TypeIDNameUnits/ValuesDescription
32 VAR0IAS (Indicated Air Speed)m/sPitot-static measurement speed
1TAS (True Air Speed)m/sSpeed relative to the airmass in which the vehicle is moving (IAS measurement corrected with Standard Atmosphere data)
2GS (Ground Speed)m/sHorizontal speed, relative to the ground
3HeadingradianDirection in which the vehicle velocity vector is pointing
4Flight Path AngleradianAngle between velocity vector and local horizontal line
5BankradianVelocity vector lateral component
6YawradianAngle around the Vertical axis of the vehicle
7PitchradianAngle around the Transverse axis of the vehicle
8RollradianAngle around the Longitudinal axis of the vehicle
9Along-Track ErrormFix error along the flight track
10Cross-Track ErrormFix error across the flight track
11Vertical-Track ErrormFix error in the vertical flight track
12Roll Raterad/s (RDS)Rate of change of the Roll angle
13Pitch Raterad/s (RDS)Rate of change of the Pitch angle
14Yaw Raterad/s (RDS)Rate of change of the Yaw angle
15Forward Acceleration – X Body Axism/s²Acceleration in the X axis
16Right Acceleration – Y Body Axism/s²Acceleration in the Y axis
17Bottom Acceleration – Z Body Axism/s²Acceleration in the Z axis
18RPMrad/s (RDS)Revolutions per minute configurable for external sensor
19Front GV (Ground Velocity)m/sGV vector X component
20Lateral GV (Ground Velocity)m/sGV vector Y component
21Velocitym/sVelocity vector modul
22Forward Load Factor – X Body AxiscustomTypeG-force in X body axis
23Right Load Factor – Y Body AxiscustomTypeG-force in Y body axis
24Bottom Load Factor – Z Body AxiscustomTypeG-force in Z body axis
25Tangential Accelerationm/s²Absolute acceleration for tangential direction
26Energy RatecustomTypeVariation from system total energy (kinetic & potential)
27Energy DistributioncustomTypeDivision of energy used between kinetic and potential
28co-yawradianAcrobatic Yaw with Body Z’ axis pointing to X
29co-pitchradianAcrobatic Pitch with Body X’ axis pointing to -Z
30co-rollradianAcrobatic Roll with Y’ keeping same as Y
31Roll accelerationradian/s²Acceleration around the longitudinal axis
32Pitch accelerationradian/s²Acceleration around the transverse axis
33Yaw Accelerationradian/s²Acceleration around the vertical axis
100Desired IAS (Indicated Air Speed)m/sCommanded IAS from guidance
101Desired TAS (True Air Speed)m/sCommanded TAS from guidance
102Desired GS (Ground Speed)m/sCommanded GS from guidance
103Desired HeadingradianCommanded Heading from guidance
104Desired Flight Path AngleradianCommanded Flight Path Angle from guidance
105Desired BankradianCommanded Bank from guidance
106Desired YawradianCommanded Yaw from guidance
107Desired PitchradianCommanded Pitch from guidance
108Desired RollradianCommanded Roll from guidance
109Desired Along-Track ErrormCommanded Along-Track error from guidance
110Desired Cross-Track ErrormCommanded Cross-Track error from guidance
111Desired Vertical-Track ErrormCommanded Vertical-Track error from guidance
112Desired Roll Raterad/s (RDS)Commanded Roll rate from guidance
113Desired Pitch Raterad/s (RDS)Commanded Pitch rate from guidance
114Desired Yaw Raterad/s (RDS)Commanded Yaw rate from guidance
115Desired Foward Acceleration – X Body Axism/s²Commanded Forward Acceleration from guidance
116Desired Right Acceleration – Y Body Axism/s²Commanded Right Acceleration from guidance
117Desired Bottom Acceleration – Z Body Axism/s²Commanded Bottom Acceleration from guidance
118Desired RPMrad/s (RDS)Commanded RPM from guidance
119Desired Front GV (Ground Velocity)m/sCommanded Front GV from guidance
120Desired Lateral GV (Ground Velocity)m/sCommanded Lateral GV from guidance
