FalconSharedMemoryArea2

[dglava]

I am trying to get values from FalconSharedMemoryArea2. I have tried to modify falcon.py to include some of the data from it, but without much success.

~I wanted to access the FlyState. Running the script below isn't returning integers in the range of 0 to 5 as expected, but somewhat random longer integers (01241535 for example). I'm not very knowledgeable about this and I'm pretty sure I'm doing something wrong. How would I access the FlyState?~

Edit: I have made some progress. I have added the FLIGHTDATA2 structure. I am however unsure if I assigned all the ctypes correctly. I am also getting a weird byte for pilotsStatus. I assume I am using it wrongly? How would I get the correct pilotsStatus?

Here's my modification of falcon.py:

import ctypes, ctypes.wintypes, sys, logging, time

FILE_MAP_COPY = 0x0001
FILE_MAP_WRITE = 0x0002
FILE_MAP_READ = 0x0004
FILE_MAP_ALL_ACCESS = 0x0008

class FLIGHTDATA(ctypes.Structure):
    _fields_ = (
        ("x", ctypes.wintypes.FLOAT), # Ownship North (Ft)
        ("y", ctypes.wintypes.FLOAT), # Ownship East (Ft)
        ("z", ctypes.wintypes.FLOAT), # Ownship Down (Ft)
        ("xDot", ctypes.wintypes.FLOAT), # Ownship North Rate (ft/sec)
        ("yDot", ctypes.wintypes.FLOAT), # Ownship East Rate (ft/sec)
        ("zDot", ctypes.wintypes.FLOAT), # Ownship Down Rate (ft/sec)
        ("alpha", ctypes.wintypes.FLOAT), # Ownship AOA (Degrees)
        ("beta", ctypes.wintypes.FLOAT), # Ownship Beta (Degrees)
        ("gamma", ctypes.wintypes.FLOAT), # Ownship Gamma (Radians)
        ("pitch", ctypes.wintypes.FLOAT), # Ownship Pitch (Radians)
        ("roll", ctypes.wintypes.FLOAT), # Ownship Pitch (Radians)
        ("yaw", ctypes.wintypes.FLOAT), # Ownship Pitch (Radians)
        ("mach", ctypes.wintypes.FLOAT), # Ownship Mach number
        ("kias", ctypes.wintypes.FLOAT), # Ownship Indicated Airspeed (Knots)
        ("vt", ctypes.wintypes.FLOAT), # Ownship True Airspeed (Ft/Sec)
        ("gs", ctypes.wintypes.FLOAT), # Ownship Normal Gs
        ("windOffset", ctypes.wintypes.FLOAT), # Wind delta to FPM (Radians)
        ("nozzlePos", ctypes.wintypes.FLOAT), # Ownship engine nozzle percent open (0-100)
        ("internalFuel", ctypes.wintypes.FLOAT), # Ownship internal fuel (Lbs)
        ("externalFuel", ctypes.wintypes.FLOAT), # Ownship external fuel (Lbs)
        ("fuelFlow", ctypes.wintypes.FLOAT), # Ownship fuel flow (Lbs/Hour)
        ("rpm", ctypes.wintypes.FLOAT), # Ownship engine rpm (Percent 0-103)
        ("ftit", ctypes.wintypes.FLOAT), # Ownship Forward Turbine Inlet Temp (Degrees C)
        ("gearPos", ctypes.wintypes.FLOAT), # Ownship Gear position 0 = up, 1 = down;
        ("speedBrake", ctypes.wintypes.FLOAT), # Ownship speed brake position 0 = closed, 1 = 60 Degrees open
        ("epuFuel", ctypes.wintypes.FLOAT), # Ownship EPU fuel (Percent 0-100)
        ("oilPressure", ctypes.wintypes.FLOAT), # Ownship Oil Pressure (Percent 0-100)
        ("lightBits", ctypes.wintypes.INT), # Cockpit Indicator Lights, one bit per bulb. See enum

        # These are inputs. Use them carefully
        # NB: these do not work when TrackIR device is enabled
        # NB2: launch falcon with the '-head' command line parameter to activate !
        ("headPitch", ctypes.wintypes.FLOAT), # Head pitch offset from design eye (radians)
        ("headRoll", ctypes.wintypes.FLOAT), # Head roll offset from design eye (radians)
        ("headYaw", ctypes.wintypes.FLOAT), # Head yaw offset from design eye (radians)

