mirror of
https://github.com/s-d-a/DCS-ExportScripts.git
synced 2026-07-18 06:42:19 +00:00
Compare commits
7 Commits
| Author | SHA1 | Date | |
|---|---|---|---|
 McMicha
|
e1a9f574a4 | ||
|
McMicha
|
e6656b02a2 | ||
|
McMicha
|
b8ed48b517 | ||
|
McMicha
|
e398ec8f83 | ||
|
McMicha
|
96dbbd34c0 | ||
|
McMicha
|
acd8897db9 | ||
|
McMicha
|
e03cc16901 |
@@ -24,11 +24,11 @@ Der Export von Daten wird für folgende Module unterstützt:
|
||||
- Mirage 2000
|
||||
- P-51D 25/30-NA
|
||||
- SA342L/M/Mistral
|
||||
- SpitfireLFMkIX
|
||||
- SpitfireLFMkIX/CW
|
||||
- Su-25T
|
||||
- TF-51D
|
||||
- UH-1H
|
||||
- alle Flaming Cliffs Flugzeuge
|
||||
- alle Flaming Cliffs Flugzeuge + J-11A
|
||||
|
||||
Kompatibel zur DCS World 2.5.4 und BETA Version
|
||||
|
||||
@@ -57,11 +57,11 @@ Following moduls are supported:
|
||||
- Mirage 2000
|
||||
- P-51D 25/30-NA
|
||||
- SA342L/M/Mistral
|
||||
- SpitfireLFMkIX
|
||||
- SpitfireLFMkIX/CW
|
||||
- Su-25T
|
||||
- TF-51D
|
||||
- UH-1H
|
||||
- all Flaming Cliffs aircrafts
|
||||
- all Flaming Cliffs aircrafts + J-11A
|
||||
|
||||
Compatible with DCS World 2.5.4 and BETA version
|
||||
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
-- F/A-18C Export
|
||||
|
||||
ExportScript.FoundDCSModule = true
|
||||
ExportScript.Version.FA18C_hornet = "1.2.0"
|
||||
ExportScript.Version.FA18C_hornet = "1.2.1"
|
||||
|
||||
ExportScript.ConfigEveryFrameArguments =
|
||||
{
|
||||
@@ -646,10 +646,10 @@ function ExportScript.ProcessIkarusDCSConfigLowImportance(mainPanelDevice)
|
||||
ExportScript.Tools.SendData(2029, " ") -- Comm2Display 2 character
|
||||
end
|
||||
|
||||
local lUHF1Radio = GetDevice(39)
|
||||
local lUHF1Radio = GetDevice(38)
|
||||
ExportScript.Tools.SendData(2030, ExportScript.Tools.DisplayFormat(ExportScript.Tools.RoundFreqeuncy((lUHF1Radio:get_frequency()/1000000))), 7)
|
||||
|
||||
local lUHF2Radio = GetDevice(40)
|
||||
local lUHF2Radio = GetDevice(39)
|
||||
ExportScript.Tools.SendData(2031, ExportScript.Tools.DisplayFormat(ExportScript.Tools.RoundFreqeuncy((lUHF2Radio:get_frequency()/1000000), "7.3", false, 0.005)), 7)
|
||||
end
|
||||
|
||||
|
||||
@@ -1,6 +1,6 @@
|
||||
-- Flaming Cliffs Auxiliary Functons
|
||||
|
||||
ExportScript.Version.FC_AuxiliaryFunctions = "1.2.0"
|
||||
ExportScript.Version.FC_AuxiliaryFunctions = "1.2.1"
|
||||
|
||||
-- Workaround for engine start-up
|
||||
ExportScript.AF.LeftEngineOn = false
|
||||
@@ -626,7 +626,7 @@ function ExportScript.AF.FC_Russian_RadarAltimeter_1000m(warningflag)
|
||||
ExportScript.Tools.SendData(28, lDangerRALT_Lamp)
|
||||
end
|
||||
|
||||
-- Barometric Altimeter for SU-25A, SU25-T
|
||||
-- Barometric Altimeter for SU-33
|
||||
function ExportScript.AF.FC_Russian_BarometricAltimeter_late()
|
||||
|
||||
local lBasicAtmospherePressure = LoGetBasicAtmospherePressure() -- BAROMETRIC PRESSURE (mm Hg)
|
||||
@@ -636,6 +636,42 @@ function ExportScript.AF.FC_Russian_BarometricAltimeter_late()
|
||||
|
||||
lAltBar = lAltBar - ((9.5 * (760 - lBasicAtmospherePressure)) / 2) -- 9.5 m per 1mmHg difference
|
||||
|
||||
lBasicAtmospherePressure = lBasicAtmospherePressure * 1.33322 -- mmHg to hPa
|
||||
|
||||
-- if lAltBar > 10000 then
|
||||
-- lAltBar_kilometer_needle = lAltBar / 100000
|
||||
-- else
|
||||
lAltBar_kilometer_needle = lAltBar / 10000
|
||||
-- end
|
||||
-- if lAltBar > 1000 then
|
||||
-- lAltBar_meter_needle = lAltBar / 1000
|
||||
-- lAltBar_meter_needle = lAltBar_meter_needle - ExportScript.Tools.round(lAltBar_meter_needle, 0, "floor")
|
||||
-- else
|
||||
lAltBar_meter_needle = lAltBar / 1000
|
||||
-- end
|
||||
lAltBar = lAltBar / 1000
|
||||
|
||||
-- AltBar_kilometer_needle {0.0,1.0}
|
||||
-- AltBar_meter_needle {0.0,1.0}
|
||||
-- BasicAtmospherePressure {947, 1080} hPa
|
||||
-- AltBar_kilometer {0, 99} km
|
||||
|
||||
ExportScript.Tools.SendData(30, string.format("%.4f", lAltBar_kilometer_needle))
|
||||
ExportScript.Tools.SendData(31, string.format("%.4f", lAltBar_meter_needle))
|
||||
ExportScript.Tools.SendData(32, string.format("%04d", ExportScript.Tools.round(lBasicAtmospherePressure, 0, "floor")))
|
||||
ExportScript.Tools.SendData(33, string.format("%02d", ExportScript.Tools.round(lAltBar, 0, "floor")))
|
||||
end
|
||||
|
||||
-- Barometric Altimeter for SU-25A, SU25-T
|
||||
function ExportScript.AF.FC_Russian_BarometricAltimeter_late_special()
|
||||
|
||||
local lBasicAtmospherePressure = LoGetBasicAtmospherePressure() -- BAROMETRIC PRESSURE (mm Hg)
|
||||
local lAltBar = LoGetAltitudeAboveSeaLevel() -- ALTITUDE SEA LEVEL (Meter)
|
||||
local lAltBar_kilometer_needle = 0
|
||||
local lAltBar_meter_needle = 0
|
||||
|
||||