121Desired Velocitym/sCommanded Velocity from guidance
122Desired Forward Load Factor – X Body AxiscustomTypeCommanded Forward Load Factor from guidance
123Desired Right Load Factor – Y Body AxiscustomTypeCommanded Right Load Factor from guidance
124Desired Bottom Load Factor – Z Body AxiscustomTypeCommanded Bottom Load Facto from guidance
125Desired Tangential Accelerationm/s²Commanded Tangential Acceleration from guidance
126Desired Energy RatecustomTypeCommanded Energy Rate from guidance
127Desired Energy DistributioncustomTypeCommanded Energy Distribution from guidance
128Desired co-yawradianCommanded co-yaw from guidance
129Desired co-pitchradianCommanded co-pitch from guidance
130Desired co-rollradianCommanded co-roll from guidance
200Desired North GV (Ground Velocity)m/sCommanded North (NED Coordinates system) GV from guidance
201Desired East GV (Ground Velocity)m/sCommanded East (NED Coordinates system) GV from guidance
202Desired Down GV (Ground Velocity)m/sCommanded Down (NED Coordinates system) GV from guidance
203Desired 2D MSL (Heigh Above Mean Sea Level)mCommanded MSL from guidance in 2D height mode
204Desired 2D AGL (Above Ground Level) – HeightmCommanded AGL from guidance in 2D height mode
205Desired 2D WGS84 Elevation (Height Over The Ellipsoid)mCommanded WGS84 Elevation from guidance in 2D height mode
206Desired LongituderadianCommanded Longitude from guidance
207Desired LongituderadianCommanded Lattitude from guidance
208Desired WGS84 Elevation (Height Over The Ellipsoid)mCommanded WGS84 Elevation from guidance
209Desired MSL (Height Above Mean Sea Level) – AltitudemCommanded MSL Altitude from guidance
210Desired AGL (Above Ground Level) – HeightmCommanded AGL Altitude from guidance
251Guidance horizontal position errormDifference from Desired and actual horizontal position
252Guidance vertical positionmDifference from Desired and actual vertical position
254Guidance PID desired horizontal velocitym/sCommanded PID horizontal velocity from guidance
255Guidance PID desired vertical velocitym/sCommanded PID vertical velocity from guidance
256Desired velocity X body axism/sCommanded velocity in X axis from guidance
257Desired velocity Y body axism/sCommanded velocity in Y axis from guidance
258Desired velocity Z body axism/sCommanded velocity in Z axis from guidance
259External yawradianYaw from external navigation source
260External pitchradianPitch from external navigation source
261External rollradianRoll from external navigation source
300Time since Hardware Start-UpsecTime spent since power on of the system
301Used Memory SpaceByteSD used memory space
302Free Memory SpaceByteSD free memory space
303Dynamic PressurepascalPhysical measurement from Pitot
304Static PressurepascalPhysical measurement from Pitot
305Internal Temperaturekelvin (K)Physical measurement from internal sensors
306External Temperaturekelvin (K)Physical measurement from Veronte sensors
307Accelerometer – X Body Axism/s²Accelerometer measurement for X axis
308Accelerometer – Y Body Axism/s²Accelerometer measurement for Y axis
309Accelerometer – Z Body Axism/s²Accelerometer measurement for Z axis
310Gyroscope – X Body Axisrad/s (RDS)Gyroscope measurement for X axis
311Gyroscope – Y Body Axisrad/s (RDS)Gyroscope measurement for Y axis
312Gyroscope – Z Body Axisrad/s (RDS)Gyroscope measurement for Z axis
313Magnetometer – X Body AxisteslaMagnetometer measurement for X axis
314Magnetometer – Y Body AxisteslaMagnetometer measurement for Y axis
315Magnetometer – Z Body AxisteslaMagnetometer measurement for Z axis
322Internal magnetometer raw X in SIteslaMagnetometer raw measurement for X axis
