SMG AircraftPlatform

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The SMG_AircraftPlatform logic component handles the aircraft platfrom module.

Type: Logic Object Component
File: SMG_AircraftPlatform.slc
Version: 450.1000.355.1


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Icon properties.png Properties

NameDescriptionMaxValueMinValueDisplayNameUnitTypeUnitName
PROP_AC_AERO_DATA_FILENAME  The aerodynamic data file name    File System  File 
PROP_AC_AEROELASTIC_DATA_FILENAME  The aeroelastic data file name    File System  File 
PROP_AC_AUTO_PITCH_TRIM_GAIN  The rate in which the trim system tries to eliminate the pitch rate  1000    Default  Default 
PROP_AC_CG_AUGMENTATION  The length to move the CG forward [m]     Default  Default 
PROP_AC_GENERAL_PARAMS_FILENAME  The general params filename    File System  File 
PROP_AC_ICING_EFFECT_PCT  The icing effect initial percentage  100    Default  Default 
PROP_AC_INITIAL_ELEVATOR_TRIM_PCT  The initial elevator trim percentage (-100 to 100)  100  -100  ElevatorTrim  Default  Default 
PROP_AC_INITIAL_FLAPS_STAGE  The initial flaps stage according to the defined stages in the parameters file    Default  Default 
PROP_AC_INITIAL_RUDDER_TRIM_PCT  The initial rudder trim percentage (-100 to 100)  100  -100  Rudder Trim  Default  Default 
PROP_AC_IS_AUTO_PITCH_TRIM  Is to use auto-pitch trim system?    Default  Default 
PROP_AC_IS_TO_ADD_PAYLOAD_EFFECT  Is to take into consideration the external and internal payload?    Default  Default 
PROP_AC_IS_TO_INCLUDE_PAYLOAD_ASSYMETRY  Is to include asssymetric loadout effect?    Default  Default 
PROP_AC_IS_TO_USE_AEROELASTIC_EFFECT  Is to include data of Aeroelastic effect?    Default  Default 
PROP_AC_IS_TO_USE_BILINEAR_STEERING  Is to use the bi-linear stick definitions for steering?    Default  Default 
PROP_AC_IS_TO_USE_SURFACES_LIMITS_FILE  Is to use steering surfaces definitions from file?    Default  Default 
PROP_AC_SURFACES_LIMITS_FILENAME  The file that is used to define the steering surfaces limitations     File System  File 
PROP_AC_UPDATE_DT_STEP  Update step    Default  Default 
PROP_AGL_HEIGHT  Object AGL Height.  AGL Height  Default  Default 
PROP_HEADING  Object heading  360  Heading  Default  Default 
PROP_INITIAL_TRUE_AIR_SPEED  The initial airspeed  1000  TAS (kts)  Default  Default 
PROP_IS_AGL  Indicates if PROP_AGL_HEIGHT should be used.  Use AGL height  Default  Default 
PROP_IS_ENGINE_ON_ON_GROUND_ON_START  Is the engine on when starting on ground?  Is Engine On On Ground On Start  Default  Default 
PROP_LATITUDE  Object Latitude  Latitude  Default  Default 
PROP_LONGITUDE  Object Longitude  Longitude  Default  Default 
PROP_WING_TIP_TRAIL_NAME  The name of the trail for wing-tip effect    Default  Default 
PROP_XPOSITION  Object X Position    Default  Default 
PROP_YPOSITION  Object Y Position    Default  Default 
PROP_ZPOSITION  Object Z Position  Altitude  Default  Default 

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Icon attributes.png Attributes