lAltBar = lAltBar - ((9.5 * (760 - lBasicAtmospherePressure)) / 2) -- 9.5 m per 1mmHg difference
|
||||
|
||||
-- if lAltBar > 10000 then
|
||||
-- lAltBar_kilometer_needle = lAltBar / 100000
|
||||
-- else
|
||||
@@ -651,16 +687,16 @@ function ExportScript.AF.FC_Russian_BarometricAltimeter_late()
|
||||
|
||||
-- AltBar_kilometer_needle {0.0,1.0}
|
||||
-- AltBar_meter_needle {0.0,1.0}
|
||||
-- BasicAtmospherePressure {600.0, 800.0}
|
||||
-- AltBar_kilometer {0.0, 99.9}
|
||||
-- BasicAtmospherePressure {600, 780} mm Hg
|
||||
-- AltBar_kilometer {0, 99} km
|
||||
|
||||
ExportScript.Tools.SendData(30, string.format("%.4f", lAltBar_kilometer_needle))
|
||||
ExportScript.Tools.SendData(31, string.format("%.4f", lAltBar_meter_needle))
|
||||
ExportScript.Tools.SendData(32, string.format("%.4f", lBasicAtmospherePressure))
|
||||
ExportScript.Tools.SendData(33, string.format("%.4f", lAltBar))
|
||||
ExportScript.Tools.SendData(32, string.format("%04d", ExportScript.Tools.round(lBasicAtmospherePressure, 0, "floor")))
|
||||
ExportScript.Tools.SendData(33, string.format("%02d", ExportScript.Tools.round(lAltBar, 0, "floor")))
|
||||
end
|
||||
|
||||
-- Barometric Altimeter for SU-27, SU-33
|
||||
-- Barometric Altimeter for SU-27
|
||||
function ExportScript.AF.FC_Russian_BarometricAltimeter_20000()
|
||||
|
||||
local lBasicAtmospherePressure = LoGetBasicAtmospherePressure() -- BAROMETRIC PRESSURE (mm Hg)
|
||||
@@ -1266,6 +1302,13 @@ function ExportScript.AF.FC_Russian_AOA_MiG29()
|
||||
|
||||
local lAoA = LoGetAngleOfAttack() -- ANGLE OF ATTACK AoA (Radian)
|
||||
local lAccelerationUnits = LoGetAccelerationUnits().y -- G-LOAD
|
||||
|
||||
if ExportScript.AF.TmpAOAMiG29GLoadMin == nil then
|
||||
ExportScript.AF.TmpAOAMiG29GLoadMin = 0
|
||||
end
|
||||
if ExportScript.AF.TmpAOAMiG29GLoadMax == nil then
|
||||
ExportScript.AF.TmpAOAMiG29GLoadMax = 0
|
||||
end
|
||||
|
||||
if lAoA > 0.0 then -- positive AOA
|
||||
--[[
|
||||
@@ -1334,9 +1377,18 @@ function ExportScript.AF.FC_Russian_AOA_MiG29()
|
||||
]]
|
||||
lAccelerationUnits = 0.09672619047619047619047619047619 * lAccelerationUnits
|
||||
end
|
||||
|
||||
if lAccelerationUnits > ExportScript.AF.TmpAOAMiG29GLoadMax then
|
||||
ExportScript.AF.TmpAOAMiG29GLoadMax = lAccelerationUnits
|
||||
end
|
||||
if lAccelerationUnits < ExportScript.AF.TmpAOAMiG29GLoadMin then
|
||||
ExportScript.AF.TmpAOAMiG29GLoadMin = lAccelerationUnits
|
||||
end
|
||||
|
||||
ExportScript.Tools.SendData(50, string.format("%.4f", lAoA))
|
||||
ExportScript.Tools.SendData(51, string.format("%.4f", lAccelerationUnits))
|
||||
ExportScript.Tools.SendData(52, string.format("%.4f", ExportScript.AF.TmpAOAMiG29GLoadMin))
|
||||
ExportScript.Tools.SendData(53, string.format("%.4f", ExportScript.AF.TmpAOAMiG29GLoadMax))
|
||||
end
|
||||
|
||||
-- Russian Clock ACS-1 for KA-50, SU-25A, MIG-29A , MIG-29S
|
||||
@@ -1402,7 +1454,7 @@ function ExportScript.AF.FC_Russian_Clock_late()
|
||||
ExportScript.Tools.SendData(55, string.format("%.4f", lCurrentHours))
|
||||
ExportScript.Tools.SendData(56, string.format("%.4f", lCurrentMinutes))
|
||||
ExportScript.Tools.SendData(57, string.format("%.4f", lCurrentSeconds))
|
||||
ExportScript.Tools.SendData(58, lDefaultNull) -- red/white flag
|
||||
--ExportScript.Tools.SendData(58, lDefaultNull) -- red/white flag
|
||||
ExportScript.Tools.SendData(59, string.format("%.4f", lFlightTimeHours))
|
||||
ExportScript.Tools.SendData(60, string.format("%.4f", lFlightTimeMinutes))
|
||||
ExportScript.Tools.SendData(61, string.format("%.4f", lCurrentSeconds))
|
||||
@@ -1456,6 +1508,29 @@ function ExportScript.AF.FC_Russian_EGT_1000gc(egttemp, exportid)
|
||||
ExportScript.Tools.SendData(lExportID, string.format("%.4f", lEGTtemp))
|
||||
end
|
||||
|
||||
-- US Standby Compass for MiG-29A/S/G
|
||||
function ExportScript.AF.FC_Russian_Compass2()
|
||||
local lDefaultNull = 0.0
|
||||
local lHeading = math.deg(LoGetSelfData().Heading) -- HEADING (Radian to Grad)
|
||||
--local lHeading = math.deg(LoGetMagneticYaw()) -- HEADING (Radian to Grad)
|
||||
--ExportScript.Tools.WriteToLog('lHeading: '..ExportScript.Tools.dump(lHeading))
|
||||
local lPitch = LoGetSelfData().Pitch -- Pitch
|
||||
local lBank = LoGetSelfData().Bank -- Bank
|
||||
|
||||
if lHeading <= 180 then
|
||||
lHeading = lHeading / 180
|
||||
else
|
||||
lHeading = (lHeading / 180) - 2
|
||||
end
|
||||
|
||||
lPitch = lPitch / 1.31 -- korrektur der maximal Werte
|
||||
lBank = lBank / 6.26 -- korrektur der maximal Werte
|
||||
|
||||
ExportScript.Tools.SendData(67, string.format("%.4f", lHeading)) -- heading
|
||||
ExportScript.Tools.SendData(68, string.format("%.4f", lPitch)) -- pitch
|
||||