323Internal magnetometer raw Y in SIteslaMagnetometer raw measurement for Y axis
324Internal magnetometer raw Z in SIteslaMagnetometer raw measurement for Z axis
325Internal magnetometer temperaturekelvin (K)Magnetometer temperature
326External LIS3MDL magnetometer raw X in SIteslaLIS3MDL external Magnetometer raw measurement for X axis
327External LIS3MDL magnetometer raw Y in SIteslaLIS3MDL external Magnetometer raw measurement for Y axis
328External LIS3MDL magnetometer raw Z in SIteslaLIS3MDL external Magnetometer raw measurement for Z axis
329External LIS3MDL magnetometer temperaturekelvin (K)LIS3MDL external Magnetometer temperature
330IMU 0 raw accelerometer x measurementm/s²IMU 0 raw accelerometer x measurement
331IMU 0 raw accelerometer y measurementm/s²IMU 0 raw accelerometer y measurement
332IMU 0 raw accelerometer z measurementm/s²IMU 0 raw accelerometer z measurement
333IMU 0 raw gyroscope x measurementrad/s (RDS)IMU 0 raw gyroscope x measurement
334IMU 0 raw gyroscope y measurementrad/s (RDS)IMU 0 raw gyroscope y measurement
335IMU 0 raw gyroscope z measurementrad/s (RDS)IMU 0 raw gyroscope z measurement
336IMU 0 temperature measurementkelvin (K)IMU 0 temperature measurement
337IMU 1 raw accelerometer x measurementm/s²IMU 1 raw accelerometer x measurement
338IMU 1 raw accelerometer y measurementm/s²IMU 1 raw accelerometer y measurement
339IMU 1 raw accelerometer z measurementm/s²IMU 1 raw accelerometer z measurement
340IMU 1 raw gyroscope x measurementrad/s (RDS)IMU 1 raw gyroscope x measurement
341IMU 1 raw gyroscope y measurementrad/s (RDS)IMU 1 raw gyroscope y measurement
342IMU 1 raw gyroscope z measurementrad/s (RDS)IMU 1 raw gyroscope z measurement
343IMU 1 temperature measurementkelvin (K)IMU 1 temperature measurement
344Static pressure sensor 1 raw measurementpascalStatic pressure sensor 1 raw measurement
345Static pressure sensor 1 temperaturekelvin (K)Static pressure sensor 1 temperature
346Dynamic pressure sensor raw measurementpascalDynamic pressure sensor raw measurement
347Dynamic pressure sensor temperaturekelvin (K)Dynamic pressure sensor temperature
348Static pressure sensor 0 raw measurementpascalStatic pressure sensor 0 raw measurement
 349Static pressure sensor 0 temperaturekelvin (K)Static pressure sensor 0 temperature
 400Power InputvoltsPower received by Veronte
 401Power Comicro 3.3VvoltsPower received by Veronte through 3.3V port
 402Power 5VvoltsPower received by Veronte thorugh 5V port
 403Power Comicro RegulatorvoltsPower received by Veronte Comicro Regulator
 404Power 3.6VvoltsPower received by Veronte thorugh 3.6V port
 405CPU Temperaturekelvin (K)Internal computer temperature
 406RSSIdecimalReceived Signal Strength Indicator
 500LongituderadianEast-West geographic coordinate
 501LatituderadianNorth-South geographic coordinate
 502WGS84 Elevation (Height Over the Ellipsoid)mElevation over WGS84 reference frame
 503MSL (Height Above Mean Sea Level) – AltitudemAltitude over the Mean Sea Level
 504AGL (Above Ground Level) – HeightmHeight Above Ground Level – Dependent on external sensors or own models with considerable error
 505Ground Velocity Northm/sGround Velocity component in the North direction (NED Coordinates system)
 506Ground Velocity Eastm/sGround Velocity component in the East direction (NED Coordinates system)
 507Ground Velocity Downm/sGround Velocity component in the resultant axis from North-East (NED Coordinates system)
 508Sensor IAS (Indicated Air Speed)m/sPitot-static measurement speed
 509Angle of Attack – AoAradianAngle between reference body line and flow direction vector
 510SideslipradianAngle between the flow direction vector and the longitudinal axis of the vehicle
