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MOOSE demonstration missions [skip ci]
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Applevangelist
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-- View scripts
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-- Copyright (C) 2004, Eagle Dynamics.
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DisableCombatViews = false -- F5 & Ctrl-F5
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ExternalObjectsLockDistance = 10000.0
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ShowTargetInfo = false
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CameraTerrainRestriction = true
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hAngleRearDefault = 180
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vAngleRearDefault = -8.0
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vAngleRearMin = -90 -- -8.0
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vAngleRearMax = 90.0
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dbg_shell = "weapons.shells.PKT_7_62_T" -- 23mm shell
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dbg_shell = "weapons.nurs.WGr21"
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-- dbg_shell = "weapons.shells.2A64_152" -- 152mm shell
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dbg_shell_v0 = -1 -- Muzzle speed m/s (-1 - speed from shall database)
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dbg_shell_fire_rate = 60
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--reformatted per-unit data to be mod system friendly
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--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)
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function default_fighter_player(t)
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local res = {
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CameraViewAngleLimits = {20.000000,140.000000},
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CameraAngleRestriction = {false ,90.000000,0.500000},
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EyePoint = {0.05 ,0.000000 ,0.000000},
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limits_6DOF = {x = {-0.050000,0.4500000},y ={-0.300000,0.100000},z = {-0.220000,0.220000},roll = 90.000000},
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Allow360rotation = false,
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CameraAngleLimits = {200,-80.000000,110.000000},
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ShoulderSize = 0.2, -- move body when azimuth value more then 90 degrees
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}
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if t then
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for i,o in pairs(t) do
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res[i] = o
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end
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end
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return res
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end
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function fulcrum()
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return {
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Cockpit = {
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default_fighter_player({CockpitLocalPoint = {4.71,1.28,0.000000}})
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},
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Chase = {
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LocalPoint = {1.220000,3.750000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-15.080000,6.350000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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end
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ViewSettings = {}
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ViewSettings["A-10A"] = {
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Cockpit = {
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[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
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EyePoint = {0.000000,0.000000,0.000000},
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limits_6DOF = {x = {-0.050000,0.600000},
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y = {-0.300000,0.100000},
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z = {-0.250000,0.250000},
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roll = 90.000000}}),
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}, -- Cockpit
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Chase = {
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LocalPoint = {0.600000,3.682000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-27.000000,12.000000,0.000000},
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AnglesDefault = {0.000000,-12.000000},
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}, -- Arcade
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}
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ViewSettings["A-10C"] = {
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Cockpit = {
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[1] = default_fighter_player({CockpitLocalPoint = {4.300000,1.282000,0.000000},
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EyePoint = {0.000000,0.000000,0.000000},
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limits_6DOF = {x = {-0.050000,0.600000},
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y = {-0.300000,0.100000},
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z = {-0.250000,0.250000},
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roll = 90.000000}}),
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}, -- Cockpit
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Chase = {
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LocalPoint = {0.600000,3.682000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-27.000000,12.000000,0.000000},
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AnglesDefault = {0.000000,-12.000000},
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}, -- Arcade
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}
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ViewSettings["F-15C"] = {
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Cockpit = {
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[1] = default_fighter_player({CockpitLocalPoint = {6.210000,1.204000,0.000000}})-- player slot 1
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}, -- Cockpit
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Chase = {
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LocalPoint = {2.510000,3.604000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-13.790000,6.204000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["Ka-50"] = {
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Cockpit = {
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[1] = {-- player slot 1