ExportScript.Tools.SendData(69, string.format("%.4f", lBank)) -- bank
|
||||
end
|
||||
|
||||
-- Russian Mechanical Device Indicator for SU-25A+T
|
||||
function ExportScript.AF.FC_Russian_MDI_SU25(FunctionTyp)
|
||||
local lFunctionTyp = FunctionTyp or "Ikarus"
|
||||
@@ -1575,7 +1650,7 @@ function ExportScript.AF.FC_Russian_FlareChaff_MiG29(FunctionTyp)
|
||||
end
|
||||
|
||||
if ExportScript.Config.IkarusExport and lFunctionTyp == "Ikarus" then
|
||||
ExportScript.Tools.SendDataDAC(800, lSnares.chaff + lSnares.flare )
|
||||
ExportScript.Tools.SendData(800, lSnares.chaff + lSnares.flare )
|
||||
end
|
||||
end
|
||||
|
||||
@@ -1587,6 +1662,20 @@ function ExportScript.AF.FuelQuantityIndicator_MiG29(FunctionTyp)
|
||||
if lEngineInfo == nil then
|
||||
return
|
||||
end
|
||||
|
||||
local lPayloadInfo = LoGetPayloadInfo()
|
||||
local lRange = 0
|
||||
local lStation5Tank = false
|
||||
local lStation6Tank = false
|
||||
local lStation7Tank = false
|
||||
|
||||
if lEngineInfo ~= nil then
|
||||
lStation5Tank = (lPayloadInfo.Stations[5].CLSID == "{C0FF4842-FBAC-11d5-9190-00A0249B6F00}" and true or false)
|
||||
lStation6Tank = (lPayloadInfo.Stations[6].CLSID == "{C0FF4842-FBAC-11d5-9190-00A0249B6F00}" and true or false)
|
||||
lStation7Tank = (lPayloadInfo.Stations[7].CLSID == "{2BEC576B-CDF5-4B7F-961F-B0FA4312B841}" and true or false)
|
||||
end
|
||||
|
||||
--ExportScript.Tools.WriteToLog('lStation7Tank: '..ExportScript.Tools.dump(lStation7Tank))
|
||||
--ExportScript.Tools.WriteToLog('lEngineInfo: '..ExportScript.Tools.dump(lEngineInfo))
|
||||
--[[
|
||||
[fuel_external] = number: "0"
|
||||
@@ -1617,89 +1706,88 @@ function ExportScript.AF.FuelQuantityIndicator_MiG29(FunctionTyp)
|
||||
local lTotalFuel = lEngineInfo.fuel_internal + lEngineInfo.fuel_external
|
||||
--ExportScript.Tools.WriteToLog('lTotalFuel: '..ExportScript.Tools.dump(lTotalFuel))
|
||||
|
||||
-- Fuel value correction, difference 3D cockpit gauges and export value
|
||||
-- 3000kg = 2740 1,10
|
||||
-- 2500kg = 2260 <- Lamp 2 1,11
|
||||
-- 1000kg = 890 1,12
|
||||
-- 800kg = 700 <- Lamp 3 1,14
|
||||
-- 650kg = 550 <- Lamp 4 1,18
|
||||
if lTotalFuel > 2740 then
|
||||
lTotalFuel = lTotalFuel * 1.1
|
||||
elseif lTotalFuel > 2260 and lTotalFuel < 2740 then
|
||||
lTotalFuel = lTotalFuel * 1.11
|
||||
elseif lTotalFuel > 890 and lTotalFuel < 2260 then
|
||||
lTotalFuel = lTotalFuel * 1.12
|
||||
elseif lTotalFuel > 700 and lTotalFuel < 290 then
|
||||
lTotalFuel = lTotalFuel * 1.14
|
||||
elseif lTotalFuel > 0 and lTotalFuel < 700 then
|
||||
lTotalFuel = lTotalFuel * 1.18
|
||||
end
|
||||
-- Internal Fuel: 3370
|
||||
-- max external Fuel: 2930
|
||||
-- max totak Fuel: 6300
|
||||
-- 1400 Liter center tank = 1163kg, station 7, CLSID {2BEC576B-CDF5-4B7F-961F-B0FA4312B841}
|
||||
-- 1150 Liter tank = 891kg, station 5,6, CLSID {C0FF4842-FBAC-11d5-9190-00A0249B6F00}
|
||||
--lEngineInfo.fuel_external < 1770 -- Tank warning 1
|
||||
--lEngineInfo.fuel_external == 0 -- Tank warning 2
|
||||
--lEngineInfo.fuel_internal < 2500 -- Tank warning 3
|
||||
--lEngineInfo.fuel_internal < 800 -- Tank warning 4
|
||||
--lEngineInfo.fuel_internal < 650 -- Tank warning 5
|
||||
|
||||
if ExportScript.Config.DACExport and lFunctionTyp == "DAC" then
|
||||
ExportScript.Tools.SendDataDAC("300", string.format("%d", ExportScript.Tools.round(((lTotalFuel) / 10), 0, "ceil") * 10) ) -- total fuel in kg
|
||||
|
||||
ExportScript.Tools.SendDataDAC("304", (lTotalFuel < 3800.0 and 1 or 0) ) -- Tank warning 1
|
||||
ExportScript.Tools.SendDataDAC("305", (lTotalFuel < 2550.0 and 1 or 0) ) -- Tank warning 2
|
||||
ExportScript.Tools.SendDataDAC("306", (lTotalFuel < 800.0 and 1 or 0) ) -- Tank warning 3
|
||||
ExportScript.Tools.SendDataDAC("307", (lTotalFuel < 650.0 and 1 or 0) ) -- Tank warning 4
|
||||
if lStation7Tank and (lStation5Tank or lStation6Tank) then
|
||||
ExportScript.Tools.SendDataDAC("304", (lEngineInfo.fuel_external < 1770.0 and 1 or 0) ) -- Tank warning 1
|
||||
ExportScript.Tools.SendDataDAC("305", (lEngineInfo.fuel_external < 1.0 and 1 or 0) ) -- Tank warning 2
|
||||
elseif lStation7Tank and not(lStation5Tank or lStation6Tank) then
|
||||
ExportScript.Tools.SendDataDAC("304", (lEngineInfo.fuel_external < 1.0 and 1 or 0) ) -- Tank warning 1
|
||||
ExportScript.Tools.SendDataDAC("305", 0 ) -- Tank warning 2
|
||||
end
|
||||
ExportScript.Tools.SendDataDAC("306", (lEngineInfo.fuel_internal < 2500.0 and 1 or 0) ) -- Tank warning 3
|
||||
ExportScript.Tools.SendDataDAC("307", (lEngineInfo.fuel_internal < 800.0 and 1 or 0) ) -- Tank warning 4
|
||||
ExportScript.Tools.SendDataDAC("308", (lEngineInfo.fuel_internal < 650.0 and 1 or 0) ) -- Tank warning 5
|
||||
end
|
||||
|
