -9.519367e-001
|
||||
almanac[41]["Mean_Anom"] = -4.578920e+000
|
||||
almanac[41]["week"] = 1390
|
||||
almanac[41]["Commit_date"] = "31.01.2003"
|
||||
almanac[41]["Life_dates"] = {}
|
||||
|
||||
almanac[42] = {}
|
||||
almanac[42]["System"] = SAT_SYS_GLONASS
|
||||
almanac[42]["Number"] = 22
|
||||
almanac[42]["Orbital"] = 3
|
||||
almanac[42]["GLONASS_Data"] = {}
|
||||
almanac[42]["GLONASS_Data"]["NKU_Number"] = 791
|
||||
almanac[42]["GLONASS_Data"]["Cosmos_Number"] = 2394
|
||||
almanac[42]["Eccentricity"] = 9.200000e-005
|
||||
almanac[42]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[42]["Orbital_Inclination"] = 1.129742e+000
|
||||
almanac[42]["Rate_of_Right_Ascen"] = -6.740456e-009
|
||||
almanac[42]["SQRT_A"] = 5.050500e+003
|
||||
almanac[42]["Right_Ascen_at_Week"] = 3.897404e+000
|
||||
almanac[42]["Argument_of_Perigee"] = 2.518211e+000
|
||||
almanac[42]["Mean_Anom"] = -2.530167e+000
|
||||
almanac[42]["week"] = 1390
|
||||
almanac[42]["Commit_date"] = "21.01.2003"
|
||||
almanac[42]["Life_dates"] = {}
|
||||
|
||||
almanac[43] = {}
|
||||
almanac[43]["System"] = SAT_SYS_GLONASS
|
||||
almanac[43]["Number"] = 23
|
||||
almanac[43]["Orbital"] = 3
|
||||
almanac[43]["GLONASS_Data"] = {}
|
||||
almanac[43]["GLONASS_Data"]["NKU_Number"] = 714
|
||||
almanac[43]["GLONASS_Data"]["Cosmos_Number"] = 2419
|
||||
almanac[43]["Eccentricity"] = 8.730000e-004
|
||||
almanac[43]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[43]["Orbital_Inclination"] = 1.132105e+000
|
||||
almanac[43]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[43]["SQRT_A"] = 5.050500e+003
|
||||
almanac[43]["Right_Ascen_at_Week"] = 3.883808e+000
|
||||
almanac[43]["Argument_of_Perigee"] = -3.039139e-001
|
||||
almanac[43]["Mean_Anom"] = -5.228304e-001
|
||||
almanac[43]["week"] = 1390
|
||||
almanac[43]["Commit_date"] = "31.08.2006"
|
||||
almanac[43]["Life_dates"] = {}
|
||||
|
||||
almanac[44] = {}
|
||||
almanac[44]["System"] = SAT_SYS_GLONASS
|
||||
almanac[44]["Number"] = 24
|
||||
almanac[44]["Orbital"] = 3
|
||||
almanac[44]["GLONASS_Data"] = {}
|
||||
almanac[44]["GLONASS_Data"]["NKU_Number"] = 713
|
||||
almanac[44]["GLONASS_Data"]["Cosmos_Number"] = 2418
|
||||
almanac[44]["Eccentricity"] = 2.044000e-003
|
||||
almanac[44]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[44]["Orbital_Inclination"] = 1.132430e+000
|
||||
almanac[44]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[44]["SQRT_A"] = 5.050500e+003
|
||||
almanac[44]["Right_Ascen_at_Week"] = 3.883983e+000
|
||||
almanac[44]["Argument_of_Perigee"] = -3.722784e-001
|
||||
almanac[44]["Mean_Anom"] = -1.240457e+000
|
||||
almanac[44]["week"] = 1390
|
||||
almanac[44]["Commit_date"] = "31.08.2006"
|
||||
almanac[44]["Life_dates"] = {}
|
||||
|
||||
--2 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 9-16
|
||||
almanac[45] = {}
|
||||
almanac[45]["System"] = SAT_SYS_GLONASS
|
||||
almanac[45]["Number"] = 9
|
||||
almanac[45]["Orbital"] = 2
|
||||
almanac[45]["GLONASS_Data"] = {}
|
||||
almanac[45]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[45]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[45]["Eccentricity"] = 1.184000e-003
|
||||
almanac[45]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[45]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[45]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[45]["SQRT_A"] = 5.050500e+003
|
||||
almanac[45]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[45]["Argument_of_Perigee"] = 2.88430067
|
||||
almanac[45]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[45]["week"] = 1390
|
||||
almanac[45]["Commit_date"] = "N/A"
|
||||
almanac[45]["Life_dates"] = {}
|
||||
|
||||
almanac[46] = {}
|
||||
almanac[46]["System"] = SAT_SYS_GLONASS
|
||||
almanac[46]["Number"] = 10
|
||||
almanac[46]["Orbital"] = 2
|
||||
almanac[46]["GLONASS_Data"] = {}
|
||||
almanac[46]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[46]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[46]["Eccentricity"] = 1.184000e-003
|
||||
almanac[46]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[46]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[46]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[46]["SQRT_A"] = 5.050500e+003
|
||||
almanac[46]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[46]["Argument_of_Perigee"] = 3.66930067
|
||||
almanac[46]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[46]["week"] = 1390
|
||||
almanac[46]["Commit_date"] = "N/A"
|
||||
almanac[46]["Life_dates"] = {}
|
||||
|
||||
almanac[47] = {}
|
||||
almanac[47]["System"] = SAT_SYS_GLONASS
|
||||
almanac[47]["Number"] = 11
|
||||
almanac[47]["Orbital"] = 2
|
||||
almanac[47]["GLONASS_Data"] = {}
|
||||
almanac[47]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[47]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[47]["Eccentricity"] = 1.184000e-003
|
||||
almanac[47]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[47]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[47]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[47]["SQRT_A"] = 5.050500e+003
|
||||
almanac[47]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[47]["Argument_of_Perigee"] = 4.45430067
|
||||
almanac[47]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[47]["week"] = 1390
|
||||
almanac[47]["Commit_date"] = "N/A"
|
||||
almanac[47]["Life_dates"] = {}
|
||||
|
||||
almanac[48] = {}
|
||||
almanac[48]["System"] = SAT_SYS_GLONASS
|
||||
almanac[48]["Number"] = 12
|
||||
almanac[48]["Orbital"] = 2
|
||||
almanac[48]["GLONASS_Data"] = {}
|
||||
almanac[48]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[48]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[48]["Eccentricity"] = 1.184000e-003
|
||||
almanac[48]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[48]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[48]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[48]["SQRT_A"] = 5.050500e+003
|
||||
almanac[48]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[48]["Argument_of_Perigee"] = 5.23930067
|
||||
almanac[48]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[48]["week"] = 1390
|
||||
almanac[48]["Commit_date"] = "N/A"
|
||||
almanac[48]["Life_dates"] = {}
|
||||
|
||||
almanac[49] = {}
|
||||
almanac[49]["System"] = SAT_SYS_GLONASS
|
||||
almanac[49]["Number"] = 13
|
||||
almanac[49]["Orbital"] = 2
|
||||
almanac[49]["GLONASS_Data"] = {}
|
||||
almanac[49]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[49]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[49]["Eccentricity"] = 1.184000e-003
|
||||
almanac[49]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[49]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[49]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[49]["SQRT_A"] = 5.050500e+003
|
||||
almanac[49]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[49]["Argument_of_Perigee"] = 6.02430067
|
||||
almanac[49]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[49]["week"] = 1390
|
||||
almanac[49]["Commit_date"] = "N/A"
|
||||
almanac[49]["Life_dates"] = {}
|
||||
|
||||
almanac[50] = {}
|
||||
almanac[50]["System"] = SAT_SYS_GLONASS
|
||||
almanac[50]["Number"] = 14
|
||||
almanac[50]["Orbital"] = 2
|
||||
almanac[50]["GLONASS_Data"] = {}
|
||||
almanac[50]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[50]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[50]["Eccentricity"] = 1.184000e-003
|
||||
almanac[50]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[50]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[50]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[50]["SQRT_A"] = 5.050500e+003
|
||||
almanac[50]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[50]["Argument_of_Perigee"] = 0.52930067
|
||||
almanac[50]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[50]["week"] = 1390
|
||||
almanac[50]["Commit_date"] = "N/A"
|
||||
almanac[50]["Life_dates"] = {}
|
||||
|
||||
almanac[51] = {}
|
||||
almanac[51]["System"] = SAT_SYS_GLONASS
|
||||
almanac[51]["Number"] = 15
|
||||
almanac[51]["Orbital"] = 2
|
||||
almanac[51]["GLONASS_Data"] = {}
|
||||
almanac[51]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[51]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[51]["Eccentricity"] = 1.184000e-003
|
||||
almanac[51]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[51]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[51]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[51]["SQRT_A"] = 5.050500e+003
|
||||
almanac[51]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[51]["Argument_of_Perigee"] = 1.31430067
|
||||
almanac[51]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[51]["week"] = 1390
|
||||
almanac[51]["Commit_date"] = "N/A"
|
||||
almanac[51]["Life_dates"] = {}
|
||||
|
||||
almanac[52] = {}
|
||||
almanac[52]["System"] = SAT_SYS_GLONASS
|
||||
almanac[52]["Number"] = 16
|
||||
almanac[52]["Orbital"] = 2
|
||||
almanac[52]["GLONASS_Data"] = {}
|
||||
almanac[52]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[52]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[52]["Eccentricity"] = 1.184000e-003
|
||||
almanac[52]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[52]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[52]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[52]["SQRT_A"] = 5.050500e+003
|
||||
almanac[52]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[52]["Argument_of_Perigee"] = 2.09930067
|
||||
almanac[52]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[52]["week"] = 1390
|
||||
almanac[52]["Commit_date"] = "N/A"
|
||||
almanac[52]["Life_dates"] = {}
|
||||
|
||||
SA_mode = false
|
||||
AS_mode = false
|
||||
@@ -1,52 +0,0 @@
|
||||
---
|
||||
-- RECOVERYTANKER: Uncontrolled_AI
|
||||
--
|
||||
-- Created by Azza276.
|
||||
--
|
||||
-- DateTime: 29/12/2020 20:47
|
||||
--
|
||||
-- Simple Recovery tanker script demonstrating the use of the RECOVERYTANKER.uncontrolledac method.
|
||||
-- or RECOVERYTANKER:SetUseUncontrolledAircraft(). Both are shown below.
|
||||
-- You will require an AI skill S-3B tanker group placed in the mission editor,
|
||||
-- Set to "Takeoff from Ramp" and ensure "Uncontrolled" is ticked.
|
||||
-- Ensure "Late activation" is not ticked.
|
||||
--
|
||||
-- 2 S-3B Tankers will be spawned on the USS Stennis as a visible objects (not late activation) but without crew.
|
||||
-- After 30 seconds, the first S-3B will start up go on station overhead at angels 6 with 274 knots TAS (~250 KIAS).
|
||||
-- After 1 minute, the second S-3B will start up and go on station overhead at angels 12 with 300 knots TAS (~250 KIAS)
|
||||
-- Radio frequencies, callsign are set below and overrule the settings of the AI group.
|
||||
---
|
||||
|
||||
-- S-3B at USS Stennis spawning on deck, Start with Delay in Moose.
|
||||
local tankerStennis=RECOVERYTANKER:New("USS Stennis", "Texaco Group")
|
||||
|
||||
-- Custom settings for radio frequency, TACAN and callsign.
|
||||
tankerStennis:SetRadio(261)
|
||||
tankerStennis:SetTACAN(37, "SHL")
|
||||
tankerStennis:SetCallsign(CALLSIGN.Tanker.Shell, 3)
|
||||
|
||||
--tankerStennis:SetTakeoffCold() --This is not required as they will always start cold from uncontrolled state.
|
||||
|
||||
--RECOVERYTANKER.uncontrolledac if true, use an uncontrolled tanker group already present in the mission.
|
||||
tankerStennis.uncontrolledac = true
|
||||
|
||||
-- Start recovery tanker.
|
||||
-- NOTE: Delay to show Aircraft visible on deck then starts later (30 seconds after mission start).
|
||||
tankerStennis:__Start(30)
|
||||
|
||||
|
||||
|
||||
-- S-3B at USS Stennis spawning on deck, Start with Delay in Mission Editor Trigger.
|
||||
tankerStennis2=RECOVERYTANKER:New( "USS Stennis", "Texaco Group-1")
|
||||
tankerStennis2:SetRadio(271)
|
||||
tankerStennis2:SetTACAN(38, "SHE")
|
||||
tankerStennis2:SetCallsign(3, 2) --First parameter is Callsign name (1=Texaco, 2=Arco, 3=Shell)
|
||||
tankerStennis2:SetAltitude(12000) --Sets Orbit Altitude
|
||||
tankerStennis2:SetSpeed(300) --Sets speed to 300 knots TAS (~250 KIAS at 12000ft)
|
||||
|
||||
--RECOVERYTANKER:SetUseUncontrolledAircraft() to use an uncontrolled tanker group already present in the mission.
|
||||
tankerStennis2:SetUseUncontrolledAircraft()
|
||||
|
||||
-- tankerStennis2:Start()
|
||||
-- The above without "--" is loaded to the Mission editor trigger "Do Script" action after 60 seconds condition.
|
||||
-- NOTE: Delay to show Aircraft visible on deck then starts later (60 seconds after mission start)..
|
||||
Binary file not shown.