        ("lightBits2", ctypes.wintypes.INT), # Cockpit Indicator Lights, one bit per bulb. See enum
        ("lightBits3", ctypes.wintypes.INT), # Cockpit Indicator Lights, one bit per bulb. See enum
        ("ChaffCount", ctypes.wintypes.FLOAT), # Number of Chaff left
        ("FlareCount", ctypes.wintypes.FLOAT), # Number of Flare left
        ("NoseGearPos", ctypes.wintypes.FLOAT), # Position of the nose landinggear; caution: full down values defined in dat files
        ("LeftGearPos", ctypes.wintypes.FLOAT), # Position of the left landinggear; caution: full down values defined in dat files
        ("RightGearPos", ctypes.wintypes.FLOAT), # Position of the right landinggear; caution: full down values defined in dat files
        ("AdiIlsHorPos", ctypes.wintypes.FLOAT), # Position of horizontal ILS bar
        ("AdiIlsVerPos", ctypes.wintypes.FLOAT), # Position of vertical ILS bar
        ("courseState", ctypes.wintypes.INT), # HSI_STA_CRS_STATE
        ("headingState", ctypes.wintypes.INT), # HSI_STA_HDG_STATE
        ("totalStates", ctypes.wintypes.INT), # HSI_STA_TOTAL_STATES; never set
        ("courseDeviation", ctypes.wintypes.FLOAT), # HSI_VAL_CRS_DEVIATION
        ("desiredCourse", ctypes.wintypes.FLOAT), # HSI_VAL_DESIRED_CRS
        ("distanceToBeacon", ctypes.wintypes.FLOAT), # HSI_VAL_DISTANCE_TO_BEACON
        ("bearingToBeacon", ctypes.wintypes.FLOAT), # HSI_VAL_BEARING_TO_BEACON
        ("currentHeading", ctypes.wintypes.FLOAT), # HSI_VAL_CURRENT_HEADING
        ("desiredHeading", ctypes.wintypes.FLOAT), # HSI_VAL_DESIRED_HEADING
        ("deviationLimit", ctypes.wintypes.FLOAT), # HSI_VAL_DEV_LIMIT
        ("halfDeviationLimit", ctypes.wintypes.FLOAT), # HSI_VAL_HALF_DEV_LIMIT
        ("localizerCourse", ctypes.wintypes.FLOAT), # HSI_VAL_LOCALIZER_CRS
        ("airbaseX", ctypes.wintypes.FLOAT), # HSI_VAL_AIRBASE_X
        ("airbaseY", ctypes.wintypes.FLOAT), # HSI_VAL_AIRBASE_Y
        ("totalValues", ctypes.wintypes.FLOAT), # HSI_VAL_TOTAL_VALUES; never set
        ("TrimPitch", ctypes.wintypes.FLOAT), # Value of trim in pitch axis, -0.5 to +0.5
        ("TrimRoll", ctypes.wintypes.FLOAT), # Value of trim in roll axis, -0.5 to +0.5
        ("TrimYaw", ctypes.wintypes.FLOAT), # Value of trim in yaw axis, -0.5 to +0.5
        ("hsiBits", ctypes.wintypes.INT), # HSI flags
        ("DEDLines", (ctypes.c_char*26)*5), #25 usable chars
        ("Invert", (ctypes.c_char*26)*5), #25 usable chars
        ("PFLLines", (ctypes.c_char*26)*5), #25 usable chars
        ("PFLInvert", (ctypes.c_char*26)*5), #25 usable chars
        ("UFCTChan", ctypes.wintypes.INT),
        ("AUXTChan", ctypes.wintypes.INT),
        ("RwrObjectCount", ctypes.wintypes.INT),
        ("RWRsymbol", ctypes.wintypes.INT*40),
        ("bearing", ctypes.wintypes.FLOAT*40),
        ("missileActivity", ctypes.wintypes.ULONG*40),
        ("missileLaunch", ctypes.wintypes.ULONG*40),
        ("selected", ctypes.wintypes.ULONG*40),
        ("lethality", ctypes.wintypes.FLOAT*40),
        ("newDetection", ctypes.wintypes.ULONG*40),
        ("fwd", ctypes.wintypes.FLOAT),
        ("aft", ctypes.wintypes.FLOAT),
        ("total", ctypes.wintypes.FLOAT),
        ("VersionNum", ctypes.wintypes.INT),
        # New values added here for header file compatibility but not implemented
        ("headX", ctypes.wintypes.FLOAT), # Head X offset from design eye (feet)
        ("headY", ctypes.wintypes.FLOAT), # Head Y offset from design eye (feet)
        ("headZ", ctypes.wintypes.FLOAT), # Head Z offset from design eye (feet)
        ("MainPower", ctypes.wintypes.INT),
    )

class FLIGHTDATA2(ctypes.Structure):
    _fields_ = (
        ("nozzlePos2", ctypes.wintypes.FLOAT),
        ("rpm2", ctypes.wintypes.FLOAT),
        ("ftit2", ctypes.wintypes.FLOAT),
        ("oilPressure2", ctypes.wintypes.FLOAT),
        ("navMode", ctypes.wintypes.BYTE),
        ("AAUZ", ctypes.wintypes.FLOAT),
        ("tacanInfo", ctypes.wintypes.CHAR),