NameDescriptionParam1Param2DisplayNameUnitTypeUnitName
ATT_ABS_VELOCITY  Absolute velocity  float &      Speed  Meter Per Second 
ATT_AC_AOA_RATE  The aircraft's AOA rate  float &      Angular Velocity  Degree Per Second 
ATT_AC_ARE_PARKING_BRAKE_ON  Are the parking brakes on  bool &      Default  Default 
ATT_AC_BODY_FORCE  The force applied on the AC body  LinearVec &      Force  Newton 
ATT_AC_BODY_MOMENT  The body moment  LinearVec &      Torque  Newton Meter 
ATT_AC_CA  Axial force coefficient  float &      Default  Default 
ATT_AC_CD  The drag coefficient  float &      Default  Default 
ATT_AC_CL  The lift coefficient  float &      Default  Default 
ATT_AC_CLL  Roll moment coefficient  float &      Default  Default 
ATT_AC_CMM  Pitch moment coefficient  float &      Default  Default 
ATT_AC_CN  Normal force coefficient  float &      Default  Default 
ATT_AC_CNN  Yaw moment coefficient  float &      Default  Default 
ATT_AC_CY  Sid force coefficient  float &      Default  Default 
ATT_AC_DEBUG_PARAM  Debug  const int  float &    Default  Default 
ATT_AC_DYNAMIC_PRESS  The dynamic pressure  float &      Pressure  PA 
ATT_AC_ELEVATOR_LIMITER_MAX_CMD  The elevator limiter maximal command (Push)  float &      Default  Default 
ATT_AC_ELEVATOR_LIMITER_MIN_CMD  The elevator limiter minimal command (Pull)  float &      Default  Default 
ATT_AC_FA  Axial force  float &      Default  Default 
ATT_AC_FLAPS_ANGLE_DEG  The flaps deflection angle [Deg]  float &      Angle  Degree 
ATT_AC_FN  Normal force  float &      Default  Default 
ATT_AC_FUEL_LB_TO_GALLON  The Lb. to Gallon ratio for the used fuel  float &      Default  Default 
ATT_AC_FUEL_SYSTEM_G_THRESHOLD_ACCUMULATING_TIME  The time permitted to fly below the G threshold without hearting the fuel flow  float &      Time  Seconds 
ATT_AC_FUEL_SYSTEM_THRESHOLD_G  The load factor in which below the fuel flow will reduce  float &      Acceleration 
ATT_AC_FY  Side force  float &      Default  Default 
ATT_AC_ICING_EFFECT_PCT  The percentage of the icing effect  int &      Default  Default 
ATT_AC_IS_GROUND_STEER_ON  Indicates if the ground steering is engaged  bool &      Default  Default 
ATT_AC_LWHEEL_BRAKE_CMD  The left main wheel brake command  int &      Default  Default 
ATT_AC_MAIN_MOMENT_OF_INERTIA  The main moments of inertia (Ixx, Iyy, Izz) [kg * m *m]  LinearVec &      Default  Default 
ATT_AC_MAX_AILERON_ANGLE  The maximum aileron symmetric deflection [Degs]  float &      Angle  Degree 
ATT_AC_MAX_ELEVATOR_ANGLE  The maximum elevator deflection [Degs]  float &      Angle  Degree 
ATT_AC_MAX_RUDDER_ANGLE  The maximum rudder deflection [Degs]  float &      Angle  Degree 
ATT_AC_MIN_ELEVATOR_ANGLE  The maximum down (nose up) elevator deflection [Degs]  float &      Angle  Degree 
ATT_AC_ML  Roll moment  float &      Default  Default 
ATT_AC_MM  Pitch moment  float &      Default  Default 
ATT_AC_MN  Yaw moment  float &      Default  Default 
ATT_AC_PAYLOADS_TOTAL_MASS  The mass addition of the payloads  float &      Mass  KG 
ATT_AC_PAYLOADS_TOTAL_SCD  The drag addition to the aircraft drag coefficient  float &      Default  Default 
ATT_AC_PROPELLER_STREAM_AIRSPEED  The airspeed behind the propeller disc  float &      Speed  Meter Per Second 