@@ -1,189 +0,0 @@
|
||||
-- View scripts
|
||||
-- Copyright (C) 2004, Eagle Dynamics.
|
||||
DisableCombatViews = false -- F5 & Ctrl-F5
|
||||
ExternalObjectsLockDistance = 10000.0
|
||||
ShowTargetInfo = false
|
||||
CameraTerrainRestriction = true
|
||||
hAngleRearDefault = 180
|
||||
vAngleRearDefault = -8.0
|
||||
vAngleRearMin = -90 -- -8.0
|
||||
vAngleRearMax = 90.0
|
||||
|
||||
dbg_shell = "weapons.shells.PKT_7_62_T" -- 23mm shell
|
||||
--dbg_shell = "weapons.shells.2A42_30_AP"
|
||||
--dbg_shell = "weapons.nurs.WGr21"
|
||||
--dbg_shell = "weapons.shells.2A64_152" -- 152mm shell
|
||||
dbg_shell_v0 = -1 -- Muzzle speed m/s (-1 - speed from shall database)
|
||||
dbg_shell_fire_rate = 120
|
||||
--reformatted per-unit data to be mod system friendly
|
||||
--this file is no longer should be edited for adding new flyable aircraft , DCS automatically check core database (i.e. where you define your aircraft in aircraft table just define ViewSettings and SnapViews tables)
|
||||
|
||||
function default_fighter_player(t)
|
||||
local res = {
|
||||
CameraViewAngleLimits = {20.000000,140.000000},
|
||||
CameraAngleRestriction = {false ,90.000000,0.500000},
|
||||
EyePoint = {0.05 ,0.000000 ,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.4500000},y ={-0.300000,0.100000},z = {-0.220000,0.220000},roll = 90.000000},
|
||||
Allow360rotation = false,
|
||||
CameraAngleLimits = {200,-80.000000,110.000000},
|
||||
ShoulderSize = 0.2, -- move body when azimuth value more then 90 degrees
|
||||
}
|
||||
if t then
|
||||
for i,o in pairs(t) do
|
||||
res[i] = o
|
||||
end
|
||||
end
|
||||
return res
|
||||
end
|
||||
|
||||
function fulcrum()
|
||||
return {
|
||||
Cockpit = {
|
||||
default_fighter_player({CockpitLocalPoint = {4.71,1.28,0.000000}})
|
||||
},
|
||||
Chase = {
|
||||
LocalPoint = {1.220000,3.750000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-15.080000,6.350000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
end
|
||||
|
||||
ViewSettings = {}
|
||||
ViewSettings["A-10A"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.600000},
|
||||
y = {-0.300000,0.100000},
|
||||
z = {-0.250000,0.250000},
|
||||
roll = 90.000000}}),
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {0.600000,3.682000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-27.000000,12.000000,0.000000},
|
||||
AnglesDefault = {0.000000,-12.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["A-10C"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.050000,0.600000},
|
||||
y = {-0.300000,0.100000},
|
||||
z = {-0.250000,0.250000},
|
||||
roll = 90.000000}}),
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {0.600000,3.682000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-27.000000,12.000000,0.000000},
|
||||
AnglesDefault = {0.000000,-12.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["F-15C"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {6.210000,1.204000,0.000000}})-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {2.510000,3.604000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-13.790000,6.204000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Ka-50"] = {
|
||||
Cockpit = {
|
||||
[1] = {-- player slot 1
|
||||
CockpitLocalPoint = {3.188000,0.390000,0.000000},
|
||||
CameraViewAngleLimits = {20.000000,120.000000},
|
||||
CameraAngleRestriction = {false,60.000000,0.400000},
|
||||
CameraAngleLimits = {140.000000,-65.000000,90.000000},
|
||||
EyePoint = {0.090000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.020000,0.350000},y ={-0.150000,0.165000},z = {-0.170000,0.170000},roll = 90.000000},
|
||||
},
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.512000,2.790000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.812000,5.390000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["MiG-29A"] = fulcrum()
|
||||
ViewSettings["MiG-29G"] = fulcrum()
|
||||
ViewSettings["MiG-29S"] = fulcrum()
|
||||
|
||||
ViewSettings["Su-25"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {3.352000,0.506000,0.000000}}),-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.348000,2.906000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.648001,5.506000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-25T"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {3.406000,0.466000,0.000000}}),-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {-0.294000,2.866000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-16.594000,5.466000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-25TM"] = {
|
||||
Cockpit = {
|
||||
[1] = {-- player slot 1
|
||||
CockpitLocalPoint = {4.000000,1.000000,0.000000},
|
||||
CameraViewAngleLimits = {20.000000,140.000000},
|
||||
CameraAngleRestriction = {true,90.000000,0.400000},
|
||||
CameraAngleLimits = {160.000000,-70.000000,90.000000},
|
||||
EyePoint = {0.000000,0.000000,0.000000},
|
||||
limits_6DOF = {x = {-0.200000,0.200000},y ={-0.200000,0.200000},z = {-0.200000,0.200000},roll = 60.000000},
|
||||
},
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {4.000000,2.000000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {4.000000,2.000000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
ViewSettings["Su-27"] = {
|
||||
Cockpit = {
|
||||
[1] = default_fighter_player({CockpitLocalPoint = {7.959000,1.419000,0.000000}})-- player slot 1
|
||||
}, -- Cockpit
|
||||
Chase = {
|
||||
LocalPoint = {4.259000,3.819000,0.000000},
|
||||
AnglesDefault = {180.000000,-8.000000},
|
||||
}, -- Chase
|
||||
Arcade = {
|
||||
LocalPoint = {-12.041000,6.419000,0.000000},
|
||||
AnglesDefault = {0.000000,-8.000000},
|
||||
}, -- Arcade
|
||||
}
|
||||
|
||||
ViewSettings["Su-33"] = ViewSettings["Su-27"]
|
||||
File diff suppressed because it is too large
Load Diff
@@ -1,128 +0,0 @@
|
||||
-- View scripts
|
||||
-- Copyright (C) 2004, Eagle Dynamics.
|
||||
|
||||
CockpitMouse = true --false
|
||||
CockpitMouseSpeedSlow = 1.0
|
||||
CockpitMouseSpeedNormal = 10.0
|
||||
CockpitMouseSpeedFast = 20.0
|
||||
CockpitKeyboardAccelerationSlow = 5.0
|
||||
CockpitKeyboardAccelerationNormal = 30.0
|
||||
CockpitKeyboardAccelerationFast = 80.0
|
||||
CockpitKeyboardZoomAcceleration = 300.0
|
||||
DisableSnapViewsSaving = false
|
||||
UseDefaultSnapViews = true
|
||||
CockpitPanStepHor = 45.0
|
||||
CockpitPanStepVert = 30.0
|
||||
CockpitNyMove = true
|
||||
|
||||
CockpitHAngleAccelerateTimeMax = 0.15
|
||||
CockpitVAngleAccelerateTimeMax = 0.15
|
||||
CockpitZoomAccelerateTimeMax = 0.2
|
||||
|
||||
function NaturalHeadMoving(tang, roll, omz)
|
||||
local r = roll
|
||||
if r > 90.0 then
|
||||
r = 180.0 - r
|
||||
elseif roll < -90.0 then
|
||||
r = -180.0 - r
|
||||
end
|
||||
local hAngle = -0.25 * r
|
||||
local vAngle = math.min(math.max(0.0, 0.4 * tang + 45.0 * omz), 90.0)
|
||||
return hAngle, vAngle
|
||||
end
|
||||
|
||||
ExternalMouse = true
|
||||
ExternalMouseSpeedSlow = 1.0
|
||||
ExternalMouseSpeedNormal = 5.0
|
||||
ExternalMouseSpeedFast = 20.0
|
||||
ExternalViewAngleMin = 3.0
|
||||
ExternalViewAngleMax = 140.0
|
||||
ExternalViewAngleDefault = 60.0
|
||||
ExternalKeyboardZoomAcceleration = 30.0
|
||||
ExternalKeyboardZoomAccelerateTimeMax = 1.0
|
||||
ExplosionExpoTime = 4.0
|
||||
ExternalKeyboardAccelerationSlow = 1.0
|
||||
ExternalKeyboardAccelerationNormal = 10.0
|
||||
ExternalKeyboardAccelerationFast = 30.0
|
||||
ExternalHAngleAccelerateTimeMax = 3.0
|
||||
ExternalVAngleAccelerateTimeMax = 3.0
|
||||
ExternalDistAccelerateTimeMax = 3.0
|
||||
ExternalHAngleLocalAccelerateTimeMax = 3.0
|
||||
ExternalVAngleLocalAccelerateTimeMax = 3.0
|
||||
ExternalAngleNormalDiscreteStep = 15.0/ExternalKeyboardAccelerationNormal -- When 'S' is pressed only
|
||||
ChaseCameraNyMove = true
|
||||
FreeCameraAngleIncrement = 3.0
|
||||
FreeCameraDistanceIncrement = 200.0
|
||||
FreeCameraLeftRightIncrement = 2.0
|
||||
FreeCameraAltitudeIncrement = 2.0
|
||||
FreeCameraScalarSpeedAcceleration = 0.1
|
||||
xMinMap = -300000
|
||||
xMaxMap = 500000
|
||||
yMinMap = -400000
|
||||
yMaxMap = 200000
|
||||
dxMap = 150000
|
||||
dyMap = 100000
|
||||
|
||||
head_roll_shaking = true
|
||||
head_roll_shaking_max = 30.0
|
||||
head_roll_shaking_compensation_gain = 0.3
|
||||
|
||||
-- CameraJiggle() and CameraFloat() functions make camera position
|
||||
-- dependent on FPS so be careful in using the Shift-J command with tracks, please.