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CockpitLocalPoint = {3.188000,0.390000,0.000000},
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CameraViewAngleLimits = {20.000000,120.000000},
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CameraAngleRestriction = {false,60.000000,0.400000},
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CameraAngleLimits = {140.000000,-65.000000,90.000000},
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EyePoint = {0.090000,0.000000,0.000000},
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limits_6DOF = {x = {-0.020000,0.350000},y ={-0.150000,0.165000},z = {-0.170000,0.170000},roll = 90.000000},
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},
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}, -- Cockpit
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Chase = {
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LocalPoint = {-0.512000,2.790000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-16.812000,5.390000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["MiG-29A"] = fulcrum()
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ViewSettings["MiG-29G"] = fulcrum()
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ViewSettings["MiG-29S"] = fulcrum()
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ViewSettings["P-51D"] = {
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Cockpit = {
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[1] = {-- player slot 1
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CockpitLocalPoint = {-1.500000,0.618000,0.000000},
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CameraViewAngleLimits = {20.000000,120.000000},
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CameraAngleRestriction = {false,90.000000,0.500000},
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CameraAngleLimits = {200,-80.000000,90.000000},
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EyePoint = {0.025000,0.100000,0.000000},
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ShoulderSize = 0.15,
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Allow360rotation = false,
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limits_6DOF = {x = {-0.050000,0.450000},y ={-0.200000,0.200000},z = {-0.220000,0.220000},roll = 90.000000},
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},
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}, -- Cockpit
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Chase = {
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LocalPoint = {0.200000,-0.652000,-0.650000},
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AnglesDefault = {0.000000,0.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-21.500000,5.618000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["Su-25"] = {
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Cockpit = {
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[1] = default_fighter_player({CockpitLocalPoint = {3.352000,0.506000,0.000000}}),-- player slot 1
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}, -- Cockpit
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Chase = {
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LocalPoint = {-0.348000,2.906000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-16.648001,5.506000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["Su-25T"] = {
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Cockpit = {
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[1] = default_fighter_player({CockpitLocalPoint = {3.406000,0.466000,0.000000}}),-- player slot 1
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}, -- Cockpit
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Chase = {
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LocalPoint = {-0.294000,2.866000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-16.594000,5.466000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["Su-25TM"] = {
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Cockpit = {
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[1] = {-- player slot 1
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CockpitLocalPoint = {4.000000,1.000000,0.000000},
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CameraViewAngleLimits = {20.000000,140.000000},
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CameraAngleRestriction = {true,90.000000,0.400000},
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CameraAngleLimits = {160.000000,-70.000000,90.000000},
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EyePoint = {0.000000,0.000000,0.000000},
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limits_6DOF = {x = {-0.200000,0.200000},y ={-0.200000,0.200000},z = {-0.200000,0.200000},roll = 60.000000},
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},
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}, -- Cockpit
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Chase = {
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LocalPoint = {4.000000,2.000000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {4.000000,2.000000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["Su-27"] = {
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Cockpit = {
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[1] = default_fighter_player({CockpitLocalPoint = {7.959000,1.419000,0.000000}})-- player slot 1
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}, -- Cockpit
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Chase = {
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LocalPoint = {4.259000,3.819000,0.000000},
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AnglesDefault = {180.000000,-8.000000},
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}, -- Chase
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Arcade = {
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LocalPoint = {-12.041000,6.419000,0.000000},
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AnglesDefault = {0.000000,-8.000000},
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}, -- Arcade
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}
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ViewSettings["Su-33"] = ViewSettings["Su-27"]
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-1698
File diff suppressed because it is too large
Load Diff
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-- View scripts
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-- Copyright (C) 2004, Eagle Dynamics.
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CockpitMouse = true --false
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CockpitMouseSpeedSlow = 1.0
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CockpitMouseSpeedNormal = 10.0
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CockpitMouseSpeedFast = 20.0
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CockpitKeyboardAccelerationSlow = 5.0
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CockpitKeyboardAccelerationNormal = 30.0