 600-603Temperature 1-4kelvin (K)Variables to be configured with external Temperature sensors
 700-705RPM 1-6rad/s (RDS)RPM associated to pulse captured 1-6
 750Selected controller time stepsecPID selected time step
 751Selected controller derivative filtered errorcustomTypePID selected derivative filtered error
 752Selected controller proportional actioncustomTypePID selected proportional action
 753Selected controller derivative actioncustomTypePID selected derivative action
 754Selected controller integral inputcustomTypePID selected integral input
 755Selected controller integral actioncustomTypePID selected integral action
 756Selected controller anti-windup inputcustomTypePID selected anti-windup input
 757Selected controller derivative errorcustomTypePID selected derivative error
 800-815PWM 1-16customTypePulse Width Modulation signal
 900-915Stick Input r1 – r16customTypeRaw stick measurement
 1000-1031Stick Input y1 – y32customTypeServo position commanded from stick
 1100-1104Lidar 1-5 DistancesmVariable configurable for Lidar distances
 1105-1109External range sensor 1-5 measuresmVariable configurable for external range sensors
 1200Cross-track DistancecustomTypeShotest distance to desired path (perpendicular distance)
 1201Radar AGL (Above Ground Level) – HeightmUser Variable
 1202Radar Speed Downm/sUser Variable
 1203External Rotation for Follow Routeradian
 1204Time to Impact with ObstaclessecTime calculated with Distance to Obstacle and travel speed
 1300-1309Clock 1-10secConfigurable timers for automations – CLock 1 correspond to Timer 1, etc
 1400Velocity – X Body Axism/sVelocity vector X component
 1401Velocity – Y Body Axism/sVelocity vector Y component
 1402Velocity – Z Body Axism/sVelocity vector Z component
 1403Estimated Dynamic Pressurepascal
 1404Barometric Pressure at Sea Level (QNH)pascalIntroduced value for QNH
 1450-1453Captured pulse 1-4customTypeInput values from pulses
 1490Internest raw x distancemRaw measurements for X axis internest distance
 1491Internest raw y distancemRaw measurements for Y axis internest distance
 1492Internest raw z distancemRaw measurements for Z axis internest distance
 1493Internest raw angleradianRaw measurements for internest angle
 1494Internest raw xy standard deviationmRaw measurements for XY axis internest standard deviation
 1495Internest raw z standard deviationmRaw measurements for Z axis internest standard deviation
 1496Internest raw angle standard deviationradianRaw measurements for internest angle standard deviation
 1497Internest position update frequencyHzFrequency at which Interest updates its position
 1500GNSS1 Time of WeeksData from GNSS1 modul: Time of the week
 1501GNSS1 ECEF Position XmData from GNSS1 modul: ECEF (Earth-Centered Earth-Fixed coordinate system) position X
 1502GNSS1 ECEF Position YmData from GNSS1 modul: ECEF (Earth-Centered Earth-Fixed coordinate system) position Y
 1503GNSS1 ECEF Position ZmData from GNSS1 modul: ECEF (Earth-Centered Earth-Fixed coordinate system) position Z
 1504GNSS1 LongituderadianData from GNSS1 modul: Longitude
 1505GNSS1 LatituderadianData from GNSS1 modul: Latitude
 1506GNSS1 Height Above Ellipsoid (WGS84)mData from GNSS1 modul: Height Above Ellipsoid (WGS84)
 1507GNSS1 Mean Sea Level (MSL)mData from GNSS1 modul: MSL
 1508GNSS1 Above Ground Level (AGL)mData from GNSS1 modul: AGL
 1509GNSS1 PDOP (Dilution of Precision of Position)customTypeData from GNSS1 modul: PDOP – Relation between user position error and satellite position error
 1510GNSS1 AccuracymData from GNSS1 modul: Accuracy
 1511GNSS1 Horizontal Accuracy EstimatemData from GNSS1 modul: Horizontal accuracy