|
||||
-- uncomment to use custom jiggle functions
|
||||
--[[
|
||||
function CameraJiggle(t,rnd1,rnd2,rnd3)
|
||||
local rotX, rotY, rotZ
|
||||
rotX = 0.05 * rnd1 * math.sin(37.0 * (t - 0.0))
|
||||
rotY = 0.05 * rnd2 * math.sin(41.0 * (t - 1.0))
|
||||
rotZ = 0.05 * rnd3 * math.sin(53.0 * (t - 2.0))
|
||||
return rotX, rotY, rotZ
|
||||
end
|
||||
|
||||
function CameraFloat(t)
|
||||
local dX, dY, dZ
|
||||
dX = 0.61 * math.sin(0.7 * t) + 0.047 * math.sin(1.6 * t);
|
||||
dY = 0.43 * math.sin(0.6 * t) + 0.067 * math.sin(1.7 * t);
|
||||
dZ = 0.53 * math.sin(1.0 * t) + 0.083 * math.sin(1.9 * t);
|
||||
return dX, dY, dZ
|
||||
end
|
||||
--]]
|
||||
--Debug keys
|
||||
|
||||
DEBUG_TEXT = 1
|
||||
DEBUG_GEOMETRY = 2
|
||||
|
||||
debug_keys = {
|
||||
[DEBUG_TEXT] = 1,
|
||||
[DEBUG_GEOMETRY] = 1
|
||||
}
|
||||
|
||||
function onDebugCommand(command)
|
||||
if command == 10000 then
|
||||
if debug_keys[DEBUG_TEXT] ~= 0 or debug_keys[DEBUG_GEOMETRY] ~= 0 then
|
||||
debug_keys[DEBUG_GEOMETRY] = 0
|
||||
debug_keys[DEBUG_TEXT] = 0
|
||||
else
|
||||
debug_keys[DEBUG_GEOMETRY] = 1
|
||||
debug_keys[DEBUG_TEXT] = 1
|
||||
end
|
||||
elseif command == 10001 then
|
||||
if debug_keys[DEBUG_TEXT] ~= 0 then
|
||||
debug_keys[DEBUG_TEXT] = 0
|
||||
else
|
||||
debug_keys[DEBUG_TEXT] = 1
|
||||
end
|
||||
elseif command == 10002 then
|
||||
if debug_keys[DEBUG_GEOMETRY] ~= 0 then
|
||||
debug_keys[DEBUG_GEOMETRY] = 0
|
||||
else
|
||||
debug_keys[DEBUG_GEOMETRY] = 1
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
-- gain values for TrackIR , to unify responce on diffrent types of aircraft
|
||||
TrackIR_gain_x = -0.6
|
||||
TrackIR_gain_y = 0.3
|
||||
TrackIR_gain_z = -0.25
|
||||
TrackIR_gain_roll = -90
|
||||
@@ -1,880 +0,0 @@
|
||||
SAT_SYS_GLONASS = 0
|
||||
SAT_SYS_GPS = 1
|
||||
|
||||
almanac = {}
|
||||
--GPS
|
||||
almanac[0] = {}
|
||||
almanac[0]["System"] = SAT_SYS_GPS
|
||||
almanac[0]["Number"] = 1
|
||||
almanac[0]["Orbital"] = "F"
|
||||
almanac[0]["Eccentricity"] = 6.294000e-003
|
||||
almanac[0]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[0]["Orbital_Inclination"] = 9.885676e-001
|
||||
almanac[0]["Rate_of_Right_Ascen"] = -7.862702e-009
|
||||
almanac[0]["SQRT_A"] = 5.153700e+003
|
||||
almanac[0]["Right_Ascen_at_Week"] = 8.096750e-001
|
||||
almanac[0]["Argument_of_Perigee"] = -1.777773e+000
|
||||
almanac[0]["Mean_Anom"] = -5.315745e-001
|
||||
almanac[0]["week"] = 1390
|
||||
|
||||
almanac[1] = {}
|
||||
almanac[1]["System"] = SAT_SYS_GPS
|
||||
almanac[1]["Number"] = 2
|
||||
almanac[1]["Orbital"] = "C"
|
||||
almanac[1]["Eccentricity"] = 8.794000e-003
|
||||
almanac[1]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[1]["Orbital_Inclination"] = 9.487811e-001
|
||||
almanac[1]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[1]["SQRT_A"] = 5.153700e+003
|
||||
almanac[1]["Right_Ascen_at_Week"] = -1.329172e+000
|
||||
almanac[1]["Argument_of_Perigee"] = 2.138637e+000
|
||||
almanac[1]["Mean_Anom"] = 7.311702e-001
|
||||
almanac[1]["week"] = 1390
|
||||
|
||||
almanac[2] = {}
|
||||
almanac[2]["System"] = SAT_SYS_GPS
|
||||
almanac[2]["Number"] = 3
|
||||
almanac[2]["Orbital"] = "F"
|
||||
almanac[2]["Eccentricity"] = 8.424000e-003
|
||||
almanac[2]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[2]["Orbital_Inclination"] = 9.262804e-001
|
||||
almanac[2]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[2]["SQRT_A"] = 5.153600e+003
|
||||
almanac[2]["Right_Ascen_at_Week"] = -2.341514e+000
|
||||
almanac[2]["Argument_of_Perigee"] = 6.749357e-001
|
||||
almanac[2]["Mean_Anom"] = -2.296153e-001
|
||||
almanac[2]["week"] = 1389
|
||||
|
||||
almanac[3] = {}
|
||||
almanac[3]["System"] = SAT_SYS_GPS
|
||||
almanac[3]["Number"] = 4
|
||||
almanac[3]["Orbital"] = "D"
|
||||
almanac[3]["Eccentricity"] = 7.413000e-003
|
||||
almanac[3]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[3]["Orbital_Inclination"] = 9.482889e-001
|
||||
almanac[3]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[3]["SQRT_A"] = 5.153600e+003
|
||||
almanac[3]["Right_Ascen_at_Week"] = -1.309589e+000
|
||||
almanac[3]["Argument_of_Perigee"] = 1.623504e-001
|
||||
almanac[3]["Mean_Anom"] = -3.022943e+000
|
||||
almanac[3]["week"] = 1390
|
||||
|
||||
almanac[4] = {}
|
||||
almanac[4]["System"] = SAT_SYS_GPS
|
||||
almanac[4]["Number"] = 5
|
||||
almanac[4]["Orbital"] = "B"
|
||||
almanac[4]["Eccentricity"] = 7.432000e-003
|
||||
almanac[4]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[4]["Orbital_Inclination"] = 9.387437e-001
|
||||
almanac[4]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[4]["SQRT_A"] = 5.153700e+003
|
||||
almanac[4]["Right_Ascen_at_Week"] = 2.779487e+000
|
||||
almanac[4]["Argument_of_Perigee"] = 1.099033e+000
|
||||
almanac[4]["Mean_Anom"] = 2.970984e+000
|
||||
almanac[4]["week"] = 1390
|
||||
|
||||
almanac[5] = {}
|
||||
almanac[5]["System"] = SAT_SYS_GPS
|
||||
almanac[5]["Number"] = 6
|
||||
almanac[5]["Orbital"] = "C"
|
||||
almanac[5]["Eccentricity"] = 6.020000e-003
|
||||
almanac[5]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[5]["Orbital_Inclination"] = 9.337591e-001
|
||||
almanac[5]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[5]["SQRT_A"] = 5.153600e+003
|
||||
almanac[5]["Right_Ascen_at_Week"] = -2.407627e+000
|
||||
almanac[5]["Argument_of_Perigee"] = -1.788263e+000
|
||||
almanac[5]["Mean_Anom"] = -2.149877e+000
|
||||
almanac[5]["week"] = 1390
|
||||
|
||||
almanac[6] = {}
|
||||
almanac[6]["System"] = SAT_SYS_GPS
|
||||
almanac[6]["Number"] = 7
|
||||
almanac[6]["Orbital"] = "C"
|
||||
almanac[6]["Eccentricity"] = 1.052400e-002
|
||||
almanac[6]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[6]["Orbital_Inclination"] = 9.353229e-001
|
||||
almanac[6]["Rate_of_Right_Ascen"] = -8.080868e-009
|
||||
almanac[6]["SQRT_A"] = 5.153700e+003
|
||||
almanac[6]["Right_Ascen_at_Week"] = -2.433580e+000
|
||||
almanac[6]["Argument_of_Perigee"] = -1.767301e+000
|
||||
almanac[6]["Mean_Anom"] = -3.141503e+000
|
||||
almanac[6]["week"] = 1390
|
||||
|
||||
almanac[7] = {}
|
||||
almanac[7]["System"] = SAT_SYS_GPS
|
||||
almanac[7]["Number"] = 8
|
||||
almanac[7]["Orbital"] = "A"
|
||||
almanac[7]["Eccentricity"] = 9.822000e-003
|
||||
almanac[7]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[7]["Orbital_Inclination"] = 9.741390e-001
|
||||
almanac[7]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[7]["SQRT_A"] = 5.153600e+003
|
||||
almanac[7]["Right_Ascen_at_Week"] = 1.857849e+000
|
||||
almanac[7]["Argument_of_Perigee"] = 2.674034e+000
|
||||
almanac[7]["Mean_Anom"] = -2.009745e+000
|
||||
almanac[7]["week"] = 1390
|
||||
|
||||
almanac[8] = {}
|
||||
almanac[8]["System"] = SAT_SYS_GPS
|
||||
almanac[8]["Number"] = 9
|
||||
almanac[8]["Orbital"] = "A"
|
||||
almanac[8]["Eccentricity"] = 1.839300e-002
|
||||
almanac[8]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[8]["Orbital_Inclination"] = 9.617541e-001
|
||||
almanac[8]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[8]["SQRT_A"] = 5.153600e+003
|
||||
almanac[8]["Right_Ascen_at_Week"] = 1.777005e+000
|
||||
almanac[8]["Argument_of_Perigee"] = 1.274962e+000
|
||||
almanac[8]["Mean_Anom"] = -2.349578e+000
|
||||
almanac[8]["week"] = 1390
|
||||
|
||||
almanac[9] = {}
|
||||
almanac[9]["System"] = SAT_SYS_GPS
|
||||
almanac[9]["Number"] = 10
|
||||
almanac[9]["Orbital"] = "E"
|
||||
almanac[9]["Eccentricity"] = 7.061000e-003
|
||||
almanac[9]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[9]["Orbital_Inclination"] = 9.728876e-001
|
||||
almanac[9]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[9]["SQRT_A"] = 5.153600e+003
|
||||
almanac[9]["Right_Ascen_at_Week"] = -2.563014e-001
|
||||
almanac[9]["Argument_of_Perigee"] = 4.377980e-001
|
||||
almanac[9]["Mean_Anom"] = 1.210716e+000
|
||||
almanac[9]["week"] = 1390
|
||||
|
||||
almanac[10] = {}
|
||||
almanac[10]["System"] = SAT_SYS_GPS
|
||||
almanac[10]["Number"] = 11
|
||||
almanac[10]["Orbital"] = "D"
|
||||
almanac[10]["Eccentricity"] = 5.744000e-003
|
||||
almanac[10]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[10]["Orbital_Inclination"] = 8.959309e-001
|
||||
almanac[10]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[10]["SQRT_A"] = 5.153600e+003
|
||||
almanac[10]["Right_Ascen_at_Week"] = -1.478816e+000
|
||||
almanac[10]["Argument_of_Perigee"] = 3.750011e-001
|
||||
almanac[10]["Mean_Anom"] = -1.522048e+000
|
||||
almanac[10]["week"] = 1390
|
||||
|
||||
almanac[11] = {}
|
||||
almanac[11]["System"] = SAT_SYS_GPS
|
||||
almanac[11]["Number"] = 13
|
||||
almanac[11]["Orbital"] = "F"
|
||||
almanac[11]["Eccentricity"] = 3.088000e-003
|
||||
almanac[11]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[11]["Orbital_Inclination"] = 9.927564e-001
|
||||
almanac[11]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[11]["SQRT_A"] = 5.153700e+003
|
||||
almanac[11]["Right_Ascen_at_Week"] = 7.956600e-001
|
||||
almanac[11]["Argument_of_Perigee"] = 1.279395e+000
|
||||
almanac[11]["Mean_Anom"] = 1.004349e+000
|
||||
almanac[11]["week"] = 1390
|
||||
|
||||
almanac[12] = {}
|
||||
almanac[12]["System"] = SAT_SYS_GPS
|
||||
almanac[12]["Number"] = 14
|
||||
almanac[12]["Orbital"] = "F"
|
||||
almanac[12]["Eccentricity"] = 2.591000e-003
|
||||
almanac[12]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[12]["Orbital_Inclination"] = 9.868729e-001
|
||||
almanac[12]["Rate_of_Right_Ascen"] = -7.885391e-009
|
||||
almanac[12]["SQRT_A"] = 5.153600e+003
|
||||
almanac[12]["Right_Ascen_at_Week"] = 7.819592e-001
|
||||
almanac[12]["Argument_of_Perigee"] = -2.158621e+000
|
||||
almanac[12]["Mean_Anom"] = 5.412611e-001
|
||||
almanac[12]["week"] = 1390
|
||||
|
||||
almanac[13] = {}
|
||||
almanac[13]["System"] = SAT_SYS_GPS
|
||||
almanac[13]["Number"] = 15
|
||||
almanac[13]["Orbital"] = "D"
|
||||
almanac[13]["Eccentricity"] = 9.828000e-003
|
||||
almanac[13]["Time_of_Applicability"] = 3.194880e+005
|
||||
almanac[13]["Orbital_Inclination"] = 9.554204e-001
|
||||
almanac[13]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[13]["SQRT_A"] = 5.153600e+003
|
||||
almanac[13]["Right_Ascen_at_Week"] = -1.123869e+000
|
||||
almanac[13]["Argument_of_Perigee"] = 2.690266e+000
|
||||
almanac[13]["Mean_Anom"] = 2.220476e+000
|
||||
almanac[13]["week"] = 1389
|
||||
|
||||
almanac[14] = {}
|
||||
almanac[14]["System"] = SAT_SYS_GPS
|
||||
almanac[14]["Number"] = 16
|
||||