||||
if ExportScript.Config.IkarusExport and lFunctionTyp == "Ikarus" then
|
||||
local lTotalFuel_5_4 = 0
|
||||
local lTotalFuel_4_0 = 0
|
||||
local lTotalFuel_7_5 = 0
|
||||
local lTotalFuel_5_0 = 0
|
||||
|
||||
if lTotalFuel < 5500 then
|
||||
if lTotalFuel > 4000 then
|
||||
--[[
|
||||
y_min = 0.0 -- minimaler Ausgabewert
|
||||
y_max = 1.0 -- maximaler Ausgabewert
|
||||
x_min = 4000 -- minimaler Eingangswert
|
||||
x_max = 5500 -- maximaler Eingangswert
|
||||
if lTotalFuel > 5000 then -- internal and external
|
||||
--[[
|
||||
y_min = 0.0 -- minimaler Ausgabewert
|
||||
y_max = 1.0 -- maximaler Ausgabewert
|
||||
x_min = 5000 -- minimaler Eingangswert
|
||||
x_max = 7500 -- maximaler Eingangswert
|
||||
|
||||
x = 5000 -- aktueller Eingangswert
|
||||
x = 6300 -- aktueller Eingangswert
|
||||
|
||||
d_y = 1 -- Delta Ausgabewerte (y_max - y_min)
|
||||
d_x = 1500 -- Delta Eingangswerte (x_max - x_min)
|
||||
m = 0.00066667 -- Steigung der linearen Funktion (d_y / d_x)
|
||||
n = -2.666685 -- Schnittpunkt der Funktion mit y-Achse (y_max - m * x_max)
|
||||
d_y = 1 -- Delta Ausgabewerte (y_max - y_min)
|
||||
d_x = 2500 -- Delta Eingangswerte (x_max - x_min)
|
||||
m = 0.0004 -- Steigung der linearen Funktion (d_y / d_x)
|
||||
n = -2.0 -- Schnittpunkt der Funktion mit y-Achse (y_max - m * x_max)
|
||||
|
||||
y = 0.666665 -- Ergebnis (m * x + n)
|
||||
]]
|
||||
lTotalFuel_5_4 = 0.00066667 * lTotalFuel + -2.666685
|
||||
else
|
||||
lTotalFuel_5_4 = 0.0
|
||||
end
|
||||
y = 0.52 -- Ergebnis (m * x + n)
|
||||
]]
|
||||
lTotalFuel_7_5 = 0.0004 * lTotalFuel + -2.0
|
||||
lTotalFuel_5_0 = 1
|
||||
else
|
||||
lTotalFuel_5_4 = 1.0
|
||||
end
|
||||
if lTotalFuel < 4000 then
|
||||
--[[
|
||||
y_min = 0.0 -- minimaler Ausgabewert
|
||||
y_max = 1.0 -- maximaler Ausgabewert
|
||||
x_min = 0 -- minimaler Eingangswert
|
||||
x_max = 4000 -- maximaler Eingangswert
|
||||
x_max = 5000 -- maximaler Eingangswert
|
||||
|
||||
x = 3000 -- aktueller Eingangswert
|
||||
x = 3500 -- aktueller Eingangswert
|
||||
|
||||
d_y = 1.0 -- Delta Ausgabewerte (y_max - y_min)
|
||||
d_x = 4000 -- Delta Eingangswerte (x_max - x_min)
|
||||
m = 0.00025 -- Steigung der linearen Funktion (d_y / d_x)
|
||||
d_y = 1 -- Delta Ausgabewerte (y_max - y_min)
|
||||
d_x = 5000 -- Delta Eingangswerte (x_max - x_min)
|
||||
m = 0.0002 -- Steigung der linearen Funktion (d_y / d_x)
|
||||
n = 0.0 -- Schnittpunkt der Funktion mit y-Achse (y_max - m * x_max)
|
||||
|
||||
y = 0.75 -- Ergebnis (m * x + n)
|
||||
y = 0.52 -- Ergebnis (m * x + n)
|
||||
]]
|
||||
lTotalFuel_4_0 = 0.00025 * lTotalFuel
|
||||
else
|
||||
lTotalFuel_4_0 = 1.0
|
||||
lTotalFuel_5_0 = 0.0002 * lTotalFuel + 0
|
||||
lTotalFuel_7_5 = 0
|
||||
end
|
||||
|
||||
ExportScript.Tools.SendData(301, string.format("%0.4f", lTotalFuel_5_4) )
|
||||
ExportScript.Tools.SendData(302, string.format("%0.4f", lTotalFuel_4_0) )
|
||||
ExportScript.Tools.SendData(301, string.format("%0.4f", lTotalFuel_7_5) )
|
||||
ExportScript.Tools.SendData(302, string.format("%0.4f", lTotalFuel_5_0) )
|
||||
|
||||
ExportScript.Tools.SendData(304, (lTotalFuel < 3800.0 and 1 or 0) ) -- Tank warning 1
|
||||
ExportScript.Tools.SendData(305, (lTotalFuel < 2550.0 and 1 or 0) ) -- Tank warning 2
|
||||
ExportScript.Tools.SendData(306, (lTotalFuel < 800.0 and 1 or 0) ) -- Tank warning 3
|
||||
ExportScript.Tools.SendData(307, (lTotalFuel < 650.0 and 1 or 0) ) -- Tank warning 4
|
||||
if lStation7Tank and (lStation5Tank or lStation6Tank) then
|
||||
ExportScript.Tools.SendData(304, (lEngineInfo.fuel_external < 1770.0 and 1 or 0) ) -- Tank warning 1
|
||||
ExportScript.Tools.SendData(305, (lEngineInfo.fuel_external < 1.0 and 1 or 0) ) -- Tank warning 2
|
||||
elseif lStation7Tank and not(lStation5Tank or lStation6Tank) then
|
||||
ExportScript.Tools.SendData(304, (lEngineInfo.fuel_external < 1.0 and 1 or 0) ) -- Tank warning 1
|
||||
ExportScript.Tools.SendData(305, 0 ) -- Tank warning 2
|
||||
end
|
||||
ExportScript.Tools.SendData(306, (lEngineInfo.fuel_internal < 2500.0 and 1 or 0) ) -- Tank warning 3
|
||||
ExportScript.Tools.SendData(307, (lEngineInfo.fuel_internal < 800.0 and 1 or 0) ) -- Tank warning 4
|
||||
ExportScript.Tools.SendData(308, (lEngineInfo.fuel_internal < 650.0 and 1 or 0) ) -- Tank warning 4
|
||||
ExportScript.Tools.SendData(303, lRange ) -- Range in km
|
||||
end
|
||||
end
|
||||
|
||||
@@ -2133,6 +2221,8 @@ function ExportScript.AF.FC_US_Compass()
|
||||
local lHeading = math.deg(LoGetSelfData().Heading) -- HEADING (Radian to Grad)
|
||||
--local lHeading = math.deg(LoGetMagneticYaw()) -- HEADING (Radian to Grad)
|
||||
--lHeading = 360 - lHeading -- muss umgerechnet werden??