ATT_AC_RUDDER_TRIM_ANGLE  The rudder trim angle  float &      Angle  Degree 
ATT_AC_RWHEEL_BRAKE_CMD  The right main wheel brake command  int &      Default  Default 
ATT_AC_SPECIFIC_POWER  The specific aircraft power (Ps)   float &      Speed  Meter Per Second 
ATT_AC_SPECIFIC_SPEED_ONLY_POWER  The specific aircraft power (Ps - Hdot)   float &      Speed  Meter Per Second 
ATT_AGL_ALT  The altitude above ground level  float &      Length  Meter 
ATT_AIR_REFUELING_CMD  The command of air-refueling [% of max rate]  const int  float &    Default  Default 
ATT_AIR_REFUELING_DESTS  The tanks that are the dests when air refueling: 01 means tanks 0 & 1  const int  string &    Default  Default 
ATT_AIR_REFUELING_MAX_RATES  The maximal air refueling fuel flow [Gal./Hr.]  const int  float &    Volume Flow  Gallon Per Hour 
ATT_AIRBREAK_DEFLECTION  The airbreak deflection  float &      Angle  Degree 
ATT_AIRCRAFT_WEIGHT  The weight of the aircraft [KG]  float &      Mass  KG 
ATT_ALTIMETER_ALT  The sea level altitude  float &      Length  Meter 
ATT_ALTIMETER_ALT_FEET  The indicated altitude  float &      Length  Feet 
ATT_ANG_ACCELERATION  ATT_ANG_ACCELERATION  AngularVec &      Default  Default 
ATT_ANG_VELOCITY  ATT_ANG_VELOCITY  AngularVec &      Default  Default 
ATT_ARE_AIR_BRAKES_OPEN  Returns if aircraft air brakes are open  bool &      Default  Default 
ATT_ARE_LANDING_GEAR_RETRACTABLE  Are the gears retractable?  bool &      Default  Default 
ATT_BODY_ACCELERATION  The acceleration in body coordinates  LinearVec &      Acceleration  Meter Per Second Squared 
ATT_BODY_AOA  The aircraft body angle of attack  float &      Angle  Degree 
ATT_BODY_BETA  The aircraft body bank angle  float &      Angle  Degree 
ATT_BODY_VELOCITY  The velocity in body coordinates  LinearVec &      Speed  Meter Per Second 
ATT_CG  The velocity in body coordinates  LinearVec &      Length  Meter 
ATT_CROSS_FEED_CMD  The command to perform cross feed [% of max rate]  const int  float &    Default  Default 
ATT_CROSS_FEED_DESTS  The dests of cross feed 13 are tanks 1 & 3  const int  string &    Default  Default 
ATT_CROSS_FEED_MAX_RATES  The maximal rates for performing cross feed according to the sources & dests arrays  const int  float &    Volume Flow  Gallon Per Hour 
ATT_CROSS_FEED_SOURCES  The source tanks for x-feed 02 are tanks 0 & 2  const int  string &    Default  Default 
ATT_CURR_FUEL_QUANTITIES  The current fuel quantity in each tank [Gal.]  const int  float &    Mass  Metric Ton 
ATT_DEBUG_PARAM  Debugging  const int  float &    Default  Default 
ATT_ELEVATOR_CMD  The elevator cmd (-100 to 100)  int &      Default  Default 
ATT_ELEVATOR_FINE_CMD  1/100 of the elevator cmd - for the AP  int &      Default  Default 
ATT_ELEVATOR_TRIM_ANGLE  The elevator trim angle  float &      Angle  Degree 
ATT_ELEVATOR_TRIM_CMD  The elevator trim (-100 to 100)  int &      Default  Default 
ATT_ENGINE_MAGNETO_LEFT_STATE  For the left magneto view  const int  float &    Default  Default 
ATT_ENGINE_MAGNETO_RIGHT_STATE  For the right magneto view  const int  float &    Default  Default 
ATT_ENGINE_MIXTURE_LEVER_POS  For the mixture view  const int  float &    Default  Default 
ATT_ENGINE_THROTTLE_LEVER_POS  For the throttle view  const int  float &    Default  Default 