almanac[14]["Orbital"] = "B"
|
||||
almanac[14]["Eccentricity"] = 3.494000e-003
|
||||
almanac[14]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[14]["Orbital_Inclination"] = 9.629340e-001
|
||||
almanac[14]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[14]["SQRT_A"] = 5.153700e+003
|
||||
almanac[14]["Right_Ascen_at_Week"] = 2.873124e+000
|
||||
almanac[14]["Argument_of_Perigee"] = -7.819243e-001
|
||||
almanac[14]["Mean_Anom"] = 2.623629e+000
|
||||
almanac[14]["week"] = 1390
|
||||
|
||||
almanac[15] = {}
|
||||
almanac[15]["System"] = SAT_SYS_GPS
|
||||
almanac[15]["Number"] = 17
|
||||
almanac[15]["Orbital"] = "C"
|
||||
almanac[15]["Eccentricity"] = 2.141000e-003
|
||||
almanac[15]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[15]["Orbital_Inclination"] = 9.601170e-001
|
||||
almanac[15]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[15]["SQRT_A"] = 5.153700e+003
|
||||
almanac[15]["Right_Ascen_at_Week"] = -2.371499e+000
|
||||
almanac[15]["Argument_of_Perigee"] = 3.087694e+000
|
||||
almanac[15]["Mean_Anom"] = 1.611217e+000
|
||||
almanac[15]["week"] = 1390
|
||||
|
||||
almanac[16] = {}
|
||||
almanac[16]["System"] = SAT_SYS_GPS
|
||||
almanac[16]["Number"] = 18
|
||||
almanac[16]["Orbital"] = "E"
|
||||
almanac[16]["Eccentricity"] = 7.636000e-003
|
||||
almanac[16]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[16]["Orbital_Inclination"] = 9.569597e-001
|
||||
almanac[16]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[16]["SQRT_A"] = 5.153700e+003
|
||||
almanac[16]["Right_Ascen_at_Week"] = -2.359858e-001
|
||||
almanac[16]["Argument_of_Perigee"] = -2.649216e+000
|
||||
almanac[16]["Mean_Anom"] = 2.675029e+000
|
||||
almanac[16]["week"] = 1390
|
||||
|
||||
almanac[17] = {}
|
||||
almanac[17]["System"] = SAT_SYS_GPS
|
||||
almanac[17]["Number"] = 19
|
||||
almanac[17]["Orbital"] = "C"
|
||||
almanac[17]["Eccentricity"] = 3.602000e-003
|
||||
almanac[17]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[17]["Orbital_Inclination"] = 9.580209e-001
|
||||
almanac[17]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[17]["SQRT_A"] = 5.153600e+003
|
||||
almanac[17]["Right_Ascen_at_Week"] = -2.312385e+000
|
||||
almanac[17]["Argument_of_Perigee"] = -1.161079e+000
|
||||
almanac[17]["Mean_Anom"] = 1.310619e+000
|
||||
almanac[17]["week"] = 1390
|
||||
|
||||
almanac[18] = {}
|
||||
almanac[18]["System"] = SAT_SYS_GPS
|
||||
almanac[18]["Number"] = 20
|
||||
almanac[18]["Orbital"] = "E"
|
||||
almanac[18]["Eccentricity"] = 2.796000e-003
|
||||
almanac[18]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[18]["Orbital_Inclination"] = 9.564693e-001
|
||||
almanac[18]["Rate_of_Right_Ascen"] = -7.908080e-009
|
||||
almanac[18]["SQRT_A"] = 5.153600e+003
|
||||
almanac[18]["Right_Ascen_at_Week"] = -2.889565e-001
|
||||
almanac[18]["Argument_of_Perigee"] = 1.379612e+000
|
||||
almanac[18]["Mean_Anom"] = 2.461750e+000
|
||||
almanac[18]["week"] = 1390
|
||||
|
||||
almanac[19] = {}
|
||||
almanac[19]["System"] = SAT_SYS_GPS
|
||||
almanac[19]["Number"] = 21
|
||||
almanac[19]["Orbital"] = "D"
|
||||
almanac[19]["Eccentricity"] = 1.162900e-002
|
||||
almanac[19]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[19]["Orbital_Inclination"] = 9.418592e-001
|
||||
almanac[19]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[19]["SQRT_A"] = 5.153600e+003
|
||||
almanac[19]["Right_Ascen_at_Week"] = -1.289972e+000
|
||||
almanac[19]["Argument_of_Perigee"] = -2.923686e+000
|
||||
almanac[19]["Mean_Anom"] = -2.349194e+000
|
||||
almanac[19]["week"] = 1390
|
||||
|
||||
almanac[20] = {}
|
||||
almanac[20]["System"] = SAT_SYS_GPS
|
||||
almanac[20]["Number"] = 22
|
||||
almanac[20]["Orbital"] = "E"
|
||||
almanac[20]["Eccentricity"] = 4.893000e-003
|
||||
almanac[20]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[20]["Orbital_Inclination"] = 9.545093e-001
|
||||
almanac[20]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[20]["SQRT_A"] = 5.153600e+003
|
||||
almanac[20]["Right_Ascen_at_Week"] = -2.280969e-001
|
||||
almanac[20]["Argument_of_Perigee"] = -1.674502e+000
|
||||
almanac[20]["Mean_Anom"] = 1.106852e+000
|
||||
almanac[20]["week"] = 1390
|
||||
|
||||
almanac[21] = {}
|
||||
almanac[21]["System"] = SAT_SYS_GPS
|
||||
almanac[21]["Number"] = 23
|
||||
almanac[21]["Orbital"] = "F"
|
||||
almanac[21]["Eccentricity"] = 4.822000e-003
|
||||
almanac[21]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[21]["Orbital_Inclination"] = 9.691247e-001
|
||||
almanac[21]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[21]["SQRT_A"] = 5.153700e+003
|
||||
almanac[21]["Right_Ascen_at_Week"] = 7.667399e-001
|
||||
almanac[21]["Argument_of_Perigee"] = 2.497634e+000
|
||||
almanac[21]["Mean_Anom"] = 3.184700e-001
|
||||
almanac[21]["week"] = 1390
|
||||
|
||||
almanac[22] = {}
|
||||
almanac[22]["System"] = SAT_SYS_GPS
|
||||
almanac[22]["Number"] = 24
|
||||
almanac[22]["Orbital"] = "D"
|
||||
almanac[22]["Eccentricity"] = 9.277000e-003
|
||||
almanac[22]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[22]["Orbital_Inclination"] = 9.585183e-001
|
||||
almanac[22]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[22]["SQRT_A"] = 5.153900e+003
|
||||
almanac[22]["Right_Ascen_at_Week"] = -1.274840e+000
|
||||
almanac[22]["Argument_of_Perigee"] = -8.815651e-001
|
||||
almanac[22]["Mean_Anom"] = -1.695551e+000
|
||||
almanac[22]["week"] = 1390
|
||||
|
||||
almanac[23] = {}
|
||||
almanac[23]["System"] = SAT_SYS_GPS
|
||||
almanac[23]["Number"] = 25
|
||||
almanac[23]["Orbital"] = "A"
|
||||
almanac[23]["Eccentricity"] = 1.257400e-002
|
||||
almanac[23]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[23]["Orbital_Inclination"] = 9.551027e-001
|
||||
almanac[23]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[23]["SQRT_A"] = 5.153600e+003
|
||||
almanac[23]["Right_Ascen_at_Week"] = 1.721853e+000
|
||||
almanac[23]["Argument_of_Perigee"] = -1.329870e+000
|
||||
almanac[23]["Mean_Anom"] = -1.769623e+000
|
||||
almanac[23]["week"] = 1390
|
||||
|
||||
almanac[24] = {}
|
||||
almanac[24]["System"] = SAT_SYS_GPS
|
||||
almanac[24]["Number"] = 26
|
||||
almanac[24]["Orbital"] = "F"
|
||||
almanac[24]["Eccentricity"] = 1.745700e-002
|
||||
almanac[24]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[24]["Orbital_Inclination"] = 9.908749e-001
|
||||
almanac[24]["Rate_of_Right_Ascen"] = -7.840012e-009
|
||||
almanac[24]["SQRT_A"] = 5.153700e+003
|
||||
almanac[24]["Right_Ascen_at_Week"] = 7.961836e-001
|
||||
almanac[24]["Argument_of_Perigee"] = 8.161502e-001
|
||||
almanac[24]["Mean_Anom"] = -5.841961e-001
|
||||
almanac[24]["week"] = 1390
|
||||
|
||||
almanac[25] = {}
|
||||
almanac[25]["System"] = SAT_SYS_GPS
|
||||
almanac[25]["Number"] = 27
|
||||
almanac[25]["Orbital"] = "A"
|
||||
almanac[25]["Eccentricity"] = 1.991000e-002
|
||||
almanac[25]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[25]["Orbital_Inclination"] = 9.596563e-001
|
||||
almanac[25]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[25]["SQRT_A"] = 5.153600e+003
|
||||
almanac[25]["Right_Ascen_at_Week"] = 1.754124e+000
|
||||
almanac[25]["Argument_of_Perigee"] = -1.900854e+000
|
||||
almanac[25]["Mean_Anom"] = 3.046487e+000
|
||||
almanac[25]["week"] = 1390
|
||||
|
||||
almanac[26] = {}
|
||||
almanac[26]["System"] = SAT_SYS_GPS
|
||||
almanac[26]["Number"] = 28
|
||||
almanac[26]["Orbital"] = "B"
|
||||
almanac[26]["Eccentricity"] = 1.162800e-002
|
||||
almanac[26]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[26]["Orbital_Inclination"] = 9.610106e-001
|
||||
almanac[26]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[26]["SQRT_A"] = 5.153600e+003
|
||||
almanac[26]["Right_Ascen_at_Week"] = 2.882583e+000
|
||||
almanac[26]["Argument_of_Perigee"] = -2.242868e+000
|
||||
almanac[26]["Mean_Anom"] = 1.860642e+000
|
||||
almanac[26]["week"] = 1390
|
||||
|
||||
almanac[27] = {}
|
||||
almanac[27]["System"] = SAT_SYS_GPS
|
||||
almanac[27]["Number"] = 29
|
||||
almanac[27]["Orbital"] = "F"
|
||||
almanac[27]["Eccentricity"] = 9.462000e-003
|
||||
almanac[27]["Time_of_Applicability"] = 1.474560e+005
|
||||
almanac[27]["Orbital_Inclination"] = 9.874838e-001
|
||||
almanac[27]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[27]["SQRT_A"] = 5.153700e+003
|
||||
almanac[27]["Right_Ascen_at_Week"] = 7.647503e-001
|
||||
almanac[27]["Argument_of_Perigee"] = -8.614589e-001
|
||||
almanac[27]["Mean_Anom"] = -4.488983e-001
|
||||
almanac[27]["week"] = 1390
|
||||
|
||||
almanac[28] = {}
|
||||
almanac[28]["System"] = SAT_SYS_GPS
|
||||
almanac[28]["Number"] = 30
|
||||
almanac[28]["Orbital"] = "B"
|
||||
almanac[28]["Eccentricity"] = 9.296000e-003
|
||||
almanac[28]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[28]["Orbital_Inclination"] = 9.452992e-001
|
||||
almanac[28]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[28]["SQRT_A"] = 5.153600e+003
|
||||
almanac[28]["Right_Ascen_at_Week"] = 2.826698e+000
|
||||
almanac[28]["Argument_of_Perigee"] = 1.306413e+000
|
||||
almanac[28]["Mean_Anom"] = 2.148725e+000
|
||||
almanac[28]["week"] = 1390
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
|
||||
--GLONASS
|
||||
--1 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 1-8
|
||||
almanac[29] = {}
|
||||
almanac[29]["System"] = SAT_SYS_GLONASS
|
||||
almanac[29]["Number"] = 1
|
||||
almanac[29]["Orbital"] = 1
|
||||
almanac[29]["GLONASS_Data"] = {}
|
||||
almanac[29]["GLONASS_Data"]["NKU_Number"] = 796
|
||||
almanac[29]["GLONASS_Data"]["Cosmos_Number"] = 2411
|
||||
almanac[29]["Eccentricity"] = 1.184000e-003
|
||||
almanac[29]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[29]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[29]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[29]["SQRT_A"] = 5.050500e+003
|
||||
almanac[29]["Right_Ascen_at_Week"] = 5.979807e+000
|
||||
almanac[29]["Argument_of_Perigee"] = 2.622634e+000
|
||||
almanac[29]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[29]["week"] = 1390
|
||||
almanac[29]["Commit_date"] = "06.02.2005"
|
||||
almanac[29]["Life_dates"] = {}
|
||||
|
||||
almanac[30] = {}
|
||||
almanac[30]["System"] = SAT_SYS_GLONASS
|
||||
almanac[30]["Number"] = 2
|
||||
almanac[30]["Orbital"] = 1
|
||||
almanac[30]["GLONASS_Data"] = {}
|
||||
almanac[30]["GLONASS_Data"]["NKU_Number"] = 794
|
||||
almanac[30]["GLONASS_Data"]["Cosmos_Number"] = 2401
|
||||
almanac[30]["Eccentricity"] = 4.486000e-003