 1512GNSS1 Vertical Accuracy EstimatemData from GNSS1 modul: Vertical accuracy
 1513GNSS1 Velocity Northm/sData from GNSS1 modul: Velocity in North direction (NED Coordinates system)
 1514GNSS1 Velocity Eastm/sData from GNSS1 modul: Velocity in East direction (NED Coordinates system)
 1515GNSS1 Velocity Downm/sData from GNSS1 modul: Velocity in Down direction (NED Coordinates system)
 1516GNSS1 Speed Accuracy Estimatem/sData from GNSS1 modul: Speed accuracy
 1517GNSS1 Related Base LongituderadianData from GNSS1 modul: RTK Base longitude
 1518GNSS1 Related Base LatituderadianData from GNSS1 modul: RTK Base latitude
 1519GNSS1 Related Base WGS84 AltitudemData from GNSS1 modul: RTK Base WGS84 Altitude
 1520GNSS1 Related Base to Rover AzimuthradianData from GNSS1 modul: RTK Base-Rover vector azimuth (Spherical COordinates system)
 1521GNSS1 Related Base to Rover ElevationradianData from GNSS1 modul: RTK Base-Rover vector elevation (Spherical COordinates system)
 1522GNSS1 Related Base to Rover DistancemData from GNSS1 modul: RTK Base-Rover vector distance (Spherical COordinates system)
 1523GNSS1 Related Base to Rover AccuracymData from GNSS1 modul: RTK Base-Rover vector accuracy
 1524GNSS1 Survey in AccuracymData from GNSS1 modul: RTK Base accuracy when base knows it is fixed in a particular position/td>
 1525GNSS1 Related Base to Rover NorthmData from GNSS1 modul: RTK Base-Rover vector North (NED Coordinate system)
 1526GNSS1 Related Base to Rover EastmData from GNSS1 modul: RTK Base-Rover vector East (NED Coordinate system)
 1527GNSS1 Related Base to Rover DownmData from GNSS1 modul: RTK Base-Rover vector Down (NED Coordinate system)
 1600GNSS2 Time of WeeksData from GNSS2 modul: Time of the week
 1601GNSS2 ECEF Position XmData from GNSS2 modul: ECEF (Earth-Centered Earth-Fixed coordinate system) position X
 1602GNSS2 ECEF Position YmData from GNSS2 modul: ECEF (Earth-Centered Earth-Fixed coordinate system) position Y
 1603GNSS2 ECEF Position ZmData from GNSS2 modul: ECEF (Earth-Centered Earth-Fixed coordinate system) position Z
 1604GNSS2 LongituderadianData from GNSS2 modul: Longitude
 1605GNSS2 LatituderadianData from GNSS2 modul: Latitude
 1606GNSS2 Height Above Ellipsoid (WGS84)mData from GNSS2 modul: Height Above Ellipsoid (WGS84)
 1607GNSS2 Mean Sea Level (MSL)mData from GNSS2 modul: MSL
 1608GNSS2 Above Ground Level (AGL)mData from GNSS2 modul: AGL
 1609GNSS2 PDOP (Dilution of Precision of Position)customTypeData from GNSS2 modul: PDOP – Relation between user position error and satellite position error
 1610GNSS2 AccuracymData from GNSS2 modul: Accuracy
 1611GNSS2 Horizontal Accuracy EstimatemData from GNSS2 modul: Horizontal accuracy
 1612GNSS2 Vertical Accuracy EstimatemData from GNSS2 modul: Vertical accuracy
 1613GNSS2 Velocity Northm/sData from GNSS2 modul: Velocity in North direction (NED Coordinates system)
 1614GNSS2 Velocity Eastm/sData from GNSS2 modul: Velocity in East direction (NED Coordinates system)
 1615GNSS2 Velocity Downm/sData from GNSS2 modul: Velocity in Down direction (NED Coordinates system)
 1616GNSS2 Speed Accuracy Estimatem/sData from GNSS2 modul: Speed accuracy
 1617GNSS2 Related Base LongituderadianData from GNSS2 modul: RTK Base longitude
 1618GNSS2 Related Base LatituderadianData from GNSS2 modul: RTK Base latitude
 1619GNSS2 Related Base WGS84 AltitudemData from GNSS2 modul: RTK Base WGS84 Altitude
 1620GNSS2 Related Base to Rover AzimuthradianData from GNSS2 modul: RTK Base-Rover vector azimuth (Spherical COordinates system)
 1621GNSS2 Related Base to Rover ElevationradianData from GNSS2 modul: RTK Base-Rover vector elevation (Spherical COordinates system)