ATT_ENGINES_NUMBER  The number of identical engines on the aircraft  int &      Default  Default 
ATT_FEED_ORDER  The feed order : 012 means tanks 0 & 1 & 2 are first  const int  string &    Default  Default 
ATT_FLAPS_DEFLECTION  The Flaps deflection  float &      Angle  Degree 
ATT_FLAPS_REQUIRED_STAGE  The required stage of the flaps  int &      Default  Default 
ATT_FLIGHT_MODEL_EXISTS  To Indicate that a flight model exists  bool &      Default  Default 
ATT_FRONT_SUSPENSION_PCT  The front gear suspension percentage (0 - close, 100 full open)  int &      Default  Default 
ATT_FUEL_DUMP_CMD  The command to perform fuel dump [% of max rate]  const int  float &    Default  Default 
ATT_FUEL_DUMP_MAX_RATES  The maximal fuel flow for fuel dump  const int  float &    Volume Flow  Gallon Per Hour 
ATT_FUEL_DUMP_SOURCES  The tanks that are sources for fuel dump  const int  string &    Default  Default 
ATT_FUEL_TANKS_CAPACITY  The fuel tanks capacities [Gal.]  const int  float &    Mass  Metric Ton 
ATT_FUEL_TANKS_NO  The number of fuel tanks in the fuel system  int &      Default  Default 
ATT_GROUND_SPEED_KNOTS  The aircraft ground speed in knots [Knots]  float &      Speed  Knots 
ATT_GROUND_VEL_IN_BODY  The ground velocity of the aircraft in body coordinates  LinearVec &      Speed  Meter Per Second 
ATT_HEADING_DOT  The heading changing rate [deg/sec]  float &      Angular Velocity  Degree Per Second 
ATT_HEIGHT  ATT_HEIGHT  float &      Length  Meter 
ATT_HEIGHT_ABOVE_GROUND_FEET  Return height above ground [ft]  float &      Length  Feet 
ATT_HEIGHT_ABOVE_LOWER_THOUSAND_FEET  The number of feet from the lower thousand feet [Ft]  float &      Length  Feet 
ATT_HEIGHT_FEET  The height msl [ft]  float &      Length  Feet 
ATT_INDICATED_AIRSPEED  the indicated air velocity  float &      Speed  Meter Per Second 
ATT_INDICATED_AIRSPEED_KNOTS  The indicated air velocity [knots]  float &      Speed  Knots 
ATT_IS_FLAPERON  Are the flaps part of the aileron mechanism?  bool &      Default  Default 
ATT_IS_IN_MANEUVER_MODE  True if the aircraft is in maneuver mode  bool &      Default  Default 
ATT_IS_IN_MOTION  Is in motion? Boolean answer.  bool &      Default  Default 
ATT_IS_LANDING_GEARS_HANDLE_UP  The landing gear handle position  bool &      Default  Default 
ATT_IS_MOTION_MODEL_UNIT  Is this SLC a part of the object's motion model?  bool &      Default  Default 
ATT_IS_ON_GROUND  Is the aircraft on the ground?  bool &      Default  Default 
ATT_IS_WHEEL_STEER_ENABLED  Is the ground steering wheel enabled?  bool &      Default  Default 
ATT_IS_WINGTIPS_SMOGE  Returns the aircraft wing tips state  bool &      Default  Default 
ATT_LAST_ADDED_PAYLOAD_INDEX  The index of the last added payload  int &      Default  Default 
ATT_LATITUDE  Entity Latitude [rad]  double &      Angle  Radian 
ATT_LIN_ACCELERATION  The velocity in world coordinates  LinearVec &      Acceleration  Meter Per Second Squared 
ATT_LIN_VELOCITY  The velocity in world coordinates  LinearVec &      Speed  Meter Per Second 
ATT_LMAIN_SUSPENSION_PCT  The left main gear suspension percentage (0 - close, 100 full open)  int &      Default  Default 
ATT_LOAD_FACTOR  The load factor of the aircraft (g)  float &      Acceleration 
ATT_LOCATION  Location (x,y,z,pitch,roll,yaw)  Location &      Coordinate System  Local 