|
||||
almanac[30]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[30]["Orbital_Inclination"] = 1.128459e+000
|
||||
almanac[30]["Rate_of_Right_Ascen"] = -6.759654e-009
|
||||
almanac[30]["SQRT_A"] = 5.050500e+003
|
||||
almanac[30]["Right_Ascen_at_Week"] = 5.997871e+000
|
||||
almanac[30]["Argument_of_Perigee"] = 1.709531e+000
|
||||
almanac[30]["Mean_Anom"] = -5.367633e+000
|
||||
almanac[30]["week"] = 1390
|
||||
almanac[30]["Commit_date"] = "02.02.2004"
|
||||
almanac[30]["Life_dates"] = {}
|
||||
|
||||
almanac[31] = {}
|
||||
almanac[31]["System"] = SAT_SYS_GLONASS
|
||||
almanac[31]["Number"] = 3
|
||||
almanac[31]["Orbital"] = 1
|
||||
almanac[31]["GLONASS_Data"] = {}
|
||||
almanac[31]["GLONASS_Data"]["NKU_Number"] = 789
|
||||
almanac[31]["GLONASS_Data"]["Cosmos_Number"] = 2381
|
||||
almanac[31]["Eccentricity"] = 2.459000e-003
|
||||
almanac[31]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[31]["Orbital_Inclination"] = 1.122958e+000
|
||||
almanac[31]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[31]["SQRT_A"] = 5.050500e+003
|
||||
almanac[31]["Right_Ascen_at_Week"] = 5.960713e+000
|
||||
almanac[31]["Argument_of_Perigee"] = -2.683407e+000
|
||||
almanac[31]["Mean_Anom"] = -1.791788e+000
|
||||
almanac[31]["week"] = 1390
|
||||
almanac[31]["Commit_date"] = "04.01.2002"
|
||||
almanac[31]["Life_dates"] = {}
|
||||
|
||||
almanac[32] = {}
|
||||
almanac[32]["System"] = SAT_SYS_GLONASS
|
||||
almanac[32]["Number"] = 4
|
||||
almanac[32]["Orbital"] = 1
|
||||
almanac[32]["GLONASS_Data"] = {}
|
||||
almanac[32]["GLONASS_Data"]["NKU_Number"] = 795
|
||||
almanac[29]["GLONASS_Data"]["Cosmos_Number"] = 2403
|
||||
almanac[32]["Eccentricity"] = 4.054000e-003
|
||||
almanac[32]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[32]["Orbital_Inclination"] = 1.128543e+000
|
||||
almanac[32]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[32]["SQRT_A"] = 5.050500e+003
|
||||
almanac[32]["Right_Ascen_at_Week"] = 5.998081e+000
|
||||
almanac[32]["Argument_of_Perigee"] = 1.497160e+000
|
||||
almanac[32]["Mean_Anom"] = -4.293681e-001
|
||||
almanac[32]["week"] = 1390
|
||||
almanac[32]["Commit_date"] = "29.01.2004"
|
||||
almanac[32]["Life_dates"] = {}
|
||||
|
||||
almanac[33] = {}
|
||||
almanac[33]["System"] = SAT_SYS_GLONASS
|
||||
almanac[33]["Number"] = 5
|
||||
almanac[33]["Orbital"] = 1
|
||||
almanac[33]["GLONASS_Data"] = {}
|
||||
almanac[33]["GLONASS_Data"]["NKU_Number"] = 711
|
||||
almanac[33]["GLONASS_Data"]["Cosmos_Number"] = 2382
|
||||
almanac[33]["Eccentricity"] = 7.040000e-004
|
||||
almanac[33]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[33]["Orbital_Inclination"] = 1.122886e+000
|
||||
almanac[33]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[33]["SQRT_A"] = 5.050600e+003
|
||||
almanac[33]["Right_Ascen_at_Week"] = 5.960713e+000
|
||||
almanac[33]["Argument_of_Perigee"] = 2.740933e+000
|
||||
almanac[33]["Mean_Anom"] = -2.523604e+000
|
||||
almanac[33]["week"] = 1390
|
||||
almanac[33]["Commit_date"] = "13.02.2003"
|
||||
almanac[33]["Life_dates"] = {}
|
||||
|
||||
almanac[34] = {}
|
||||
almanac[34]["System"] = SAT_SYS_GLONASS
|
||||
almanac[34]["Number"] = 6
|
||||
almanac[34]["Orbital"] = 1
|
||||
almanac[34]["GLONASS_Data"] = {}
|
||||
almanac[34]["GLONASS_Data"]["NKU_Number"] = 701
|
||||
almanac[34]["GLONASS_Data"]["Cosmos_Number"] = 2404
|
||||
almanac[34]["Eccentricity"] = 4.766000e-003
|
||||
almanac[34]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[34]["Orbital_Inclination"] = 1.128276e+000
|
||||
almanac[34]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[34]["SQRT_A"] = 5.050500e+003
|
||||
almanac[34]["Right_Ascen_at_Week"] = 5.997906e+000
|
||||
almanac[34]["Argument_of_Perigee"] = 1.802417e+000
|
||||
almanac[34]["Mean_Anom"] = -2.426512e+000
|
||||
almanac[34]["week"] = 1390
|
||||
almanac[34]["Commit_date"] = "08.12.2004"
|
||||
almanac[34]["Life_dates"] = {}
|
||||
|
||||
almanac[35] = {}
|
||||
almanac[35]["System"] = SAT_SYS_GLONASS
|
||||
almanac[35]["Number"] = 7
|
||||
almanac[35]["Orbital"] = 1
|
||||
almanac[35]["GLONASS_Data"] = {}
|
||||
almanac[35]["GLONASS_Data"]["NKU_Number"] = 712
|
||||
almanac[35]["GLONASS_Data"]["Cosmos_Number"] = 2413
|
||||
almanac[35]["Eccentricity"] = 7.570000e-004
|
||||
almanac[35]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[35]["Orbital_Inclination"] = 1.126344e+000
|
||||
almanac[35]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[35]["SQRT_A"] = 5.050500e+003
|
||||
almanac[35]["Right_Ascen_at_Week"] = 5.979388e+000
|
||||
almanac[35]["Argument_of_Perigee"] = 2.566068e+000
|
||||
almanac[35]["Mean_Anom"] = -3.921228e+000
|
||||
almanac[35]["week"] = 1390
|
||||
almanac[35]["Commit_date"] = "07.10.2005"
|
||||
almanac[35]["Life_dates"] = {}
|
||||
|
||||
almanac[36] = {}
|
||||
almanac[36]["System"] = SAT_SYS_GLONASS
|
||||
almanac[36]["GLONASS_Data"] = {}
|
||||
almanac[36]["Number"] = 8
|
||||
almanac[36]["Orbital"] = 1
|
||||
almanac[36]["GLONASS_Data"] = {}
|
||||
almanac[36]["GLONASS_Data"]["NKU_Number"] = 797
|
||||
almanac[36]["GLONASS_Data"]["Cosmos_Number"] = 2412
|
||||
almanac[36]["Eccentricity"] = 4.060000e-004
|
||||
almanac[36]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[36]["Orbital_Inclination"] = 1.126564e+000
|
||||
almanac[36]["Rate_of_Right_Ascen"] = -6.785834e-009
|
||||
almanac[36]["SQRT_A"] = 5.050600e+003
|
||||
almanac[36]["Right_Ascen_at_Week"] = 5.980069e+000
|
||||
almanac[36]["Argument_of_Perigee"] = 2.673633e+000
|
||||
almanac[36]["Mean_Anom"] = -4.812026e+000
|
||||
almanac[36]["week"] = 1390
|
||||
almanac[36]["Commit_date"] = "06.02.2005"
|
||||
almanac[36]["Life_dates"] = {}
|
||||
|
||||
--3 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 17-24
|
||||
almanac[37] = {}
|
||||
almanac[37]["System"] = SAT_SYS_GLONASS
|
||||
almanac[37]["Number"] = 17
|
||||
almanac[37]["Orbital"] = 3
|
||||
almanac[37]["GLONASS_Data"] = {}
|
||||
almanac[37]["GLONASS_Data"]["NKU_Number"] = 787
|
||||
almanac[37]["GLONASS_Data"]["Cosmos_Number"] = 2375
|
||||
almanac[37]["Eccentricity"] = 5.670000e-004
|
||||
almanac[37]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[37]["Orbital_Inclination"] = 1.126524e+000
|
||||
almanac[37]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[37]["SQRT_A"] = 5.050500e+003
|
||||
almanac[37]["Right_Ascen_at_Week"] = 3.895554e+000
|
||||
almanac[37]["Argument_of_Perigee"] = 6.085085e-001
|
||||
almanac[37]["Mean_Anom"] = -2.977407e+000
|
||||
almanac[37]["week"] = 1390
|
||||
almanac[37]["Commit_date"] = "04.11.2000"
|
||||
almanac[37]["Life_dates"] = {}
|
||||
|
||||
|
||||
almanac[38] = {}
|
||||
almanac[38]["System"] = SAT_SYS_GLONASS
|
||||
almanac[38]["Number"] = 18
|
||||
almanac[38]["Orbital"] = 3
|
||||
almanac[38]["GLONASS_Data"] = {}
|
||||
almanac[38]["GLONASS_Data"]["NKU_Number"] = 783
|
||||
almanac[38]["GLONASS_Data"]["Cosmos_Number"] = 2374
|
||||
almanac[38]["Eccentricity"] = 4.520000e-003
|
||||
almanac[38]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[38]["Orbital_Inclination"] = 1.126239e+000
|
||||
almanac[38]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[38]["SQRT_A"] = 5.050600e+003
|
||||
almanac[38]["Right_Ascen_at_Week"] = 3.894071e+000
|
||||
almanac[38]["Argument_of_Perigee"] = -2.509589e+000
|
||||
almanac[38]["Mean_Anom"] = -1.020057e+000
|
||||
almanac[38]["week"] = 1390
|
||||
almanac[38]["Commit_date"] = "05.01.2001"
|
||||
almanac[38]["Life_dates"] = {}
|
||||
|
||||
almanac[39] = {}
|
||||
almanac[39]["System"] = SAT_SYS_GLONASS
|
||||
almanac[39]["Number"] = 19
|
||||
almanac[39]["Orbital"] = 3
|
||||
almanac[39]["GLONASS_Data"] = {}
|
||||
almanac[39]["GLONASS_Data"]["NKU_Number"] = 798
|
||||
almanac[39]["GLONASS_Data"]["Cosmos_Number"] = 2417
|
||||
almanac[39]["Eccentricity"] = 2.023000e-003
|
||||
almanac[39]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[39]["Orbital_Inclination"] = 1.132205e+000
|
||||
almanac[39]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[39]["SQRT_A"] = 5.050500e+003
|
||||
almanac[39]["Right_Ascen_at_Week"] = 3.884018e+000
|
||||
almanac[39]["Argument_of_Perigee"] = 2.718313e+000
|
||||
almanac[39]["Mean_Anom"] = -3.933620e-001
|
||||
almanac[39]["week"] = 1390
|
||||
almanac[39]["Commit_date"] = "22.01.2006"
|
||||
almanac[39]["Life_dates"] = {}
|
||||
|
||||
almanac[40] = {}
|
||||
almanac[40]["System"] = SAT_SYS_GLONASS
|
||||
almanac[40]["Number"] = 20
|
||||
almanac[40]["Orbital"] = 3
|
||||
almanac[40]["GLONASS_Data"] = {}
|
||||
almanac[40]["GLONASS_Data"]["NKU_Number"] = 793
|
||||
almanac[40]["GLONASS_Data"]["Cosmos_Number"] = 2396
|
||||
almanac[40]["Eccentricity"] = 1.822000e-003
|
||||
almanac[40]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[40]["Orbital_Inclination"] = 1.129789e+000
|
||||
almanac[40]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[40]["SQRT_A"] = 5.050500e+003
|
||||
almanac[40]["Right_Ascen_at_Week"] = 3.896863e+000
|
||||
almanac[40]["Argument_of_Perigee"] = 2.723776e+000
|
||||
almanac[40]["Mean_Anom"] = -1.193647e+000
|
||||
almanac[40]["week"] = 1390
|
||||
almanac[40]["Commit_date"] = "31.01.2003"
|
||||
almanac[40]["Life_dates"] = {}
|
||||
|
||||
almanac[41] = {}
|
||||
almanac[41]["System"] = SAT_SYS_GLONASS
|
||||
almanac[41]["Number"] = 21
|
||||
almanac[41]["Orbital"] = 3
|
||||
almanac[41]["GLONASS_Data"] = {}
|
||||
almanac[41]["GLONASS_Data"]["NKU_Number"] = 792
|
||||
almanac[41]["GLONASS_Data"]["Cosmos_Number"] = 2395
|
||||
almanac[41]["Eccentricity"] = 5.290000e-004
|
||||
almanac[41]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[41]["Orbital_Inclination"] = 1.129957e+000
|
||||
almanac[41]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[41]["SQRT_A"] = 5.050500e+003
|
||||
almanac[41]["Right_Ascen_at_Week"] = 3.897806e+000
|
||||
almanac[41]["Argument_of_Perigee"] = -9.519367e-001
|
||||
almanac[41]["Mean_Anom"] = -4.578920e+000
|
||||
almanac[41]["week"] = 1390
|
||||
almanac[41]["Commit_date"] = "31.01.2003"
|
||||
almanac[41]["Life_dates"] = {}
|
||||
|
||||
almanac[42] = {}
|
||||
almanac[42]["System"] = SAT_SYS_GLONASS
|
||||
almanac[42]["Number"] = 22
|
||||
almanac[42]["Orbital"] = 3
|
||||
almanac[42]["GLONASS_Data"] = {}
|
||||
almanac[42]["GLONASS_Data"]["NKU_Number"] = 791
|
||||
almanac[42]["GLONASS_Data"]["Cosmos_Number"] = 2394
|
||||
almanac[42]["Eccentricity"] = 9.200000e-005