|
||||
local lPitch = LoGetSelfData().Pitch -- Pitch
|
||||
local lBank = LoGetSelfData().Bank -- Bank
|
||||
|
||||
--[[
|
||||
y_min = 1.0 -- minimaler Ausgabewert
|
||||
@@ -2150,9 +2240,9 @@ function ExportScript.AF.FC_US_Compass()
|
||||
]]
|
||||
lHeading = -0.00555555555555555555555555555556 * lHeading + 1.0
|
||||
|
||||
ExportScript.Tools.SendData(31, string.format("%.4f", lHeading)) -- heading
|
||||
ExportScript.Tools.SendData(32, string.format("%.4f", lDefaultNull)) -- pitch
|
||||
ExportScript.Tools.SendData(33, string.format("%.4f", lDefaultNull)) -- bank
|
||||
ExportScript.Tools.SendData(31, string.format("%.4f", lHeading)) -- heading
|
||||
ExportScript.Tools.SendData(32, string.format("%.4f", lDefaultNull)) -- bank
|
||||
ExportScript.Tools.SendData(33, string.format("%.4f", lDefaultNull)) -- pitch
|
||||
end
|
||||
|
||||
-- US F-15C Exaust Gas Temperature
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
-- MiG-29A Export
|
||||
|
||||
ExportScript.FoundFCModule = true
|
||||
ExportScript.Version.MiG29A = "1.2.0"
|
||||
ExportScript.Version.MiG29A = "1.2.1"
|
||||
|
||||
-- auxiliary function
|
||||
dofile(ExportScript.Config.ExportModulePath.."FC_AuxiliaryFuntions.lua")
|
||||
@@ -105,6 +105,9 @@ function ExportScript.ProcessIkarusFCHighImportanceConfig()
|
||||
|
||||
-- Machmeter
|
||||
ExportScript.AF.FC_Russian_Mach_MiG29()
|
||||
|
||||
-- Magnetic Compass
|
||||
ExportScript.AF.FC_Russian_Compass2()
|
||||
else
|
||||
ExportScript.Tools.WriteToLog("Unknown FC Error, no LoGetSelfData.")
|
||||
end
|
||||
@@ -145,21 +148,38 @@ function ExportScript.ProcessIkarusFCLowImportanceConfig()
|
||||
|
||||
-- Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.right, 240, 86)
|
||||
|
||||
-- Hydraulic Pressure Left
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.left, 240, 87)
|
||||
|
||||
-- Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.right, 240, 89)
|
||||
end
|
||||
|
||||
-- Engine Lamps, Start and Afterburner
|
||||
ExportScript.AF.FC_EngineLamps_MiG29(lFunctionTyp)
|
||||
|
||||
-- Oxygen Pressure Left
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 89)
|
||||
|
||||
-- Oxygen Pressure Center
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 90)
|
||||
|
||||
-- Oxygen Pressure Right
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 91)
|
||||
|
||||
local lMechInfo = LoGetMechInfo() -- mechanical components, e.g. Flaps, Wheelbrakes,...
|
||||
if lMechInfo ~= nil then
|
||||
-- Wheelbrakes Hydraulic Pressure Left
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 87)
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 16, 92)
|
||||
|
||||
-- Wheelbrakes Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 88)
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 16, 93)
|
||||
end
|
||||
|
||||
ExportScript.AF.FC_Russian_FlareChaff_MiG29(lFunctionTyp)
|
||||
|
||||
--[[
|
||||
--[[
|
||||
local lPayloadInfo = LoGetPayloadInfo()
|
||||
ExportScript.Tools.WriteToLog('lPayloadInfo: '..ExportScript.Tools.dump(lPayloadInfo))
|
||||
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
-- MiG-29G Export
|
||||
|
||||
ExportScript.FoundFCModule = true
|
||||
ExportScript.Version.MiG29G = "1.2.0"
|
||||
ExportScript.Version.MiG29G = "1.2.1"
|
||||
|
||||
-- auxiliary function
|
||||
dofile(ExportScript.Config.ExportModulePath.."FC_AuxiliaryFuntions.lua")
|
||||
@@ -99,12 +99,15 @@ function ExportScript.ProcessIkarusFCHighImportanceConfig()
|
||||
|
||||
-- Right Jet Engine Turbine Temperature Indicator (EngineTemp, ExportID)
|
||||
ExportScript.AF.FC_Russian_EGT_1000gc(lEngineTempRight, 71)
|
||||
|
||||
|
||||
-- Clock from Ka-50
|
||||
ExportScript.AF.FC_Russian_Clock_late()
|
||||
|
||||
-- Machmeter
|
||||
ExportScript.AF.FC_Russian_Mach_MiG29()
|
||||
|
||||
-- Magnetic Compass
|
||||
ExportScript.AF.FC_Russian_Compass2()
|
||||
else
|
||||
ExportScript.Tools.WriteToLog("Unknown FC Error, no LoGetSelfData.")
|
||||
end
|
||||
@@ -145,21 +148,38 @@ function ExportScript.ProcessIkarusFCLowImportanceConfig()
|
||||
|
||||
-- Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.right, 240, 86)
|
||||
|
||||
-- Hydraulic Pressure Left
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.left, 240, 87)
|
||||
|
||||
-- Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.right, 240, 89)
|
||||
end
|
||||
|
||||
-- Engine Lamps, Start and Afterburner
|
||||
ExportScript.AF.FC_EngineLamps_MiG29(lFunctionTyp)
|
||||
|
||||
-- Oxygen Pressure Left
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 89)
|
||||
|
||||
-- Oxygen Pressure Center
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 90)
|
||||
|
||||
-- Oxygen Pressure Right
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 91)
|
||||
|
||||
local lMechInfo = LoGetMechInfo() -- mechanical components, e.g. Flaps, Wheelbrakes,...
|
||||
if lMechInfo ~= nil then
|
||||
-- Wheelbrakes Hydraulic Pressure Left
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 87)
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 16, 92)
|
||||
|
||||
-- Wheelbrakes Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 88)
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 16, 93)
|
||||
end
|
||||
|
||||
ExportScript.AF.FC_Russian_FlareChaff_MiG29(lFunctionTyp)
|
||||
|
||||
--[[
|
||||
--[[
|
||||
local lPayloadInfo = LoGetPayloadInfo()
|
||||
ExportScript.Tools.WriteToLog('lPayloadInfo: '..ExportScript.Tools.dump(lPayloadInfo))
|
||||
|
||||
|
||||
@@ -1,7 +1,7 @@
|
||||
-- MiG-29S Export
|
||||
|
||||
ExportScript.FoundFCModule = true
|
||||
ExportScript.Version.MiG29S = "1.2.0"
|
||||
ExportScript.Version.MiG29S = "1.2.1"
|
||||
|
||||
-- auxiliary function
|
||||
dofile(ExportScript.Config.ExportModulePath.."FC_AuxiliaryFuntions.lua")
|
||||
@@ -99,12 +99,15 @@ function ExportScript.ProcessIkarusFCHighImportanceConfig()
|
||||
|
||||
-- Right Jet Engine Turbine Temperature Indicator (EngineTemp, ExportID)
|
||||
ExportScript.AF.FC_Russian_EGT_1000gc(lEngineTempRight, 71)
|
||||
|
||||
|
||||
-- Clock from Ka-50
|
||||
ExportScript.AF.FC_Russian_Clock_late()
|
||||
|
||||
-- Machmeter
|
||||
ExportScript.AF.FC_Russian_Mach_MiG29()
|
||||
|
||||
-- Magnetic Compass
|
||||
ExportScript.AF.FC_Russian_Compass2()
|
||||
else
|
||||
ExportScript.Tools.WriteToLog("Unknown FC Error, no LoGetSelfData.")