 1622GNSS2 Related Base to Rover DistancemData from GNSS2 modul: RTK Base-Rover vector distance (Spherical COordinates system)
 1623GNSS2 Related Base to Rover AccuracymData from GNSS2 modul: RTK Base-Rover vector accuracy
 1624GNSS2 Survey in AccuracymData from GNSS2 modul: RTK Base accuracy when base knows it is fixed in a particular position/td>
 1625GNSS2 Related Base to Rover NorthmData from GNSS2 modul: RTK Base-Rover vector North (NED Coordinate system)
 1626GNSS2 Related Base to Rover EastmData from GNSS2 modul: RTK Base-Rover vector East (NED Coordinate system)
 1627GNSS2 Related Base to Rover DownmData from GNSS2 modul: RTK Base-Rover vector Down (NED Coordinate system)
 1700-1731Actuator Output s1 – s32customTypeConfigurable variable from actuator outputs to be transformed by the system
 1800-1895Distance, azimuth and elevation to Object of Interest 1-32m, radian and m (respectively)Spherical coordinates to Object of interest
 2000RX Packet Error Rate (on board)decimal Value relating RX packets and expected RX packets, given as % error
 2001TX Packet Error Rate (on board)decimal Value relating TX packets and expected TX packets, given as % error
 2002Computed RX pkt/s used for RX PERmessages
 2003Remote RX pkt/s used for TX PERmessages
 2004Computed TX pkt/s used for TX PERmessages
 2005Remote TX pkt/s used for RX PERmessages
 2019Stick RX rateHz
 2020Position fix Timesec
 2046Max duration of step in acquisitionsec
 2047Acquisition task timestepsec
 2048Acquisition task maximum timestepsec
 2049Cross core message queue CPU ratiopercentage
 2050Acquisition task average CPU ratiopercentage
 2051Acquisition task maximum CPU ratiopercentage
 2052Acquisition task average timesec
 2053Acquisition task maximum timesec
 2094GNC task average CPU ratiopercentage
 2095GNC task maximum CPU ratiopercentage
 2096GNC task average timesec
 2097GNC task maximum timesec
 2098GNC task maximum timestepsec
 2099Max duration of step in GNCsec
 2100Gyroscope Based on Accelerometer – X Body Axisrad/s (RDS)
 2101Gyroscope Based on Accelerometer – Y Body Axisrad/s (RDS)
 2102Gyroscope Based on Accelerometer – Z Body Axisrad/s (RDS)
 2103Acceleration Northm/s²Acceleration in the North direction (NED Coordinates System)
 2104Acceleration Eastm/s²Acceleration in the East direction (NED Coordinates System)
 2105Acceleration Downm/s²Acceleration in the Down direction (NED Coordinates System)
 2112Estimated DemmAltitude given by the estimated Digital ELevation Model
 2200Curve Length CoveredmTotal distance from current mission leg covered
 2201Curve LengthmTotal distance from current mission leg
 2202Curve Length PendingmTotal distance from current mission leg to be covered yet
 2203Curve Parameter CoveredcustomTypeTotal amount from current mission leg covered according to parameter selected
 2204Curve Parameter RangecustomTypeTotal distance from current mission leg according to parameter selected
 2205Curve Parameter PendingcustomTypeTotal distance from current mission leg to be covered according to parameter selected yet
 2250-2259Reserved 1-10customTypeSystem reserved variables
 2300-2302Joint 1-3 of Gimbal 1radianVariables for Gimbal 1 configuration – Angles sent to gimbal as Yaw (1), Pitch (2) and Roll (3)
 2303-2305Joint 1-3 of Gimbal 2radianVariables for Gimbal 2 configuration – Angles sent to gimbal as Yaw (1), Pitch (2) and Roll (3)
 2400-2419Control Output u1 – u20customTypePID Output values that are transformed into Actuators Output through SU matrix
 2500-2519Stick Input u1-u20customTypeIntermediate values from stick used for arcade mode
 2600-2619Stick Input d1-d20customTypeIntermediate values from stick used for arcade mode – delta values