        ("AltCalReading", ctypes.wintypes.INT),
        ("altBits", ctypes.wintypes.INT),
        ("powerBits", ctypes.wintypes.INT),
        ("blinkBits", ctypes.wintypes.INT),

        ("cmdsMode", ctypes.wintypes.INT),
        ("BupUhfPreset", ctypes.wintypes.INT),

        ("BupUhfFreq", ctypes.wintypes.INT),
        ("cabinAlt", ctypes.wintypes.FLOAT),
        ("hydPressureA", ctypes.wintypes.FLOAT),
        ("hydPressureB", ctypes.wintypes.FLOAT),
        ("currentTime", ctypes.wintypes.INT),
        ("vehicleACD", ctypes.wintypes.SHORT),
        ("VersionNum", ctypes.wintypes.INT),

        ("fuelFlow2", ctypes.wintypes.FLOAT),

        ("RwrInfo", ctypes.wintypes.CHAR),
        ("lefPos", ctypes.wintypes.FLOAT),
        ("tefPos", ctypes.wintypes.FLOAT),

        ("vtolPos", ctypes.wintypes.FLOAT),

        ("pilotsOnline", ctypes.wintypes.CHAR),
        ("pilotsCallsign", ctypes.wintypes.CHAR),
        ("pilotsStatus", ctypes.wintypes.CHAR),

        ("bumpIntensity", ctypes.wintypes.FLOAT),

        ("latitude", ctypes.wintypes.FLOAT),
        ("longitude", ctypes.wintypes.FLOAT),

        ("RTT_size", ctypes.wintypes.USHORT),
        ("RTT_area", ctypes.wintypes.USHORT),

        ("iffBackupMode1Digit1", ctypes.wintypes.CHAR),
        ("iffBackupMode1Digit2", ctypes.wintypes.CHAR),
        ("iffBackupMode3Digit1", ctypes.wintypes.CHAR),
        ("iffBackupMode3Digit2", ctypes.wintypes.CHAR),

        ("instrLight", ctypes.wintypes.CHAR),

        ("bettyBits", ctypes.wintypes.UINT),
        ("miscBits", ctypes.wintypes.UINT),
        ("RALT", ctypes.wintypes.FLOAT),
        ("bingoFuel", ctypes.wintypes.FLOAT),
        ("caraAlow", ctypes.wintypes.FLOAT),
        ("bullseyeX", ctypes.wintypes.FLOAT),
        ("bullseyeY", ctypes.wintypes.FLOAT),
        ("BMSVersionMajor", ctypes.wintypes.INT),
        ("BMSVersionMinor", ctypes.wintypes.INT),
        ("BMSVersionMicro", ctypes.wintypes.INT),
        ("BMSBuildNumber", ctypes.wintypes.INT),
        ("StringAreaSize", ctypes.wintypes.UINT),
        ("StringAreaTime", ctypes.wintypes.UINT),
        ("DrawingAreaSize", ctypes.wintypes.UINT),

        ("turnRate", ctypes.wintypes.FLOAT),
)

_log = logging.getLogger(__name__)
_pFlightData = None
_pFlightData2 = None
_pOSBData = None

def getFlightData():

    global _pFlightData

    if _pFlightData == None:

        handle = ctypes.windll.kernel32.OpenFileMappingA(FILE_MAP_READ|FILE_MAP_WRITE, False, "FalconSharedMemoryArea".encode())
        if handle:
            ctypes.windll.kernel32.MapViewOfFile.restype = ctypes.POINTER(FLIGHTDATA)
            _pFlightData = ctypes.windll.kernel32.MapViewOfFile(handle, FILE_MAP_READ|FILE_MAP_WRITE, 0, 0, 0)

    if _pFlightData == None:
        raise EnvironmentError("can't access falcon shared memory area")

    return _pFlightData.contents

def getOSBData():
    global _pOSBData

    if _pOSBData == None:

        handle = ctypes.windll.kernel32.OpenFileMappingA(FILE_MAP_READ|FILE_MAP_WRITE, False, "FalconSharedOsbMemoryArea".encode())
        if handle:
            ctypes.windll.kernel32.MapViewOfFile.restype = ctypes.POINTER(OSBDATA)
            _pOSBData = ctypes.windll.kernel32.MapViewOfFile(handle, FILE_MAP_READ|FILE_MAP_WRITE, 0, 0, 0)

    if not _pOSBData:
        raise EnvironmentError("can't access falcon shared memory area")

    return _pOSBData.contents

def getFlightData2():    

    global _pFlightData2

    if _pFlightData2 == None:

        handle = ctypes.windll.kernel32.OpenFileMappingA(FILE_MAP_READ|FILE_MAP_WRITE, False, "FalconSharedMemoryArea2".encode())
        if handle:
            ctypes.windll.kernel32.MapViewOfFile.restype = ctypes.POINTER(FLIGHTDATA2)
            _pFlightData2 = ctypes.windll.kernel32.MapViewOfFile(handle, FILE_MAP_READ|FILE_MAP_WRITE, 0, 0, 0)

    if not _pFlightData2:
        raise EnvironmentError("can't access falcon shared memory area")

    return _pFlightData2.contents

print(getFlightData2().pilotsStatus)

Thanks for this neat utility. I would have never figured out myself how to access Falcon BMS' shared memory via Python without it.

[nmeier]

Hi

I reviewed up to pilotsStatus, and believe you have to use the multipliers for the array lengths. After that the fields might be from a newer version of FlightData.h? Where can I see the latest?

Nils

redacted

[dglava]

Here's a link to a copy of version 4.35 FlightData.h: https://gist.github.com/dglava/55a823cb6d8f899f11790b2a4c3e4356

Thanks for looking into this.

[nmeier]

ok, try the struct description in my post https://github.com/nmeier/simscript/issues/2#issuecomment-885982638, that looks right atm

[dglava]

I have tried it, but I'm still getting weird data. I tried a few things:

• "caraAlow" is giving me"1.3508517196091237e-42" instead of the CARA ALOW value.
• "turnRate" is giving me constantly 0.0

But then stuff like "cmdsMode" seems to give me the correct data. Do you reckon it's an issue with the FlightData2 class or with the shared memory in Falcon BMS itself?

[nmeier]

Ok, found another mistake that would break anything after RTT_*, see below

class FLIGHTDATA2(ctypes.Structure):
    _fields_ = (
        ("nozzlePos2", ctypes.wintypes.FLOAT),
        ("rpm2", ctypes.wintypes.FLOAT),
        ("ftit2", ctypes.wintypes.FLOAT),
        ("oilPressure2", ctypes.wintypes.FLOAT),
        ("navMode", ctypes.wintypes.BYTE),
        ("AAUZ", ctypes.wintypes.FLOAT),
        ("tacanInfo", ctypes.wintypes.CHAR * 2),

        ("AltCalReading", ctypes.wintypes.INT),
        ("altBits", ctypes.wintypes.INT),
        ("powerBits", ctypes.wintypes.INT),
        ("blinkBits", ctypes.wintypes.INT),

        ("cmdsMode", ctypes.wintypes.INT),
        ("BupUhfPreset", ctypes.wintypes.INT),

        ("BupUhfFreq", ctypes.wintypes.INT),
        ("cabinAlt", ctypes.wintypes.FLOAT),
        ("hydPressureA", ctypes.wintypes.FLOAT),
        ("hydPressureB", ctypes.wintypes.FLOAT),
        ("currentTime", ctypes.wintypes.INT),
        ("vehicleACD", ctypes.wintypes.SHORT),
        ("VersionNum", ctypes.wintypes.INT),

        ("fuelFlow2", ctypes.wintypes.FLOAT),

        ("RwrInfo", ctypes.wintypes.CHAR * 512),
        ("lefPos", ctypes.wintypes.FLOAT),
        ("tefPos", ctypes.wintypes.FLOAT),

        ("vtolPos", ctypes.wintypes.FLOAT),

        ("pilotsOnline", ctypes.wintypes.CHAR),
        ("pilotsCallsign", ctypes.wintypes.CHAR * 32 * 12),
        ("pilotsStatus", ctypes.wintypes.CHAR * 32),

        ("bumpIntensity", ctypes.wintypes.FLOAT),

        ("latitude", ctypes.wintypes.FLOAT),
        ("longitude", ctypes.wintypes.FLOAT),