|
||||
end
|
||||
@@ -145,21 +148,38 @@ function ExportScript.ProcessIkarusFCLowImportanceConfig()
|
||||
|
||||
-- Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.right, 240, 86)
|
||||
|
||||
-- Hydraulic Pressure Left
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.left, 240, 87)
|
||||
|
||||
-- Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lEngineInfo.HydraulicPressure.right, 240, 89)
|
||||
end
|
||||
|
||||
-- Engine Lamps, Start and Afterburner
|
||||
ExportScript.AF.FC_EngineLamps_MiG29(lFunctionTyp)
|
||||
|
||||
-- Oxygen Pressure Left
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 89)
|
||||
|
||||
-- Oxygen Pressure Center
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 90)
|
||||
|
||||
-- Oxygen Pressure Right
|
||||
--ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 91)
|
||||
|
||||
local lMechInfo = LoGetMechInfo() -- mechanical components, e.g. Flaps, Wheelbrakes,...
|
||||
if lMechInfo ~= nil then
|
||||
-- Wheelbrakes Hydraulic Pressure Left
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 87)
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 16, 92)
|
||||
|
||||
-- Wheelbrakes Hydraulic Pressure Right
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 240, 88)
|
||||
ExportScript.AF.FC_OneNeedleGauge(lMechInfo.wheelbrakes.value, 16, 93)
|
||||
end
|
||||
|
||||
ExportScript.AF.FC_Russian_FlareChaff_MiG29(lFunctionTyp)
|
||||
|
||||
--[[
|
||||
--[[
|
||||
local lPayloadInfo = LoGetPayloadInfo()
|
||||
ExportScript.Tools.WriteToLog('lPayloadInfo: '..ExportScript.Tools.dump(lPayloadInfo))
|
||||
|
||||
|
||||
@@ -0,0 +1,268 @@
|
||||
-- Spitfire LFMk IX CW
|
||||
|
||||
ExportScript.FoundDCSModule = true
|
||||
ExportScript.Version.SpitfireLFMkIXCW = "1.2.0"
|
||||
|
||||
ExportScript.ConfigEveryFrameArguments =
|
||||
{
|
||||
--[[
|
||||
every frames arguments
|
||||
based of "mainpanel_init.lua"
|
||||
Example (http://www.lua.org/manual/5.1/manual.html#pdf-string.format)
|
||||
[DeviceID] = "Format"
|
||||
[4] = "%.4f", <- floating-point number with 4 digits after point
|
||||
[19] = "%0.1f", <- floating-point number with 1 digit after point
|
||||
[129] = "%1d", <- decimal number
|
||||
[5] = "%.f", <- floating point number rounded to a decimal number
|
||||
]]
|
||||
-- Flight Instruments
|
||||
[11] = "%.4f", -- OxygenDeliveryGauge {0.0, 0.4}{0.0, 4000.0}
|
||||
[12] = "%.4f", -- OxygenSupplyGauge
|
||||
[17] = "%.4f", -- TrimGauge {-1.0, 1.0}
|
||||
[18] = "%.4f", -- PneumaticPressureGauge {0.0, 1.0}{0.0, 600.0}
|
||||
[19] = "%.4f", -- Left wheel brake pressure gauge {0.0, 1.0}{0.0, 130.0}
|
||||
[20] = "%.4f", -- Right wheel brake pressure gauge {0.0, 1.0}{0.0, 130.0}
|
||||
[21] = "%.4f", -- Airspeed gauge {0.0, 0.5}{0.0, 500.0}
|
||||
[23] = "%.4f", -- Attitude Horizon Bank {-1.0, 1.0}
|
||||
[24] = "%.4f", -- Attitude Horizon Pitch {-1.0, 1.0}
|
||||
[25] = "%.4f", -- Variometer gauge {-1.0, 1.0}{-4000.0, 4000.0}
|
||||
[26] = "%.4f", -- Altimeter gauge Hundreds {0.0, 1.0}{0.0, 10.0}
|
||||
[27] = "%.4f", -- Altimeter gauge Thousands {0.0, 1.0}{0.0, 10.0}
|
||||
[28] = "%.4f", -- Altimeter gauge Tens Thousabds {0.0, 1.0}{0.0, 10.0}
|
||||
[29] = "%.4f", -- Altimeter gauge Pressure {0.0, 1.0}{800.0, 1050.0}
|
||||
[31] = "%.4f", -- DI gauge {0.0, 1.0}{0.0, 2.0 * 3.1415926}
|
||||
[33] = "%.4f", -- Sideslip gauge {-1.0, 1.0}
|
||||
[34] = "%.4f", -- Turn gauge {-1.0, 1.0}
|
||||
[35] = "%.4f", -- Voltmeter {0.0, 1.0}{0.0, 20.0}
|
||||
[37] = "%.4f", -- Tachometer {0.0, 0.5}{0.0, 5000.0}
|
||||
[39] = "%.4f", -- Boost gauge {0.0, 1.0}{-7.0, 24.0}
|
||||
[40] = "%.4f", -- Oil pressure gauge {0.0, 1.0}{0.0, 150.0}
|
||||
[41] = "%.4f", -- Oil temperature gauge {0.0, 1.0}{0.0, 100.0}
|
||||
[42] = "%.4f", -- Radiator temperature gauge {0.0, 0.7}{0.0, 140.0}
|
||||
[43] = "%.4f", -- Fuel contents gauge {0.0, 0.1, 1.0}{-1.0, 0.0, 37.0}
|
||||
[51] = "%.4f", -- Clock Hour
|
||||
[52] = "%.4f", -- Clock Minute
|
||||
[53] = "%.4f", -- Clock Second
|
||||
[71] = "%.4f", -- Magnetic compass CompassRoseRoll {-1.0, 1.0}{-20.0, 20.0}
|
||||
[72] = "%.4f", -- Magnetic compass CompassRosePitch {-1.0, 1.0}{-20.0, 20.0}
|
||||
[73] = "%.4f", -- Magnetic compass CompassHeading{0.0, 1.0}
|
||||
[120] = "%1d", -- Radio Lamp A
|
||||
[121] = "%1d", -- Radio Lamp B
|
||||
[122] = "%1d", -- Radio Lamp C
|
||||
[123] = "%1d", -- Radio Lamp D
|
||||
[124] = "%1d", -- Radio Lamp R
|
||||
--[131] = "%1d", -- UC_DOWN_C ???
|
||||
[49] = "%1d", -- Gear Lamp Down
|
||||
[48] = "%1d", -- Gear Lamp Up
|
||||
--[62] = "%.4f", -- ???
|
||||
--[63] = "%.4f", -- ???
|
||||
--[59] = "%.4f", -- ???
|
||||
--[45] = "%.4f" -- GUNSIGHT_RANGE ???