 2700-2712Operation Guidance 1-13customTypeConfigurable values used in different guidances – Position or values or vectors
 2800Wind Velocity Northm/sWind velocity vector pointing North direction (NED Coordinate system)
 2801Wind Velocity Eastm/sWind velocity vector pointing East direction (NED Coordinate system)
 2802Wind Velocity Downm/sWind velocity vector pointing Down direction (NED Coordinate system)
 2803Wind Velocity North Estimation Covariancem/sWind velocity vector pointing North direction (NED Coordinate system) estimation covariance
 2804Cross North-East Wind Velocity Estimation Covariancem/sWind velocity vector pointing cross North-East direction (NED Coordinate system) estimation covariance
 2805Wind Velocity Estimation Uncertainty (Element 2-0)m/s
 2806Wind Velocity Estimation Uncertainty (Element 0-1)m/s
 2807Wind Velocity Estimation Uncertainty (Element 1-1)m/s
 2808Wind Velocity Estimation Uncertainty (Element 2-1)m/s
 2809Wind Velocity Estimation Uncertainty (Element 0-2)m/s
 2810Wind Velocity Estimation Uncertainty (Element 1-2)m/s
 2811Wind Velocity Estimation Uncertainty (Element 2-2)m/s
 2900MSL Right from Actual QNH and Pressure MeasurementmMean Sea Level obtained from Actual QNH and current Pressure Measurement
 2901MSL for ISA and Pressure MeasurementmMean Sea Level calculated for ISO International Standard Atmosphere and Pressure Measurement
 2902Time Since Entering Current PhasesecTime lapse considered since entering the current phase
 2903GNC Timestepsec
 2904Total Flight TimesTime lapse since the vehicle exited Standby
 2905Total Flight DistancemDistance covered by the vehicle in all mission length
 2906Reception Frequency of Simulated Navigation DataHzFrequency at which the system receives Simulation Navigation Data
 2907Reception Frequency of External Navigation DataHzFrequency at which the system receives External Navigation Data
 2908-2927Time Spent Within Phase 1-20secTime lapse spent by the vehicle in any phase
 3000-3031Simulation Variable 1-32customTypeVariables used for Simulation data
 3100-3199User Variable 01-100 (Real – 32 bits)customTypeFree variables for the user to use
BIT0-2Initialisation valuesBit for fail, ok and license – 0 for error, 1 for running
3System ReadinessSystem is ready to start operating – 0 for not ready, 1 for ready
4Writing telemetryTelemetry is properly sending/receiving – 0 for no, 1 for yes
5Readiness to flightSystem is ready to start operation/flight – 0 for no, 1 for yes
6File System stateSystem file manager is working – 0 for error, 1 for running
50Sensors stateError/Running
51Main IMU0 for not enable, 1 for enable
52Secondary IMU0 for not enable, 1 for enable
53MagnetometerInternal magnetometer – 0 for not enable, 1 for enable
54External magnetometer (Hmr2300)HMR2300 External magnetometer – 0 for not enable, 1 for enable
55External Magnetometer (LIS3MDL)LIS3MDL External magnetometer – 0 for not enable, 1 for enable
56Static pressure sensor (HSC)HSC Static Pressure Sensor – 0 for not enable, 1 for enable
57Static pressure sensor (MS56)MS56 Static Pressure Sensor – 0 for not enable, 1 for enable
58Dynamic pressure sensor (HSC)HSC Dynamic Pressure Sensor – 0 for not enable, 1 for enable
59External I2C devices0 for not enable, 1 for enable
60-64External I2CExternal communication I2C – 0 for not enable, 1 for enable
65-72SCI A-DSerial Communication Interface – 0 for transmision, 1 for reception
73-76CAN A-BCAN Bus communication – 0 for error, 1 for running
100Position FixGNSS data reception – 0 for not receiving, 1 for receiving
101Georeferenced Area0 for being outside a Georeferenced area, 1 for being inside