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CockpitKeyboardAccelerationFast = 80.0
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CockpitKeyboardZoomAcceleration = 300.0
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DisableSnapViewsSaving = false
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UseDefaultSnapViews = true
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CockpitPanStepHor = 45.0
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CockpitPanStepVert = 30.0
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CockpitNyMove = true
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CockpitHAngleAccelerateTimeMax = 0.15
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CockpitVAngleAccelerateTimeMax = 0.15
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CockpitZoomAccelerateTimeMax = 0.2
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function NaturalHeadMoving(tang, roll, omz)
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local r = roll
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if r > 90.0 then
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r = 180.0 - r
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elseif roll < -90.0 then
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r = -180.0 - r
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end
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local hAngle = -0.25 * r
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local vAngle = math.min(math.max(0.0, 0.4 * tang + 45.0 * omz), 90.0)
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return hAngle, vAngle
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end
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ExternalMouse = true
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ExternalMouseSpeedSlow = 1.0
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ExternalMouseSpeedNormal = 5.0
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ExternalMouseSpeedFast = 20.0
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ExternalViewAngleMin = 3.0
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ExternalViewAngleMax = 170.0
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ExternalViewAngleDefault = 60.0
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ExternalKeyboardZoomAcceleration = 30.0
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ExternalKeyboardZoomAccelerateTimeMax = 1.0
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ExplosionExpoTime = 4.0
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ExternalKeyboardAccelerationSlow = 1.0
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ExternalKeyboardAccelerationNormal = 10.0
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ExternalKeyboardAccelerationFast = 30.0
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ExternalHAngleAccelerateTimeMax = 3.0
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ExternalVAngleAccelerateTimeMax = 3.0
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ExternalDistAccelerateTimeMax = 3.0
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ExternalHAngleLocalAccelerateTimeMax = 3.0
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ExternalVAngleLocalAccelerateTimeMax = 3.0
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ExternalAngleNormalDiscreteStep = 15.0/ExternalKeyboardAccelerationNormal -- When 'S' is pressed only
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ChaseCameraNyMove = true
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FreeCameraAngleIncrement = 3.0
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FreeCameraDistanceIncrement = 200.0
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FreeCameraLeftRightIncrement = 2.0
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FreeCameraAltitudeIncrement = 2.0
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FreeCameraScalarSpeedAcceleration = 0.1
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xMinMap = -300000
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xMaxMap = 500000
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yMinMap = -400000
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yMaxMap = 200000
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dxMap = 150000
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dyMap = 100000
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head_roll_shaking = true
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head_roll_shaking_max = 30.0
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head_roll_shaking_compensation_gain = 0.3
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-- CameraJiggle() and CameraFloat() functions make camera position
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-- dependent on FPS so be careful in using the Shift-J command with tracks, please.
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-- uncomment to use custom jiggle functions
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--[[
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function CameraJiggle(t,rnd1,rnd2,rnd3)
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local rotX, rotY, rotZ
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rotX = 0.05 * rnd1 * math.sin(37.0 * (t - 0.0))
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rotY = 0.05 * rnd2 * math.sin(41.0 * (t - 1.0))
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rotZ = 0.05 * rnd3 * math.sin(53.0 * (t - 2.0))
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return rotX, rotY, rotZ
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end
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function CameraFloat(t)
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local dX, dY, dZ
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dX = 0.61 * math.sin(0.7 * t) + 0.047 * math.sin(1.6 * t);
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dY = 0.43 * math.sin(0.6 * t) + 0.067 * math.sin(1.7 * t);
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dZ = 0.53 * math.sin(1.0 * t) + 0.083 * math.sin(1.9 * t);
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return dX, dY, dZ
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end
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--]]
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--Debug keys
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DEBUG_TEXT = 1
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DEBUG_GEOMETRY = 2
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debug_keys = {
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[DEBUG_TEXT] = 1,
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[DEBUG_GEOMETRY] = 1
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}
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function onDebugCommand(command)
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if command == 10000 then
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if debug_keys[DEBUG_TEXT] ~= 0 or debug_keys[DEBUG_GEOMETRY] ~= 0 then