ATT_LONGITUDE  Entity Longitude [rad]  double &      Angle  Radian 
ATT_MACH_NO  The mach number of the aircraft  float &      Default  Default 
ATT_ORIENTATION  Orientation (pitch,roll,yaw)  AngularVec &      Default  Default 
ATT_ORIENTATION_DOT  Orientation dot (pitch,roll,yaw)  AngularVec &      Default  Default 
ATT_OUT_OF_FUEL  Is out of fuel?  bool &      Default  Default 
ATT_OUTSIDE_AIR_TEMPERATURE  The outside air temperature [oC]  float &      Temperature  Celsius 
ATT_POSITION  Position (x,y,z)  LinearVec &      Coordinate System  Local 
ATT_RMAIN_SUSPENSION_PCT  The right main gear suspension percentage (0 - close, 100 full open)  int &      Default  Default 
ATT_ROLL_CMD  The roll comand (ailerons) (-100 to 100)  int &      Default  Default 
ATT_ROLL_FINE_CMD  1/100 of the roll comand - for the AP  int &      Default  Default 
ATT_RUDDER_CMD  The rudder cmd (-100 to 100)  int &      Default  Default 
ATT_RUDDER_FINE_CMD  1/100 of the rudder cmd - for the AP  int &      Default  Default 
ATT_SIDESLIP_ANGLE_RAD  The sideslip angle  float &      Angle  Radian 
ATT_SUBPART_ANG_AIRBRAKE  The subpart angle of the airbrake  float &      Angle  Radian 
ATT_SUBPART_ANG_FLAPS  The flaps subpart angle  float &      Angle  Radian 
ATT_SUBPART_ANG_LEFT_AILRON  The subpart angle of the left ailron  float &      Angle  Radian 
ATT_SUBPART_ANG_LEFT_ELEVATORS  The subpart angle of the left elevators  float &      Angle  Radian 
ATT_SUBPART_ANG_LEFT_RUDDER  The subpart angle of the left rudder  float &      Angle  Radian 
ATT_SUBPART_ANG_RIGHT_AILRON  The subpart angle of the right ailron  float &      Angle  Radian 
ATT_SUBPART_ANG_RIGHT_ELEVATORS  The subpart angle of the right elevators  float &      Angle  Radian 
ATT_SUBPART_ANG_RIGHT_RUDDER  The subpart angle of the right rudder  float &      Angle  Radian 
ATT_SUBPART_ANG_STEERING_WHEEL  flaps  float &      Angle  Radian 
ATT_SUBPART_FRONTGEARZ_ABOVE_GROUND  Z position of the front gear subpart - for inside the ground  float &      Length  Meter 
ATT_SUBPART_GROUND_STEER_ANG  The steering wheel deflection  float &      Angle  Radian 
ATT_SUBPART_LMAINGEARZ_ABOVE_GROUND  Z position of the left main gear subpart - for inside the ground  float &      Length  Meter 
ATT_SUBPART_RMAINGEARZ_ABOVE_GROUND  Z position of the right main gear subpart - for inside the ground  float &      Length  Meter 
ATT_SUBPART_VISIBLE_PIPE  Get subpart visible status (PIPE_A==0 || PIPE_B==1 || ...)   int &      Default  Default 
ATT_TRUE_AIR_SPEED_KNOTS  Return entity velocity - TAS [knots]  float &      Speed  Knots 
ATT_TRUE_AIRSPEED  Returns the aircraft true AirSpeed [m/s]  float &      Speed  Meter Per Second 
ATT_TRUE_AIRSPEED_KNOTS  The true air velocity  float &      Speed  Knots 
ATT_TRUE_COURSE  The aircraft true ground course [degs]   float &      Angle  Degree 
ATT_TRUE_HEADING  The true heading  float &      Angle  Degree 
ATT_TURN_RATE  The turn rate [Deg / Sec]  float &      Angular Velocity  Degree Per Second 
ATT_VERTICAL_VELOCITY  The vertical velocity  float &      Speed  Meter Per Second 
ATT_WHEEL_BREAK_CMD  The wheel break cmd (0 to 100)  int &      Default  Default 
ATT_WIND_DRIFT_ANGLE  The wind drift angle   float &      Default  Default 