        ("RTT_size", ctypes.wintypes.USHORT * 2),
        ("RTT_area", ctypes.wintypes.USHORT) * 7 * 4,

        ("iffBackupMode1Digit1", ctypes.wintypes.CHAR),
        ("iffBackupMode1Digit2", ctypes.wintypes.CHAR),
        ("iffBackupMode3Digit1", ctypes.wintypes.CHAR),
        ("iffBackupMode3Digit2", ctypes.wintypes.CHAR),

        ("instrLight", ctypes.wintypes.CHAR),

        ("bettyBits", ctypes.wintypes.UINT),
        ("miscBits", ctypes.wintypes.UINT),
        ("RALT", ctypes.wintypes.FLOAT),
        ("bingoFuel", ctypes.wintypes.FLOAT),
        ("caraAlow", ctypes.wintypes.FLOAT),
        ("bullseyeX", ctypes.wintypes.FLOAT),
        ("bullseyeY", ctypes.wintypes.FLOAT),
        ("BMSVersionMajor", ctypes.wintypes.INT),
        ("BMSVersionMinor", ctypes.wintypes.INT),
        ("BMSVersionMicro", ctypes.wintypes.INT),
        ("BMSBuildNumber", ctypes.wintypes.INT),
        ("StringAreaSize", ctypes.wintypes.UINT),
        ("StringAreaTime", ctypes.wintypes.UINT),
        ("DrawingAreaSize", ctypes.wintypes.UINT),

        ("turnRate", ctypes.wintypes.FLOAT),
)

[dglava]

Thanks, it's working!

Sorry for bothering you, but would you also know why this additional Falcon BMS shared memory part isn't working when trying to access it? It's the IntelliVibe values which can be seen in the "IVibe" tab inside Falcon BMS shared memory viewer. It's not documented in the FlightData.h file. Here's a related thread and the only documentation I could find.

I have created a new class and defined those fields according to the info above. The first few ones (BYTE and INT) are working, but the BOOL fields aren't.

Here's what I have:

class IVDATA(ctypes.Structure):
    _fields_ = (
        ("AAMissileFired", ctypes.wintypes.BYTE),
        ("AGMissileFired", ctypes.wintypes.BYTE),
        ("BombDropped", ctypes.wintypes.BYTE),
        ("FlareDropped", ctypes.wintypes.BYTE),
        ("ChaffDropped", ctypes.wintypes.BYTE),
        ("BulletsFired", ctypes.wintypes.BYTE),
        ("CollisionCounter", ctypes.wintypes.INT),
        ("IsFiringGun", ctypes.wintypes.BOOL),
        ("IsEndFlight", ctypes.wintypes.BOOL),
        ("IsEjecting", ctypes.wintypes.BOOL),
        ("In3D", ctypes.wintypes.BOOL),
        ("IsPaused", ctypes.wintypes.BOOL),
        ("IsFrozen", ctypes.wintypes.BOOL),
        ("IsOverG", ctypes.wintypes.BOOL),
        ("IsOnGround", ctypes.wintypes.BOOL),
        ("IsExitGame", ctypes.wintypes.BOOL),
        ("Gforce", ctypes.wintypes.FLOAT),
        ("eyex", ctypes.wintypes.FLOAT),
        ("eyey", ctypes.wintypes.FLOAT),
        ("eyez", ctypes.wintypes.FLOAT),
        ("lastdamage", ctypes.wintypes.INT),
        ("damageforce", ctypes.wintypes.FLOAT),
        ("whendamage", ctypes.wintypes.INT)
)

def getIV():
    global _pIV

    if _pIV == None:

        handle = ctypes.windll.kernel32.OpenFileMappingA(FILE_MAP_READ|FILE_MAP_WRITE, False, "FalconIntellivibeSharedMemoryArea".encode())
        if handle:
            ctypes.windll.kernel32.MapViewOfFile.restype = ctypes.POINTER(IVDATA)
            _pIV = ctypes.windll.kernel32.MapViewOfFile(handle, FILE_MAP_READ|FILE_MAP_WRITE, 0, 0, 0)

    if not _pIV:
        raise EnvironmentError("can't access falcon shared memory area")

    return _pIV.contents

When I do print(getIV().In3D) it's giving me 1065307441 instead of something resembling a boolean value. I don't know anything about this really, but was wondering if it could have something to do with this?

[nmeier]

Glad it works, can you create a pull request so your shared memory area 2 ends up in code?

For your additional example try ctypes.wintypes.BOOLEAN (not BOOL which seems to be a long)

[dglava]

Using BOOLEAN instead of BOOL fixed it!