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debug_keys[DEBUG_GEOMETRY] = 0
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debug_keys[DEBUG_TEXT] = 0
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else
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debug_keys[DEBUG_GEOMETRY] = 1
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debug_keys[DEBUG_TEXT] = 1
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end
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elseif command == 10001 then
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if debug_keys[DEBUG_TEXT] ~= 0 then
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debug_keys[DEBUG_TEXT] = 0
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else
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debug_keys[DEBUG_TEXT] = 1
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end
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elseif command == 10002 then
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if debug_keys[DEBUG_GEOMETRY] ~= 0 then
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debug_keys[DEBUG_GEOMETRY] = 0
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else
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debug_keys[DEBUG_GEOMETRY] = 1
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end
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end
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end
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-- gain values for TrackIR , to unify responce on diffrent types of aircraft
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TrackIR_gain_x = -0.6
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TrackIR_gain_y = 0.3
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TrackIR_gain_z = -0.25
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TrackIR_gain_roll = -90
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-880
@@ -1,880 +0,0 @@
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SAT_SYS_GLONASS = 0
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SAT_SYS_GPS = 1
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almanac = {}
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--GPS
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almanac[0] = {}
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almanac[0]["System"] = SAT_SYS_GPS
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almanac[0]["Number"] = 1
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almanac[0]["Orbital"] = "F"
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almanac[0]["Eccentricity"] = 6.294000e-003
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almanac[0]["Time_of_Applicability"] = 5.898240e+005
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almanac[0]["Orbital_Inclination"] = 9.885676e-001
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almanac[0]["Rate_of_Right_Ascen"] = -7.862702e-009
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almanac[0]["SQRT_A"] = 5.153700e+003
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almanac[0]["Right_Ascen_at_Week"] = 8.096750e-001
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almanac[0]["Argument_of_Perigee"] = -1.777773e+000
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almanac[0]["Mean_Anom"] = -5.315745e-001
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almanac[0]["week"] = 1390
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almanac[1] = {}
|
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almanac[1]["System"] = SAT_SYS_GPS
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||||
almanac[1]["Number"] = 2
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||||
almanac[1]["Orbital"] = "C"
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almanac[1]["Eccentricity"] = 8.794000e-003
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||||
almanac[1]["Time_of_Applicability"] = 5.898240e+005
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||||
almanac[1]["Orbital_Inclination"] = 9.487811e-001
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almanac[1]["Rate_of_Right_Ascen"] = 0.000000e+000
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almanac[1]["SQRT_A"] = 5.153700e+003
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||||
almanac[1]["Right_Ascen_at_Week"] = -1.329172e+000
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||||
almanac[1]["Argument_of_Perigee"] = 2.138637e+000
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||||
almanac[1]["Mean_Anom"] = 7.311702e-001
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||||
almanac[1]["week"] = 1390
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almanac[2] = {}
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almanac[2]["System"] = SAT_SYS_GPS
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almanac[2]["Number"] = 3
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||||
almanac[2]["Orbital"] = "F"
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||||
almanac[2]["Eccentricity"] = 8.424000e-003
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||||
almanac[2]["Time_of_Applicability"] = 5.898240e+005
|
||||
almanac[2]["Orbital_Inclination"] = 9.262804e-001
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||||
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
|
||||
-49
@@ -1,49 +0,0 @@
|
||||
---
|
||||
-- Name: DET-310 - EWR - Line Of Sight
|
||||
-- Author: FlightControl
|
||||
-- Date Created: 12 Sep 2018
|
||||
--
|
||||
-- # Situation:
|
||||
--
|
||||
-- Demonstrates the lost of line of sight using an airplane.
|
||||
|
||||
SetGroup = SET_GROUP:New():FilterPrefixes( "Recce" ):FilterStart()
|
||||
|
||||
HQ = GROUP:FindByName( "HQ" )
|
||||
|
||||
CC = COMMANDCENTER:New( HQ, "HQ" )
|
||||
|
||||
RecceDetection = DETECTION_AREAS
|
||||
:New( SetGroup, 1500 )
|
||||
:FilterCategories( { Unit.Category.AIRPLANE } )
|
||||
--:InitDetectVisual( true )
|
||||
:InitDetectIRST( true )
|
||||
:InitDetectRadar( true )
|
||||
:InitDetectRWR( true )
|
||||
:InitDetectOptical( true )
|
||||
|
||||
RecceDetection:Start()
|
||||
|
||||
_SETTINGS:SetA2A_BRAA()
|
||||
_SETTINGS:SetA2G_BR()
|
||||
|
||||
--- OnAfter Transition Handler for Event DetectedItem.
|
||||
-- @param Functional.Detection#DETECTION_AREAS RecceDetection self
|
||||
-- @param #string From The From State string.
|
||||
-- @param #string Event The Event string.
|
||||
-- @param #string To The To State string.
|
||||
-- @param Functional.Detection#DETECTION_BASE.DetectedItem DetectedItem
|
||||
function RecceDetection:OnAfterDetectedItem(From,Event,To,DetectedItem)
|
||||
|
||||
local DetectionReport = self:DetectedReportDetailed( SetGroup:GetFirst() )
|
||||
|
||||
HQ:MessageToAll( DetectionReport, 15, "Detection" )
|
||||
|
||||
if DetectedItem.IsDetected then
|
||||
local Coordinate = DetectedItem.Coordinate -- Core.Point#COORDINATE
|
||||
HQ:MessageToAll( "Detected", 15, "Detection" )
|
||||
end
|
||||
|
||||
end
|
||||
|
||||
garbagecollect()
|
||||
Reference in New Issue
Block a user