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Icon actions.png Actions

NameDescriptionParam1Param2DisplayNameUnitTypeUnitName
ACTION_AC_SET_AILERON_CMD  Sets the aileron command  const int      Default  Default 
ACTION_AC_SET_AILERON_FINE_CMD  Sets the aileron fine command (-100 to 100)  const int      Default  Default 
ACTION_AC_SET_BOTH_WHEELS_BRAKE_CMD  Sets the brake command for Left+Right main wheels  const int      Default  Default 
ACTION_AC_SET_ELEV_CMD  Sets the command to the elevator (-100 to 100)  const int      Default  Default 
ACTION_AC_SET_ELEV_FINE_CMD  Sets the elevator fine command (-100 to 100)  const int      Default  Default 
ACTION_AC_SET_ELEVATOR_TRIM_PCT  Sets the elevator trim percentage (-100 to 100)  const float      Default  Default 
ACTION_AC_SET_FLIGHT_HEADING  Sets the flight heading  const float      Angle  Degree 
ACTION_AC_SET_ICING_PCT  Sets the icing conditions percentage  const float      Default  Default 
ACTION_AC_SET_INDICATED_AIRSPEED  Sets indicated airspeed  const float      Speed  Knots 
ACTION_AC_SET_PARKING_BRAKES  Engages/Disengages the parking brakes  const bool      Default  Default 
ACTION_AC_SET_REQUIRED_FLAPS_ANGLE  Sets the required flaps angle  const float      Angle  Degree 
ACTION_AC_SET_RUDDER_CMD  Sets the rudder command (-100 to 100)  const int      Default  Default 
ACTION_AC_SET_RUDDER_TRIM_PCT  Sets the rudder trim percentage (-100 to 100)  const float      Default  Default 
ACTION_ADD_PAYLOAD  Adds a payload. The new payload index is published in ATT_LAST_ADDED_PAYLOAD_INDEX.        Default  Default 
ACTION_REMOVE_PAYLOAD  Removed a previously added payload  const int      Default  Default 
ACTION_SET_PAYLOAD_BODY_POSITION  Sets the body position of the added payload [m]  const int  const LinearVec &    Default  Default 
ACTION_SET_PAYLOAD_MASS  Sets the mass of the added payload [Kg]  const int  const float    Default  Default 
ACTION_SET_PAYLOAD_SCD  Sets the drag coefficient of the added payload  const int  const float    Default  Default 
ACTION_START_FLIGHT_MOTION_MODEL  Start model motion  const Location &  const LinearVec &    Default  Default 
INPUT_AC_AIRBRAKE_IN_ONE_STEP  Airbrake in one step  const int  const int    Default  Default 
INPUT_AC_AIRBRAKE_OUT_ONE_STEP  Airbrake out one step  const int  const int    Default  Default 
INPUT_AC_ELEV_TRIM_NOSE_DOWN  Add to the nose down trim  const int  const int    Default  Default 
INPUT_AC_ELEV_TRIM_NOSE_DOWN_RELEASE  Release of the aircraft elevation trim nose down  const int  const int    Default  Default 
INPUT_AC_ELEV_TRIM_NOSE_UP  Add to the nose up trim  const int  const int    Default  Default 
INPUT_AC_ELEV_TRIM_NOSE_UP_RELEASE  Release of the aircraft elevation trim nose up  const int  const int    Default  Default 
INPUT_AC_ELEVATOR_TRIM_NOSE_UP|INPUT_AC_ELEVATOR_TRIM_NOSE_DOWN  Elevator trim nose up / nose down  const int  const int    Default  Default 
INPUT_AC_EXTRACT_AIRBRAKE_ANGLE|INPUT_AC_RETRACT_AIRBRAKE_ANGLE  Continuously extract the airbrake angle as long as the key is pressed  const int  const int    Default  Default 
INPUT_AC_FLAPS_DOWN_ONE_STEP  Lower the flaps one step  const int  const int    Default  Default 
INPUT_AC_FLAPS_UP_ONE_STEP  Raise the flaps one step  const int  const int    Default  Default 
INPUT_AC_FULL_BRAKES_PRESS  Applies 100% of braking command  const int  const int    Default  Default 
INPUT_AC_FULL_BRAKES_RELEASE  Release the 100% brakes press  const int  const int    Default  Default 
INPUT_AC_GROUND_STEER_OFF  Disengages the ground steer  const int  const int    Default  Default 
INPUT_AC_GROUND_STEER_ON  Engages the ground steering  const int  const int    Default  Default 
INPUT_AC_LMAIN_WHEEL_BRAKE|INPUT_AC_LMAIN_WHEEL_BRAKE2  Left wheel brake  const int  const int    Default  Default 
INPUT_AC_LOWER_FLAPS_ANGLE_PRESS  Lowering the flaps continuously  const int  const int    Default  Default 
INPUT_AC_LOWER_FLAPS_ANGLE_RELEASE  Lowering the flaps continuously release  const int  const int    Default  Default 
INPUT_AC_LOWER_FLAPS_ANGLE|INPUT_AC_RAISE_FLAPS_ANGLE  Continuously lowering the flaps angle as long as the key is pressed  const int  const int    Default  Default 
INPUT_AC_PARKING_BRAKE_TOGGLE  Parking brake on/off  const int  const int    Default  Default 
INPUT_AC_RAISE_FLAPS_ANGLE_PRESS  Raising the flaps continuously  const int  const int    Default  Default 
INPUT_AC_RAISE_FLAPS_ANGLE_RELEASE  Raising the flaps continuously release  const int  const int    Default  Default 
INPUT_AC_RMAIN_WHEEL_BRAKE|INPUT_AC_RMAIN_WHEEL_BRAKE2  Right wheel brake  const int  const int    Default  Default 
INPUT_AC_RUDDER_TRIM_LEFT_PRESS  Adds left rudder trim according to the rate defined  const int  const int    Default  Default 
INPUT_AC_RUDDER_TRIM_LEFT_RELEASE  Stops left rudder trim  const int  const int    Default  Default 
INPUT_AC_RUDDER_TRIM_RIGHT_PRESS  Adds right rudder trim according to the rate defined  const int  const int    Default  Default 
INPUT_AC_RUDDER_TRIM_RIGHT_RELEASE  Stops right rudder trim  const int  const int    Default  Default 
INPUT_GEARS_IN_CMD  retract gears  const int  const int    Default  Default 
INPUT_GEARS_OUT_CMD  extend gears  const int  const int    Default  Default 
INPUT_STARTER_MAGNETO_ADD_CMD  Add to the starter state  const int  const int    Default  Default 
INPUT_STARTER_MAGNETO_REDUCE_CMD  Reduces the starter state  const int  const int    Default  Default 
ACTION_ENABLE_FLIGHT_MODEL  Enables / disables the flight model  const bool      Default  Default 