|
||||
almanac[42]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[42]["Orbital_Inclination"] = 1.129742e+000
|
||||
almanac[42]["Rate_of_Right_Ascen"] = -6.740456e-009
|
||||
almanac[42]["SQRT_A"] = 5.050500e+003
|
||||
almanac[42]["Right_Ascen_at_Week"] = 3.897404e+000
|
||||
almanac[42]["Argument_of_Perigee"] = 2.518211e+000
|
||||
almanac[42]["Mean_Anom"] = -2.530167e+000
|
||||
almanac[42]["week"] = 1390
|
||||
almanac[42]["Commit_date"] = "21.01.2003"
|
||||
almanac[42]["Life_dates"] = {}
|
||||
|
||||
almanac[43] = {}
|
||||
almanac[43]["System"] = SAT_SYS_GLONASS
|
||||
almanac[43]["Number"] = 23
|
||||
almanac[43]["Orbital"] = 3
|
||||
almanac[43]["GLONASS_Data"] = {}
|
||||
almanac[43]["GLONASS_Data"]["NKU_Number"] = 714
|
||||
almanac[43]["GLONASS_Data"]["Cosmos_Number"] = 2419
|
||||
almanac[43]["Eccentricity"] = 8.730000e-004
|
||||
almanac[43]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[43]["Orbital_Inclination"] = 1.132105e+000
|
||||
almanac[43]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[43]["SQRT_A"] = 5.050500e+003
|
||||
almanac[43]["Right_Ascen_at_Week"] = 3.883808e+000
|
||||
almanac[43]["Argument_of_Perigee"] = -3.039139e-001
|
||||
almanac[43]["Mean_Anom"] = -5.228304e-001
|
||||
almanac[43]["week"] = 1390
|
||||
almanac[43]["Commit_date"] = "31.08.2006"
|
||||
almanac[43]["Life_dates"] = {}
|
||||
|
||||
almanac[44] = {}
|
||||
almanac[44]["System"] = SAT_SYS_GLONASS
|
||||
almanac[44]["Number"] = 24
|
||||
almanac[44]["Orbital"] = 3
|
||||
almanac[44]["GLONASS_Data"] = {}
|
||||
almanac[44]["GLONASS_Data"]["NKU_Number"] = 713
|
||||
almanac[44]["GLONASS_Data"]["Cosmos_Number"] = 2418
|
||||
almanac[44]["Eccentricity"] = 2.044000e-003
|
||||
almanac[44]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[44]["Orbital_Inclination"] = 1.132430e+000
|
||||
almanac[44]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[44]["SQRT_A"] = 5.050500e+003
|
||||
almanac[44]["Right_Ascen_at_Week"] = 3.883983e+000
|
||||
almanac[44]["Argument_of_Perigee"] = -3.722784e-001
|
||||
almanac[44]["Mean_Anom"] = -1.240457e+000
|
||||
almanac[44]["week"] = 1390
|
||||
almanac[44]["Commit_date"] = "31.08.2006"
|
||||
almanac[44]["Life_dates"] = {}
|
||||
|
||||
--2 îðáèòàëüíàÿ ïëîñêîñòü, íîìåðà 9-16
|
||||
almanac[45] = {}
|
||||
almanac[45]["System"] = SAT_SYS_GLONASS
|
||||
almanac[45]["Number"] = 9
|
||||
almanac[45]["Orbital"] = 2
|
||||
almanac[45]["GLONASS_Data"] = {}
|
||||
almanac[45]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[45]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[45]["Eccentricity"] = 1.184000e-003
|
||||
almanac[45]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[45]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[45]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[45]["SQRT_A"] = 5.050500e+003
|
||||
almanac[45]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[45]["Argument_of_Perigee"] = 2.88430067
|
||||
almanac[45]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[45]["week"] = 1390
|
||||
almanac[45]["Commit_date"] = "N/A"
|
||||
almanac[45]["Life_dates"] = {}
|
||||
|
||||
almanac[46] = {}
|
||||
almanac[46]["System"] = SAT_SYS_GLONASS
|
||||
almanac[46]["Number"] = 10
|
||||
almanac[46]["Orbital"] = 2
|
||||
almanac[46]["GLONASS_Data"] = {}
|
||||
almanac[46]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[46]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[46]["Eccentricity"] = 1.184000e-003
|
||||
almanac[46]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[46]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[46]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[46]["SQRT_A"] = 5.050500e+003
|
||||
almanac[46]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[46]["Argument_of_Perigee"] = 3.66930067
|
||||
almanac[46]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[46]["week"] = 1390
|
||||
almanac[46]["Commit_date"] = "N/A"
|
||||
almanac[46]["Life_dates"] = {}
|
||||
|
||||
almanac[47] = {}
|
||||
almanac[47]["System"] = SAT_SYS_GLONASS
|
||||
almanac[47]["Number"] = 11
|
||||
almanac[47]["Orbital"] = 2
|
||||
almanac[47]["GLONASS_Data"] = {}
|
||||
almanac[47]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[47]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[47]["Eccentricity"] = 1.184000e-003
|
||||
almanac[47]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[47]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[47]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[47]["SQRT_A"] = 5.050500e+003
|
||||
almanac[47]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[47]["Argument_of_Perigee"] = 4.45430067
|
||||
almanac[47]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[47]["week"] = 1390
|
||||
almanac[47]["Commit_date"] = "N/A"
|
||||
almanac[47]["Life_dates"] = {}
|
||||
|
||||
almanac[48] = {}
|
||||
almanac[48]["System"] = SAT_SYS_GLONASS
|
||||
almanac[48]["Number"] = 12
|
||||
almanac[48]["Orbital"] = 2
|
||||
almanac[48]["GLONASS_Data"] = {}
|
||||
almanac[48]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[48]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[48]["Eccentricity"] = 1.184000e-003
|
||||
almanac[48]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[48]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[48]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[48]["SQRT_A"] = 5.050500e+003
|
||||
almanac[48]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[48]["Argument_of_Perigee"] = 5.23930067
|
||||
almanac[48]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[48]["week"] = 1390
|
||||
almanac[48]["Commit_date"] = "N/A"
|
||||
almanac[48]["Life_dates"] = {}
|
||||
|
||||
almanac[49] = {}
|
||||
almanac[49]["System"] = SAT_SYS_GLONASS
|
||||
almanac[49]["Number"] = 13
|
||||
almanac[49]["Orbital"] = 2
|
||||
almanac[49]["GLONASS_Data"] = {}
|
||||
almanac[49]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[49]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[49]["Eccentricity"] = 1.184000e-003
|
||||
almanac[49]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[49]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[49]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[49]["SQRT_A"] = 5.050500e+003
|
||||
almanac[49]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[49]["Argument_of_Perigee"] = 6.02430067
|
||||
almanac[49]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[49]["week"] = 1390
|
||||
almanac[49]["Commit_date"] = "N/A"
|
||||
almanac[49]["Life_dates"] = {}
|
||||
|
||||
almanac[50] = {}
|
||||
almanac[50]["System"] = SAT_SYS_GLONASS
|
||||
almanac[50]["Number"] = 14
|
||||
almanac[50]["Orbital"] = 2
|
||||
almanac[50]["GLONASS_Data"] = {}
|
||||
almanac[50]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[50]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[50]["Eccentricity"] = 1.184000e-003
|
||||
almanac[50]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[50]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[50]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[50]["SQRT_A"] = 5.050500e+003
|
||||
almanac[50]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[50]["Argument_of_Perigee"] = 0.52930067
|
||||
almanac[50]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[50]["week"] = 1390
|
||||
almanac[50]["Commit_date"] = "N/A"
|
||||
almanac[50]["Life_dates"] = {}
|
||||
|
||||
almanac[51] = {}
|
||||
almanac[51]["System"] = SAT_SYS_GLONASS
|
||||
almanac[51]["Number"] = 15
|
||||
almanac[51]["Orbital"] = 2
|
||||
almanac[51]["GLONASS_Data"] = {}
|
||||
almanac[51]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[51]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[51]["Eccentricity"] = 1.184000e-003
|
||||
almanac[51]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[51]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[51]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[51]["SQRT_A"] = 5.050500e+003
|
||||
almanac[51]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[51]["Argument_of_Perigee"] = 1.31430067
|
||||
almanac[51]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[51]["week"] = 1390
|
||||
almanac[51]["Commit_date"] = "N/A"
|
||||
almanac[51]["Life_dates"] = {}
|
||||
|
||||
almanac[52] = {}
|
||||
almanac[52]["System"] = SAT_SYS_GLONASS
|
||||
almanac[52]["Number"] = 16
|
||||
almanac[52]["Orbital"] = 2
|
||||
almanac[52]["GLONASS_Data"] = {}
|
||||
almanac[52]["GLONASS_Data"]["NKU_Number"] = "N/A"
|
||||
almanac[52]["GLONASS_Data"]["Cosmos_Number"] = "N/A"
|
||||
almanac[52]["Eccentricity"] = 1.184000e-003
|
||||
almanac[52]["Time_of_Applicability"] = 0.000000e+000
|
||||
almanac[52]["Orbital_Inclination"] = 1.126443e+000
|
||||
almanac[52]["Rate_of_Right_Ascen"] = 0.000000e+000
|
||||
almanac[52]["SQRT_A"] = 5.050500e+003
|
||||
almanac[52]["Right_Ascen_at_Week"] = 1.79067e+000
|
||||
almanac[52]["Argument_of_Perigee"] = 2.09930067
|
||||
almanac[52]["Mean_Anom"] = -5.519651e+000
|
||||
almanac[52]["week"] = 1390
|
||||
almanac[52]["Commit_date"] = "N/A"
|
||||
almanac[52]["Life_dates"] = {}
|
||||
|
||||
SA_mode = false
|
||||
AS_mode = false
|
||||
@@ -1,27 +0,0 @@
|
||||
birds_avail = true --Birds availability. false - there is no birds
|
||||
birds_maximum_hrad = 200 --Maximum altitude above ground al sea level bird could be met
|
||||
birds_maximum_absolute_height = 8000 --Maximum absolute altitude bird could be met
|
||||
birds_minimum_velocity = 40 --Minimum velocity bird could be met
|
||||
birds_delta_time = 3.55
|
||||
birds_probability = {0.006333333*150,
|
||||
0.004166667*150,
|
||||
0.001966667*150,
|
||||
0.001090909*150,
|
||||
0.000741818*150,
|
||||
0.0006*150,
|
||||
0.000510545*150,
|
||||
0.000447273*150,
|
||||
0.000389455*150,
|
||||
0.000349091*150,
|
||||
0.000310909*150,
|
||||
0.000282545*150,
|
||||
0.000250909*150,
|
||||
0.000220364*150,
|
||||
0.000196364*150,
|
||||
0.000174545*150,
|
||||
0.000152727*150,
|
||||
0.000128727*150,
|
||||
0.000103636*150,
|
||||
7.63636E-05*150,
|
||||
0*150
|
||||
}
|
||||
@@ -1,124 +0,0 @@
|
||||
----------------------------------------------------------------------------------------
|
||||
---
|
||||
-- Name: BOS-200 - Tarawa Harrier
|
||||
-- Author: funkyfranky
|
||||
-- Date Created: 18 August 2019
|
||||
--
|
||||
-- # Situation:
|
||||
--
|
||||
-- Practice Case I/II/III recovery using the AV-8B Harrier on the USS Tarawa.
