common.xml Sensor and DSC control loads. Sensor DSC Load Control DSC Load Battery Voltage in millivolts Air data for altitude and airspeed computation. Dynamic pressure (Pa) Static pressure (Pa) Board temperature Accelerometer and gyro biases. Accelerometer X bias (m/s) Accelerometer Y bias (m/s) Accelerometer Z bias (m/s) Gyro X bias (rad/s) Gyro Y bias (rad/s) Gyro Z bias (rad/s) Configurable diagnostic messages. Diagnostic float 1 Diagnostic float 2 Diagnostic float 3 Diagnostic short 1 Diagnostic short 2 Diagnostic short 3 Pilot console PWM messges. Pilot's console throttle command Pilot's console left aileron command Pilot's console right aileron command Pilot's console rudder command Pilot's console elevator command PWM Commands from the AP to the control surfaces. AutoPilot's throttle command AutoPilot's left aileron command AutoPilot's right aileron command AutoPilot's rudder command AutoPilot's left elevator command AutoPilot's right elevator command AutoPilot's left flap command AutoPilot's right flap command AutoPilot's aux1 command AutoPilot's aux2 command Data used in the navigation algorithm. Measured Airspeed prior to the Nav Filter Commanded Roll Commanded Pitch Commanded Turn rate Y component of the body acceleration Total Distance to Run on this leg of Navigation Remaining distance to Run on this leg of Navigation Origin WP Destination WP Configurable data log probes to be used inside Simulink Log value 1 Log value 2 Log value 3 Log value 4 Log value 5 Log value 6 Measured value from the IMU in units after sensor calibration and temperature compensation. Note that this IS NOT the output of the attitude filter, for that see messages 30 and 33. Accelerometer X value (m/s^2) Accelerometer Y value (m/s^2) Accelerometer Z value (m/s^2) Gyro X value (rad/s) Gyro Y value (rad/s) Gyro Z value (rad/s) Magnetometer X (normalized to 1) Magnetometer Y (normalized to 1) Magnetometer Z (normalized to 1) Pilot console PWM messges. Year reported by Gps Month reported by Gps Day reported by Gps Hour reported by Gps Min reported by Gps Sec reported by Gps Visible sattelites reported by Gps Mid Level commands sent from the GS to the autopilot. These are only sent when being opperated in mid-level commands mode from the ground; for periodic report of these commands generated from the autopilot see message XXXX. The system setting the commands Commanded Airspeed Log value 2 Log value 3 This message configures the Selective Passthrough mode. it allows to select which control surfaces the Pilot can control from his console. It is implemented as a bitfield as follows: Position Bit Code ================================= 15-8 Reserved 7 dt_pass 128 6 dla_pass 64 5 dra_pass 32 4 dr_pass 16 3 dle_pass 8 2 dre_pass 4 1 dlf_pass 2 0 drf_pass 1 Where Bit 15 is the MSb. 0 = AP has control of the surface; 1 = Pilot Console has control of the surface. The system setting the commands Bitfield containing the PT configuration Configure a PID loop. The system setting the PID values Proportional gain Integral gain Derivative gain PID loop index Action messages focused on the SLUGS AP. The system reporting the action Action ID. See apDefinitions.h in the SLUGS /clib directory for the ID names Value associated with the action