|
||||
}
|
||||
ExportScript.ConfigArguments =
|
||||
{
|
||||
--[[
|
||||
arguments for export in low tick interval
|
||||
based on "clickabledata.lua"
|
||||
]]
|
||||
[13] = "%1d", -- Oxygen Apparatus Controls Valve
|
||||
-- Main Panel
|
||||
[30] = "%.1f", -- Altimeter (Axis) {0.0, 1.0} in 0.1 Steps
|
||||
[32] = "%.1f", -- DI (Axis) {0.0, 1.0} in 0.1 Steps
|
||||
[44] = "%1d", -- Fuel Gauge Button
|
||||
[46] = "%1d", -- Nav. Lights Toggle
|
||||
[47] = "%1d", -- Flaps Lever
|
||||
[50] = "%1d", -- U/C Indicator Blind
|
||||
[54] = "%1d", -- Clock Setter Pinion
|
||||
[55] = "%.1f", -- Clock Setter Pinion (Axis) {0.0, 1.0} in 0.1 Steps
|
||||
[56] = "%1d", -- Magnetos Toggles 1
|
||||
[57] = "%1d", -- Magnetos Toggles 2
|
||||
[58] = "%1d", -- Supercharger Mode Toggle
|
||||
[60] = "%.1f", -- Illumination Controls Left (Axis) {0.0, 1.0} in 0.1 Steps
|
||||
[61] = "%.1f", -- Illumination Controls Right (Axis) {0.0, 1.0} in 0.1 Steps
|
||||
[65] = "%1d", -- Starter Button
|
||||
[67] = "%1d", -- Booster Coil Button
|
||||
[69] = "%1d", -- Primer Pump
|
||||
[68] = "%.2f", -- Primer Pump (Axis) {0.0, 1.0} in 0.04 Steps
|
||||
[70] = "%1d", -- Tank Pressurizer Lever
|
||||
[74] = "%.4f", -- Magnetic Compass Ring (Axis) {0.0, 1.0} in 0.0333 Steps
|
||||
-- Gun Sight and Tertiary Weapons Controls
|
||||
[77] = "%.2f", -- Gun Sight Setter Rings Range (Axis) {0.0, 1.0} in 0.15 Steps
|
||||
[78] = "%.2f", -- Gun Sight Setter Rings Base (Axis) {0.0, 1.0} in 0.15 Steps
|
||||
[79] = "%1d", -- Gun Sight Tint Screen
|
||||
[80] = "%1d", -- Gun Sight Master Switch
|
||||
[81] = "%.1f", -- Gun Sight Dimmer (Axis) {0.0, 1.0} in 0.1 Steps
|
||||
-- Port Wall
|
||||
[145] = "%.2f", -- Elevator Trim Wheel (Axis) {-1.0, 1.0} in 0.01 Steps
|
||||
[146] = "%.1f", -- Rudder Trim Wheel (Axis) {-1.0, 1.0} in 0.1 Steps
|
||||
-- Radio Remote Channel Switcher
|
||||
[115] = "%1d", -- Off Button
|
||||
[116] = "%1d", -- A Button
|
||||
[117] = "%1d", -- B Button
|
||||
[118] = "%1d", -- C Button
|
||||
[119] = "%1d", -- D Button
|
||||
[125] = "%1d", -- Dimmer Toggle
|
||||
[155] = "%1d", -- Transmit Lock Toggle
|
||||
[156] = "%1d", -- Mode Selector
|
||||
-- Throttle Quadrant
|
||||
[126] = "%.1f", -- Throttle Lever (Axis) {-1.0, 1.0} in 0.1 Steps
|
||||
[128] = "%1d", -- Bomb Drop Button
|
||||
[129] = "%.1f", -- Airscrew Lever (Axis) {-1.0, 1.0} in 0.1 Steps
|
||||
[130] = "%1d", -- Mix Cut-Off Lever
|
||||
[131] = "%1d", -- U/C Indicator Cut-Off Toggle
|
||||
--
|
||||
[133] = "%1d", -- Radiator Control Toggle
|
||||
[134] = "%1d", -- Pitot Heater Toggle
|
||||
[135] = "%1d", -- Fuel Pump Toggle
|
||||
[137] = "%1d", -- Carb. Air Control Lever
|
||||
[158] = "%1d", -- Oil Diluter Button
|
||||
[160] = "%1d", -- Supercharger Mode Test Button
|
||||
[162] = "%1d", -- Radiator Flap Test Button
|
||||
-- Stbd. Wall
|
||||
[87] = "%1d", -- De-Icer Lever
|
||||
[88] = "%1d", -- U/C Emergency Release Lever
|
||||
[90] = "%1d", -- Wobble Type Fuel Pump
|
||||
-- Wobble Type Fuel Pump
|
||||
[92] = "%.1f", -- Upward Lamp Mode Selector {0.0,0.5,1.0}
|
||||
[93] = "%.1f", -- Downward Lamp Mode Selector {0.0,0.5,1.0}
|
||||
[94] = "%1d", -- Morse Key
|
||||
--
|
||||
[148] = "%1d", -- U/C Lever
|
||||
-- I.F.F. Control Box
|
||||
[106] = "%1d", -- I.F.F. Upper Toggle (Type B)
|
||||
[107] = "%1d", -- I.F.F. Lower Toggle (Type D)
|
||||
[109] = "%1d", -- I.F.F. Fore Button (0)
|
||||
[110] = "%1d", -- I.F.F. Aft Button (1)
|
||||
-- Fuel Cocks & Tertiary
|
||||
[100] = "%1d", -- Fuel Cock
|
||||
[98] = "%1d", -- Droptank Cock
|
||||
[99] = "%1d", -- Droptank Release Handle
|
||||
-- Canopy Controls
|
||||
[149] = "%1d", -- Cockpit Open/Close Control
|
||||
[140] = "%1d", -- Cockpit Jettison Pull Ball
|
||||
[147] = "%1d" -- Cockpit Side Door Open/Close Control
|
||||
}
|
||||
|
||||
-----------------------------
|
||||
-- HIGH IMPORTANCE EXPORTS --
|
||||
-- done every export event --
|
||||
-----------------------------
|
||||
|
||||
-- Pointed to by ProcessIkarusDCSHighImportance
|
||||
function ExportScript.ProcessIkarusDCSConfigHighImportance(mainPanelDevice)
|
||||
--[[
|
||||
every frame export to Ikarus
|
||||
Example from A-10C
|
||||
Get Radio Frequencies
|
||||
get data from device
|
||||
local lUHFRadio = GetDevice(54)
|
||||
ExportScript.Tools.SendData("ExportID", "Format")
|
||||
ExportScript.Tools.SendData(2000, string.format("%7.3f", lUHFRadio:get_frequency()/1000000)) -- <- special function for get frequency data
|
||||
ExportScript.Tools.SendData(2000, ExportScript.Tools.RoundFreqeuncy((UHF_RADIO:get_frequency()/1000000))) -- ExportScript.Tools.RoundFreqeuncy(frequency (MHz|KHz), format ("7.3"), PrefixZeros (false), LeastValue (0.025))
|
||||
]]
|
||||
end
|
||||
|
||||
function ExportScript.ProcessDACConfigHighImportance(mainPanelDevice)
|
||||
--[[
|
||||
every frame export to DAC
|
||||
Example from A-10C
|
||||
Get Radio Frequencies
|
||||
get data from device
|
||||
local UHF_RADIO = GetDevice(54)
|
||||
ExportScript.Tools.SendDataDAC("ExportID", "Format")
|
||||
ExportScript.Tools.SendDataDAC("ExportID", "Format", HardwareConfigID)
|
||||
ExportScript.Tools.SendDataDAC("2000", string.format("%7.3f", UHF_RADIO:get_frequency()/1000000))
|
||||