102-103CAN A-BCAN A or B communication – 0 for not receiving, 1 for receiving
104-105Stick PPM 1-2 detectionStick PPM (1 or 2) – 0 for not detecting, 1 for detecting
106-108SCI A-C StateDefines the state of the Serial Communication Interface bus – 0 for error, 1 for running
109MCBSPDefines the state of the Multichannel Buffered Serial Port – 0 for error, 1 for running
110Stick stateShow if the stick is being detected – 0 for error, 1 for running
111-112CAN A-BCAN A or B communication – 0 for not Transmitting, 1 for transmitting
113Iridium ReadinessIridium ready state – 0 for not ready, 1 for ready
114-115EKFExtendad Kalman Filter working – 0 for error, 1 for running
116Radar Altimeter CAN-RXRadar Altimeter State – 0 for error, 1 for running
117-118Power A-B StatePower A-B State – 0 for error, 1 for running
130EFK Navigation StateExtended Kalman Filter Navigation State – 0 for error, 1 for running
150External navigation StateExternal Navigation State – 0 for error, 1 for running
180AttitudeKind of attitude calculation – 0 for external, 1 for internal
181Reserved StateSystem Bit
190Internest ultrasound position status0 for error, 1 for running
191Internest ultrasound angle status0 for error, 1 for running
200-206(D)GNSS1(Differential) GNSS1 Navigation, Input, Survey In, Float and Fixed Solution and Relative Position – 0 for Off, 1 for On
300-306(D)GNSS2(Differential) GNSS2 Navigation, Input, Survey In, Float and Fixed Solution and Relative Position – 0 for Off, 1 for On
400, 403-405ReservedSystem Bit
401GNC progressGNC Step Missed (0) and GNC Task ok (1)
402Acquisition progressAcquisition Step Missed (0) and Acquisition Task ok (1)
500-519Polygon0 for being outside a Polygon, 1 for being inside
600-619Circle0 for being outside a Circle, 1 for being inside
700-731Servo 1-32 stateServos state – 0 for saturated, 1 for Ok
800-815PWM GPIO StatePWM GPIO communication Sate – 0 for Off, 1 for On
816-819IO 1-4 StateInput/Output Sate – 0 for Off, 1 for On
820-822RSSI LED 1-3 StateReceived Signal Strength Indicator led state – 0 for Off, 1 for On
1000-1009Simulation BIT 1-10 StateVariables used for Simulation data – 0 for error, 1 for running
1200-1299User BIT 1-100Free bits for the user to use – 0 for error, 1 for running
16 VAR
0Control ModeIndex pointing to the Control mode in use
1Mission Phase IDPhase Identifier
2 -18ADC Channel 1-17Internal ADC 1, 7-8 ADC 1-5
19Current envelopeIndex pointing to the envelope in use
80Detour calculation identifierIndex for a route change
100-101GNSS1-2 Satellites Number InformationNumber of Satellites Used in Solution
200Radar Altimeter StateIndex for the radar altimeter state
201Current SectionIndex showing section
202Last Achieved SectionIndex showing sections achieved
203Track StageIndex showed when a route change happes
204Current patchset IDIndex showing the patchset
303-305HMR2300 Magnetometer Raw MeasurementX, Y & Z
310-311IridiumSent & Received
399Identifier of max duration step in acquisitionIndex
400Internest raw statusIndex
401Navigation sourceIndex pointing to the primary navigation source
402Raw position source identifierIndex
403-409Sensor selectionStatic & Dynamic Pressure, Pimary accelerometer & gyroscope and magnetometer
425Step in GNC max durationIdentifier for the step with maximum duration
450-453CAN errorsTx & Rx
497-499ConfigurationConfig manager status, global configuration state of files & memory
500Transponder sequence numberValue of the transponder sequnce number
501System ReservedSystem variables not configurable
900-909Simulation variablesVariables used for Simulation data
1000-1099User VariablesFree variables for the user to use