|
||||
--
|
||||
-- See mission briefing for further details.
|
||||
--
|
||||
-- *** IMPORTANT ***
|
||||
-- If you run the mission in single player, hit ESC twice before entering a slot!
|
||||
-- Otherwise the script will not load due to a long standing DCS bug.
|
||||
--
|
||||
----------------------------------------------------------------------------------------
|
||||
|
||||
-- No MOOSE settings menu. Comment out this line if required.
|
||||
_SETTINGS:SetPlayerMenuOff()
|
||||
|
||||
-- Rescue Helo with home base USS Viksburg. Has to be a global object!
|
||||
rescuehelo=RESCUEHELO:New("USS Tarawa", "Rescue Helo")
|
||||
rescuehelo:SetHomeBase(AIRBASE:FindByName("USS Viksburg"))
|
||||
rescuehelo:SetModex(42)
|
||||
|
||||
-- Create AIRBOSS object.
|
||||
local AirbossTarawa=AIRBOSS:New("USS Tarawa")
|
||||
|
||||
-- Add recovery windows:
|
||||
-- Case I from 9:00 to 10:00 am.
|
||||
local window1=AirbossTarawa:AddRecoveryWindow( "9:00", "10:00", 1, nil, true, 25)
|
||||
-- Case II with +15 degrees holding offset from 15:00 for 60 min.
|
||||
local window2=AirbossTarawa:AddRecoveryWindow("15:00", "16:00", 2, 15, true, 20)
|
||||
-- Case III with +30 degrees holding offset from 2100 to 2200.
|
||||
local window3=AirbossTarawa:AddRecoveryWindow("21:00", "22:00", 3, 30, true, 20)
|
||||
|
||||
-- Set TACAN.
|
||||
AirbossTarawa:SetTACAN(73, "X", "LHA")
|
||||
|
||||
-- Not sure if Tarawa has ICLS?
|
||||
--AirbossTarawa:SetICLSoff()
|
||||
|
||||
-- Load all saved player grades from your "Saved Games\DCS" folder (if lfs was desanitized).
|
||||
AirbossTarawa:Load()
|
||||
|
||||
-- Automatically save player results to your "Saved Games\DCS" folder each time a player get a final grade from the LSO.
|
||||
AirbossTarawa:SetAutoSave()
|
||||
|
||||
-- Set radio relay units in order to properly send transmissions with subtitles only visible if correct frequency is tuned in.
|
||||
AirbossTarawa:SetRadioRelayLSO("CH-53E Radio Relay")
|
||||
AirbossTarawa:SetRadioRelayMarshal("SH-60B Radio Relay")
|
||||
|
||||
-- Radios.
|
||||
AirbossTarawa:SetMarshalRadio(243)
|
||||
AirbossTarawa:SetLSORadio(265)
|
||||
|
||||
--Set folder of airboss sound files within miz file.
|
||||
AirbossTarawa:SetSoundfilesFolder("Airboss Soundfiles/")
|
||||
|
||||
-- Remove landed AI planes from flight deck.
|
||||
AirbossTarawa:SetDespawnOnEngineShutdown()
|
||||
|
||||
-- Single carrier menu optimization.
|
||||
AirbossTarawa:SetMenuSingleCarrier()
|
||||
|
||||
-- Add Skipper menu to start recovery via F10 radio menu.
|
||||
AirbossTarawa:SetMenuRecovery(30, 20, true)
|
||||
|
||||
-- Start Airboss.
|
||||
AirbossTarawa:Start()
|
||||
|
||||
|
||||
--- Function called when a recovery starts.
|
||||
function AirbossTarawa:OnAfterRecoveryStart(From, Event, To, Case, Offset)
|
||||
-- Start helo.
|
||||
rescuehelo:Start()
|
||||
end
|
||||
|
||||
--- Function called when a recovery ends.
|
||||
function AirbossTarawa:OnAfterRecoveryStop(From,Event,To)
|
||||
-- Send helo RTB.
|
||||
rescuehelo:RTB()
|
||||
end
|
||||
|
||||
--- Function called when the rescue helo has returned to base.
|
||||
function rescuehelo:OnAfterReturned(From, Event, To, airbase)
|
||||
-- Stop helo.
|
||||
self:__Stop(3)
|
||||
end
|
||||
|
||||
--- Function called when a player gets graded by the LSO.
|
||||
function AirbossTarawa:OnAfterLSOGrade(From, Event, To, playerData, grade)
|
||||
local PlayerData=playerData --Ops.Airboss#AIRBOSS.PlayerData
|
||||
local Grade=grade --Ops.Airboss#AIRBOSS.LSOgrade
|
||||
|
||||
----------------------------------------
|
||||
--- Interface your Discord bot here! ---
|
||||
----------------------------------------
|
||||
|
||||
local score=tonumber(Grade.points)
|
||||
local name=tostring(PlayerData.name)
|
||||
|
||||
-- Report LSO grade to dcs.log file.
|
||||
env.info(self.lid..string.format("Player %s scored %.1f", name, score))
|
||||
end
|
||||
|
||||
|
||||
---------------------------
|
||||
--- Generate AI Traffic ---
|
||||
---------------------------
|
||||
|
||||
local AV8B1=SPAWN:New("Harrier Group 1"):InitModex(70)
|
||||
local AV8B2=SPAWN:New("Harrier Group 2"):InitModex(80)
|
||||
|
||||
-- Spawn always 9 min before the recovery window opens.
|
||||
local spawntimes={"9:06", "14:51", "20:51"}
|
||||
for _,spawntime in pairs(spawntimes) do
|
||||
local _time=UTILS.ClockToSeconds(spawntime)-timer.getAbsTime()
|
||||
if _time>0 then
|
||||
SCHEDULER:New(nil, AV8B1.Spawn, {AV8B1}, _time)
|
||||
SCHEDULER:New(nil, AV8B2.Spawn, {AV8B2}, _time)
|
||||
end
|
||||
end
|
||||
@@ -1,363 +0,0 @@
|
||||
options = {
|
||||
["VR"] = {
|
||||
["box_mouse_cursor"] = true,
|
||||
["custom_IPD"] = "50",
|
||||
["custom_IPD_enable"] = true,
|
||||
["enable"] = false,
|
||||
["hand_controllers"] = false,
|
||||
["pixel_density"] = 1,
|
||||
["prefer_built_in_audio"] = false,
|
||||
["use_mouse"] = true,
|
||||
},
|
||||
["difficulty"] = {
|
||||
["RBDAI"] = true,
|
||||
["aircraftMode"] = true,
|
||||
["avionicsLanguage"] = "english",
|
||||
["birds"] = 0,
|
||||
["cockpitStatusBarAllowed"] = false,
|
||||
["cockpitVisualRM"] = false,
|
||||
["compassTape"] = true,
|
||||
["controlsIndicator"] = true,
|
||||
["easyCommunication"] = false,
|
||||
["easyFlight"] = false,
|
||||
["easyRadar"] = false,
|
||||
["externalViews"] = true,
|
||||
["fuel"] = false,
|
||||
["geffect"] = "realistic",
|
||||
["hideStick"] = false,
|
||||
["iconsTheme"] = "russian",
|
||||
["immortal"] = false,
|
||||
["labels"] = 0,
|
||||
["map"] = true,
|
||||
["miniHUD"] = false,
|
||||
["optionsView"] = "optview_all",
|
||||
["padlock"] = false,
|
||||
["permitCrash"] = true,
|
||||
["radio"] = false,
|
||||
["reports"] = true,
|
||||
["setGlobal"] = true,
|
||||
["spectatorExternalViews"] = true,
|
||||
["tips"] = true,
|
||||
["units"] = "imperial",
|
||||
["userMarks"] = true,
|
||||
["userSnapView"] = true,
|
||||
["weapons"] = false,
|
||||
},
|
||||
["format"] = 1,
|
||||
["graphics"] = {
|
||||
["DOF"] = 0,
|
||||
["LensEffects"] = 3,
|
||||
["MSAA"] = 1,
|
||||
["SSAA"] = 0,
|
||||
["SSAO"] = 0,
|
||||
["anisotropy"] = 4,
|
||||
["aspect"] = 1.7777777777778,
|
||||
["chimneySmokeDensity"] = 3,
|
||||
["civTraffic"] = "low",
|
||||
["clouds"] = 1,
|
||||
["clutterMaxDistance"] = 1500,
|
||||
["cockpitGI"] = 1,
|
||||
["disableAero"] = false,
|
||||
["effects"] = 3,
|
||||
["flatTerrainShadows"] = 0,
|
||||
["forestDistanceFactor"] = 1,
|
||||
["fullScreen"] = false,
|
||||
["heatBlr"] = 2,
|
||||
["height"] = 1440,
|
||||
["lights"] = 2,
|
||||
["motionBlur"] = 0,
|
||||
["multiMonitorSetup"] = "1camera",
|
||||
["outputGamma"] = 1.8,
|
||||
["preloadRadius"] = 150000,
|
||||
["rainDroplets"] = 1,
|
||||
["scaleGui"] = false,
|
||||
["shadowTree"] = false,
|
||||
["shadows"] = 4,
|
||||
["sync"] = false,
|
||||
["terrainTextures"] = "max",
|
||||
["textures"] = 2,
|
||||
["treesVisibility"] = 6000,
|
||||
["useDeferredShading"] = 1,
|
||||
["visibRange"] = "Extreme",
|
||||
["water"] = 2,
|
||||
["width"] = 2560,
|
||||
},
|
||||
["miscellaneous"] = {
|
||||
["Coordinate_Display"] = "Lat Long",
|
||||
["F2_view_effects"] = 1,
|
||||
["TrackIR_external_views"] = false,
|
||||
["accidental_failures"] = false,
|
||||
["autologin"] = true,
|
||||
["chat_window_at_start"] = false,
|
||||
["collect_stat"] = true,
|
||||
["f10_awacs"] = true,
|
||||
["f11_free_camera"] = true,
|
||||
["f5_nearest_ac"] = true,
|
||||
["force_feedback_enabled"] = false,
|
||||
["headmove"] = false,
|
||||
["show_pilot_body"] = false,
|
||||
["synchronize_controls"] = false,
|
||||
},
|
||||
["plugins"] = {
|
||||
["A-10C"] = {
|
||||
["CPLocalList"] = "default",
|
||||
},
|
||||
["A-4E-C"] = {
|
||||
["hideControlStick"] = 0,
|
||||
["rwrType"] = 0,
|
||||
["trimSpeed"] = 0,
|
||||
},
|
||||
["AJS37"] = {
|
||||
["CPLocalList"] = "default",
|
||||
},
|
||||
["AV8BNA"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["INS_Alignment"] = 0,
|
||||
["INS_GYROHasNAV"] = false,
|
||||
["MPCD_EXPORT"] = false,
|
||||
},
|
||||
["Bf-109K-4"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["aileronTrim"] = 0,
|
||||
["assistance"] = 0,
|
||||
["autoRudder"] = false,
|
||||
["cameraOrigin"] = 1,
|
||||
["rudderTrim"] = 0,
|
||||
},
|
||||
["C-101EB"] = {
|
||||
["CPLocalList"] = "english",
|
||||
},
|
||||
["CA"] = {
|
||||
["ground_aim_helper"] = true,
|
||||
["ground_automatic"] = true,
|
||||
["ground_platform_shake"] = false,
|
||||
["ground_target_info"] = true,
|
||||
["kompass_options"] = 1,
|
||||
},
|
||||
["CaptoGlove"] = {
|
||||
["armBending"] = 60,
|
||||
["enable"] = false,
|
||||
},
|
||||
["Christen Eagle II"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["SimplifiedRudder"] = false,
|
||||
},
|
||||
["F-14B"] = {
|
||||
["JESTER_Camera"] = true,
|
||||
["JESTER_HeadMenu"] = true,
|
||||
["JESTER_LandingCallouts"] = true,
|
||||
["JESTER_SwitchToPSTT"] = true,
|
||||
["RadioMenuPttOptions"] = 0,
|
||||
},
|
||||
["F-5E-3"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["JoystickMode"] = 0,
|
||||
["SightCamera"] = 0,
|
||||
["aiHelper"] = false,
|
||||
},
|
||||