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Icon attributes.png Required Attributes

Name
ATT_3D_OBJECT_HANDLE 
ATT_ALTIMETER_BARO_PRESSURE 
ATT_ARE_LANDING_GEARS_DOWN 
ATT_ENGINE_NUMBER_OF_STARTER_STAGES 
ATT_ENGINE_STARTER_STATE 
ATT_ENGINE_THRUST 
ATT_FLAPS_CURRENT_STAGE 
ATT_FLAPS_TRANSITION_TIME 
ATT_HEIGHT_ABOVE_GROUND 
ATT_IS_MOTION_MODEL_ENABLED 
ATT_IS_TO_STOP_HIGH_LEVEL_MODEL 
ATT_LANDING_GEAR_DOWN_PCT 
ATT_MANEUVERS_STACK_POINTER 
ATT_NUMBER_OF_LOADED_WEAPONS_BY_NAME 
ATT_NUMBER_OF_WEAPONS_BY_TYPE 
ATT_PROPELLER_DIAMETER 
ATT_REQUIRED_FLAPS_ANGLE 
ATT_SMS_NUMBER_OF_PHYSICAL_STATIONS 
ATT_STEER_IS_PITCH_AUTO_TRIM_ON 
ATT_WEAPON_IDS_ON_STATION 

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Icon actions.png Required Actions

Name
ACTION_AP_SET_HDG 
ACTION_AP_SET_ON 
ACTION_AP_SET_SPEED 
ACTION_EXTRACT_GEARS 
ACTION_PLAY_GEAR_TOUCH_SOUND 
ACTION_RETRACT_GEARS 
ACTION_SET_DAMAGE 

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