ExportScript.Tools.SendDataDAC("2000", ExportScript.Tools.RoundFreqeuncy((UHF_RADIO:get_frequency()/1000000))) -- ExportScript.Tools.RoundFreqeuncy(frequency (MHz|KHz), format ("7.3"), PrefixZeros (false), LeastValue (0.025))
|
||||
]]
|
||||
end
|
||||
|
||||
-----------------------------------------------------
|
||||
-- LOW IMPORTANCE EXPORTS --
|
||||
-- done every gExportLowTickInterval export events --
|
||||
-----------------------------------------------------
|
||||
|
||||
-- Pointed to by ExportScript.ProcessIkarusDCSConfigLowImportance
|
||||
function ExportScript.ProcessIkarusDCSConfigLowImportance(mainPanelDevice)
|
||||
--[[
|
||||
export in low tick interval to Ikarus
|
||||
Example from A-10C
|
||||
Get Radio Frequencies
|
||||
get data from device
|
||||
local lUHFRadio = GetDevice(54)
|
||||
ExportScript.Tools.SendData("ExportID", "Format")
|
||||
ExportScript.Tools.SendData(2000, string.format("%7.3f", lUHFRadio:get_frequency()/1000000)) -- <- special function for get frequency data
|
||||
ExportScript.Tools.SendData(2000, ExportScript.Tools.RoundFreqeuncy((UHF_RADIO:get_frequency()/1000000))) -- ExportScript.Tools.RoundFreqeuncy(frequency (MHz|KHz), format ("7.3"), PrefixZeros (false), LeastValue (0.025))
|
||||
]]
|
||||
-- Cockpit Light
|
||||
ExportScript.Tools.IkarusCockpitLights(mainPanelDevice, {163, 62, 63})
|
||||
-- Gauges light, left panel light, right panel light
|
||||
end
|
||||
|
||||
function ExportScript.ProcessDACConfigLowImportance(mainPanelDevice)
|
||||
--[[
|
||||
export in low tick interval to DAC
|
||||
Example from A-10C
|
||||
Get Radio Frequencies
|
||||
get data from device
|
||||
local UHF_RADIO = GetDevice(54)
|
||||
ExportScript.Tools.SendDataDAC("ExportID", "Format")
|
||||
ExportScript.Tools.SendDataDAC("ExportID", "Format", HardwareConfigID)
|
||||
ExportScript.Tools.SendDataDAC("2000", string.format("%7.3f", UHF_RADIO:get_frequency()/1000000))
|
||||
ExportScript.Tools.SendDataDAC("2000", ExportScript.Tools.RoundFreqeuncy((UHF_RADIO:get_frequency()/1000000))) -- ExportScript.Tools.RoundFreqeuncy(frequency (MHz|KHz), format ("7.3"), PrefixZeros (false), LeastValue (0.025))
|
||||
]]
|
||||
|
||||
--=====================================================================================
|
||||
--[[
|
||||
ExportScript.Tools.WriteToLog('list_cockpit_params(): '..ExportScript.Tools.dump(list_cockpit_params()))
|
||||
ExportScript.Tools.WriteToLog('CMSP: '..ExportScript.Tools.dump(list_indication(7)))
|
||||
|
||||
-- list_indication get tehe value of cockpit displays
|
||||
local ltmp1 = 0
|
||||
for ltmp2 = 0, 20, 1 do
|
||||
ltmp1 = list_indication(ltmp2)
|
||||
ExportScript.Tools.WriteToLog(ltmp2..': '..ExportScript.Tools.dump(ltmp1))
|
||||
end
|
||||
]]
|
||||
--[[
|
||||
-- getmetatable get function name from devices
|
||||
local ltmp1 = 0
|
||||
for ltmp2 = 1, 70, 1 do
|
||||
ltmp1 = GetDevice(ltmp2)
|
||||
ExportScript.Tools.WriteToLog(ltmp2..': '..ExportScript.Tools.dump(ltmp1))
|
||||
ExportScript.Tools.WriteToLog(ltmp2..' (metatable): '..ExportScript.Tools.dump(getmetatable(ltmp1)))
|
||||
end
|
||||
]]
|
||||
|
||||
-- VHF_Radio
|
||||
local lVHF_Radio = GetDevice(15)
|
||||
if lVHF_Radio:is_on() then
|
||||
ExportScript.Tools.SendDataDAC("2000", string.format("%7.3f", lVHF_Radio:get_frequency()/1000000))
|
||||
ExportScript.Tools.SendDataDAC("2000", ExportScript.Tools.RoundFreqeuncy(lVHF_Radio:get_frequency()/1000000))
|
||||
else
|
||||
ExportScript.Tools.SendDataDAC("2000", " ")
|
||||
end
|
||||
|
||||
--[[
|
||||
[115] = "%1d", -- Off Button
|
||||
[116] = "%1d", -- A Button
|
||||
[117] = "%1d", -- B Button
|
||||
[118] = "%1d", -- C Button
|
||||
[119] = "%1d", -- D Button]]
|
||||
local lVHF_Radio_PRESET = ""
|
||||
if mainPanelDevice:get_argument_value(116) > 0.8 then
|
||||
lVHF_Radio_PRESET = 1
|
||||
elseif mainPanelDevice:get_argument_value(117) > 0.8 then
|
||||
lVHF_Radio_PRESET = 2
|
||||
elseif mainPanelDevice:get_argument_value(118) > 0.8 then
|
||||
lVHF_Radio_PRESET = 3
|
||||
elseif mainPanelDevice:get_argument_value(119) > 0.8 then
|
||||
lVHF_Radio_PRESET = 4
|
||||
else
|
||||
lVHF_Radio_PRESET = ""
|
||||
end
|
||||
ExportScript.Tools.SendDataDAC("2001", lVHF_Radio_PRESET)
|
||||
end
|
||||
|
||||
-----------------------------
|
||||
-- Custom functions --
|
||||
-----------------------------
|
||||
@@ -90,7 +90,7 @@ function ExportScript.ProcessIkarusFCHighImportanceConfig()
|
||||
ExportScript.AF.FC_Russian_RadarAltimeter_1500m(100)
|
||||
|
||||
-- Barometric Altimeter
|
||||
ExportScript.AF.FC_Russian_BarometricAltimeter_late()
|
||||
ExportScript.AF.FC_Russian_BarometricAltimeter_late_special()
|
||||
|
||||
-- Tachometer (RPM)
|
||||
ExportScript.AF.FC_Russian_EngineRPM()
|
||||
|
||||
@@ -88,7 +88,7 @@ function ExportScript.ProcessIkarusFCHighImportanceConfig()
|
||||
ExportScript.AF.FC_Russian_RadarAltimeter_1500m(100)
|
||||
|
||||
-- Barometric Altimeter
|
||||
ExportScript.AF.FC_Russian_BarometricAltimeter_late()
|
||||
ExportScript.AF.FC_Russian_BarometricAltimeter_late_special()
|
||||
|
||||
-- Tachometer (RPM)
|
||||
ExportScript.AF.FC_Russian_EngineRPM()
|
||||
|
||||
Binary file not shown.
Binary file not shown.
Reference in New Issue
Block a user