["F-86F"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["NoseWheelSteeringSimpleBehaviourF86"] = false,
|
||||
["aiHelper"] = false,
|
||||
["gunCamera"] = 0,
|
||||
["landSeatAdjustF86"] = false,
|
||||
},
|
||||
["F/A-18C"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["F18RealisticTDC"] = true,
|
||||
["abDetent"] = 0,
|
||||
["hmdEye"] = 2,
|
||||
},
|
||||
["FC3"] = {
|
||||
["CPLocalList_A-10A"] = "default",
|
||||
["CPLocalList_F-15C"] = "default",
|
||||
["CPLocalList_J-11A"] = "default",
|
||||
["CPLocalList_MiG-29A"] = "default",
|
||||
["CPLocalList_MiG-29G"] = "default",
|
||||
["CPLocalList_MiG-29S"] = "default",
|
||||
["CPLocalList_Su-25"] = "default",
|
||||
["CPLocalList_Su-27"] = "default",
|
||||
["CPLocalList_Su-33"] = "default",
|
||||
},
|
||||
["FW-190D9"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["assistance"] = 0,
|
||||
["autoRudder"] = false,
|
||||
},
|
||||
["Ka-50"] = {
|
||||
["CPLocalList"] = "english",
|
||||
["Ka50RudderTrimmer"] = false,
|
||||
["Ka50TrimmingMethod"] = 0,
|
||||
["helmetCircleDisplacement"] = 11,
|
||||
},
|
||||
["L-39C"] = {
|
||||
["CPLocalList"] = "english",
|
||||
["CPLocalZAList"] = "english",
|
||||
["gunCamera"] = 1,
|
||||
["sarpp"] = 1,
|
||||
},
|
||||
["M-2000C"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["PPA_TOTPAR"] = false,
|
||||
["UNI_ALIGNED"] = false,
|
||||
["UNI_NODRIFT"] = false,
|
||||
},
|
||||
["Mi-8MTV2"] = {
|
||||
["CPLocalList"] = "english",
|
||||
["Mi8AutopilotAdjustment"] = false,
|
||||
["Mi8CockpitShake"] = 5,
|
||||
["Mi8FOV"] = 120,
|
||||
["Mi8RudderTrimmer"] = false,
|
||||
["Mi8TrimmingMethod"] = 0,
|
||||
["controlHelperMi8"] = false,
|
||||
["gunCamera"] = 0,
|
||||
},
|
||||
["MiG-15bis"] = {
|
||||
["CPLocalList"] = "english",
|
||||
["aiHelper"] = false,
|
||||
["autoLeanToAimMiG15"] = false,
|
||||
["gunCamera"] = 0,
|
||||
},
|
||||
["MiG-19P"] = {
|
||||
["ACHS1_System_Time"] = false,
|
||||
["ARK5_Frequency"] = false,
|
||||
["CPLocalList"] = "default",
|
||||
["CPT_Camera_OFF"] = false,
|
||||
["GYROERR_Disable"] = false,
|
||||
["RP5_Ground_Return"] = 0,
|
||||
},
|
||||
["MiG-21Bis"] = {
|
||||
["CPLocalList"] = "English - Metric",
|
||||
["Engine"] = false,
|
||||
["Freeze"] = false,
|
||||
["Pitot"] = false,
|
||||
["Reticle"] = true,
|
||||
["Shake"] = 5,
|
||||
},
|
||||
["NS430"] = {
|
||||
["SpitfireLFMkIXCW_enabled"] = true,
|
||||
["SpitfireLFMkIX_enabled"] = true,
|
||||
["a10a_enabled"] = true,
|
||||
["a10c_enabled"] = false,
|
||||
["ajs37_enabled"] = true,
|
||||
["av8b_enabled"] = true,
|
||||
["bf109k4_enabled"] = true,
|
||||
["c101cc_enabled"] = true,
|
||||
["c101eb_enabled"] = true,
|
||||
["f15c_enabled"] = true,
|
||||
["f5e3_enabled"] = true,
|
||||
["f86f_enabled"] = true,
|
||||
["fa18c_enabled"] = false,
|
||||
["fw190d9_enabled"] = true,
|
||||
["hawk_enabled"] = true,
|
||||
["i16_enabled"] = true,
|
||||
["j11a_enabled"] = true,
|
||||
["ka50_enabled"] = false,
|
||||
["l39c_3D_enabled"] = true,
|
||||
["l39c_common_enabled"] = true,
|
||||
["l39za_enabled"] = true,
|
||||
["mi8_3D_enabled"] = true,
|
||||
["mi8_common_enabled"] = true,
|
||||
["mig15bis_enabled"] = true,
|
||||
["mig21bis_enabled"] = true,
|
||||
["mig29a_enabled"] = true,
|
||||
["mig29g_enabled"] = true,
|
||||
["mig29s_enabled"] = true,
|
||||
["miraj_enabled"] = true,
|
||||
["p51d_enabled"] = true,
|
||||
["sa342l_enabled"] = true,
|
||||
["sa342m_enabled"] = true,
|
||||
["sa342minigun_enabled"] = true,
|
||||
["sa342mistral_enabled"] = true,
|
||||
["su25_enabled"] = true,
|
||||
["su25t_enabled"] = true,
|
||||
["su27_enabled"] = true,
|
||||
["su33_enabled"] = true,
|
||||
["tf51d_enabled"] = true,
|
||||
["uh1h_enabled"] = true,
|
||||
["yak52_enabled"] = true,
|
||||
},
|
||||
["P-51D"] = {
|
||||
["assistance"] = 0,
|
||||
["autoRudder"] = false,
|
||||
},
|
||||
["SA342"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["CPLocalListL"] = "default",
|
||||
["CPLocalListM"] = "default",
|
||||
["CPLocalListMG"] = "default",
|
||||
["ControlsDisplayLocation"] = 0,
|
||||
["EasierControls"] = false,
|
||||
["EngineBreak"] = true,
|
||||
["MiniStick"] = true,
|
||||
["PreloadWaypoints"] = true,
|
||||
["RudderTrim"] = false,
|
||||
["StickPitchCurve"] = 0,
|
||||
["StickRollCurve"] = 0,
|
||||
["VibrationRate"] = 5,
|
||||
},
|
||||
["SpitfireLFMkIX"] = {
|
||||
["aileronTrim"] = 0,
|
||||
["assistance"] = 0,
|
||||
["autoRudder"] = false,
|
||||
},
|
||||
["Su-25T"] = {
|
||||
["CPLocalList"] = "default",
|
||||
},
|
||||
["TF-51D"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["assistance"] = 0,
|
||||
["autoRudder"] = false,
|
||||
},
|
||||
["Tacview"] = {
|
||||
["tacviewBookmarkShortcut"] = 0,
|
||||
["tacviewClientTelemetryPassword"] = "",
|
||||
["tacviewCompressionLevel"] = 1,
|
||||
["tacviewDataRecordingEnabled"] = true,
|
||||
["tacviewDebugModeEnabled"] = false,
|
||||
["tacviewHostTelemetryPassword"] = "",
|
||||
["tacviewPlaybackDelay"] = 0,
|
||||
["tacviewProfilingPeriod"] = 600,
|
||||
["tacviewRealTimeTelemetryPort"] = "42674",
|
||||
["tacviewRecordClientsSessionsEnabled"] = false,
|
||||
["tacviewRemoteControlPassword"] = "",
|
||||
["tacviewRemoteControlPort"] = "42675",
|
||||
["tacviewTerrainExport"] = 0,
|
||||
},
|
||||
["UH-1H"] = {
|
||||
["CPLocalList"] = "default",
|
||||
["UH1HCockpitShake"] = 5,
|
||||
["UHRudderTrimmer"] = false,
|
||||
["UHTrimmingMethod"] = 0,
|
||||
["autoPilot"] = true,
|
||||
["weapTooltips"] = false,
|
||||
},
|
||||
["Yak52"] = {
|
||||
["CPLocalList"] = "english",
|
||||
["aileronTrim"] = 0,
|
||||
["assistance"] = 0,
|
||||
["autoRudder"] = false,
|
||||
["rudderTrim"] = 0,
|
||||
},
|
||||
},
|
||||
["sound"] = {
|
||||
["GBreathEffect"] = false,
|
||||
["cockpit"] = 100,
|
||||
["gui"] = 100,
|
||||
["headphones"] = 100,
|
||||
["headphones_on_external_views"] = true,
|
||||
["hear_in_helmet"] = true,
|
||||
["music"] = 5,
|
||||
["radioSpeech"] = true,
|
||||
["subtitles"] = true,
|
||||
["volume"] = 25,
|
||||
["world"] = 100,
|
||||
},
|
||||
["views"] = {
|
||||
["cockpit"] = {
|
||||
["avionics"] = 1,
|
||||
["mirrors"] = false,
|
||||
["reflections"] = false,
|
||||
},
|
||||
},
|
||||
}
|
||||
Binary file not shown.
@@ -1,83 +0,0 @@
|
||||
-------------------------
|
||||
-- AIRBOSS Test Script --
|
||||
-------------------------
|
||||
|
||||
-- Set mission menu.
|
||||
AIRBOSS.MenuF10Root=MENU_MISSION:New("Airboss").MenuPath
|
||||
|
||||
-- No MOOSE settings menu.
|
||||
_SETTINGS:SetPlayerMenuOff()
|
||||
|
||||
-- S-3B Recovery Tanker spawning in air.
|
||||
local tanker=RECOVERYTANKER:New("CVN-74", "- Texaco Tanker")
|
||||
tanker:SetTakeoffAir()
|
||||
tanker:SetRadio(256)
|
||||
tanker:SetModex(511)
|
||||
tanker:SetTACAN(1, "TKR")
|
||||
tanker:Start()
|
||||
|
||||
-- E-2D AWACS spawning in air
|
||||
local awacs=RECOVERYTANKER:New("CVN-74", "AWACS")
|
||||
awacs:SetAWACS()
|
||||
awacs:SetTakeoffAir()
|
||||
awacs:SetRadio(264)
|
||||
awacs:SetAltitude(20000)
|
||||
awacs:SetCallsign(CALLSIGN.AWACS.Overloard)
|
||||
awacs:SetRacetrackDistances(20, 8)
|
||||
awacs:SetModex(611)
|
||||
awacs:SetTACAN(2, "OLV")
|
||||
awacs:Start()
|
||||
|
||||
-- Rescue Helo spawned in air with home base USS Perry. Has to be a global object!
|
||||
rescuehelo=RESCUEHELO:New("CVN-74", "CV Helo")
|
||||
rescuehelo:SetHomeBase(AIRBASE:FindByName("CG-67"))
|
||||
rescuehelo:SetTakeoffAir()
|
||||
rescuehelo:SetModex(42)
|
||||
rescuehelo:Start()
|
||||
|
||||
-- Create AIRBOSS object.
|
||||
local AirbossStennis=AIRBOSS:New("CVN-74")
|
||||
|
||||
-- Add recovery windows:
|
||||
local window1=AirbossStennis:AddRecoveryWindow("18:30", "21:00", 1, nil, true, 20)
|
||||
|
||||
-- Radio freqs.
|
||||
AirbossStennis:SetMarshalRadio(305)
|
||||
AirbossStennis:SetLSORadio(265)
|
||||
|
||||
-- Radio relay units.
|
||||
AirbossStennis:SetRadioRelayLSO(rescuehelo:GetUnitName())
|
||||
AirbossStennis:SetRadioRelayMarshal(tanker:GetUnitName())
|
||||
|
||||
-- Set folder of airboss sound files within miz file.
|
||||
AirbossStennis:SetSoundfilesFolder("Airboss Soundfiles/")
|
||||
|
||||
-- Single carrier menu optimization.
|
||||
AirbossStennis:SetMenuSingleCarrier()
|
||||
|
||||
-- Enable skipper menu.
|
||||
AirbossStennis:SetMenuRecovery(15, 30, true)
|
||||
|
||||
-- AI groups explicitly excluded from handling by the Airboss
|
||||
AirbossStennis:SetHandleAIOFF()
|
||||
|
||||
-- Remove landed AI planes from flight deck.
|
||||
AirbossStennis:SetDespawnOnEngineShutdown()
|
||||
|
||||
-- Load all saved player grades from your "Saved Games\DCS" folder (if lfs was desanitized).
|
||||
AirbossStennis:Load()
|
||||
|
||||
-- Automatically save player results to your "Saved Games\DCS" folder each time a player get a final grade from the LSO.
|
||||
AirbossStennis:SetAutoSave()
|
||||
|
||||
-- Enable trap sheet.
|
||||
AirbossStennis:SetTrapSheet()
|
||||
|
||||
-- Set recovery tanker
|
||||
AirbossStennis:SetRecoveryTanker(tanker)
|
||||
|
||||
-- Set AWACS.
|
||||
AirbossStennis:SetAWACS(awacs)
|
||||
|
||||
-- Start airboss class.
|
||||
AirbossStennis:Start()
|
||||
Reference in New Issue
Block a user