Note. Bit Variables displayed on Labels (see Workspace – Gauge Display) will be shown as Red/Green depending on its state. Red stands for 0 and Green for 1, changing the name displayed accordingly to the BIT value.

Type ID Name Units/Values Description
32 VAR 0 IAS (Indicated Air Speed) m/s Pitot-static measurement speed
1 TAS (True Air Speed) m/s Speed relative to the airmass in which the vehicle is moving (IAS measurement corrected with Standard Atmosphere data)
2 GS (Ground Speed) m/s Horizontal speed, relative to the ground
3 Heading radian Direction in which the vehicle velocity vector is pointing
4 Flight Path Angle radian Angle between velocity vector and local horizontal line
5 Bank radian Velocity vector lateral component
6 Yaw radian Angle around the Vertical axis of the vehicle
7 Pitch radian Angle around the Transverse axis of the vehicle
8 Roll radian Angle around the Longitudinal axis of the vehicle
9 Along-Track Error m Fix error along the flight track
10 Cross-Track Error m Fix error across the flight track
11 Vertical-Track Error m Fix error in the vertical flight track
12 Roll Rate rad/s (RDS) Rate of change of the Roll angle
13 Pitch Rate rad/s (RDS) Rate of change of the Pitch angle
14 Yaw Rate rad/s (RDS) Rate of change of the Yaw angle
15 Forward Acceleration – X Body Axis m/s² Acceleration in the X-axis
16 Right Acceleration – Y Body Axis m/s² Acceleration in the Y-axis
17 Bottom Acceleration – Z Body Axis m/s² Acceleration in the Z-axis
18 RPM rad/s (RDS) Revolutions per minute configurable for external sensor
19 Front GV (Ground Velocity) m/s GV vector X component
20 Lateral GV (Ground Velocity) m/s GV vector Y component
21 Velocity m/s Velocity vector module
22 Forward Load Factor – X Body Axis customType G-force in X body axis
23 Right Load Factor – Y Body Axis customType G-force in Y body axis
24 Bottom Load Factor – Z Body Axis customType G-force in Z body axis
25 Tangential Acceleration m/s² Absolute acceleration for tangential direction
26 Energy Rate customType Variation from system total energy (kinetic & potential)
27 Energy Distribution customType Division of energy used between kinetic and potential
28 co-yaw radian Acrobatic Yaw with Body Z’ axis pointing to X
29 co-pitch radian Acrobatic Pitch with Body X’ axis pointing to -Z
30 co-roll radian Acrobatic Roll with Y’ keeping same as Y
31 Roll acceleration radian/s² Acceleration around the longitudinal axis
32 Pitch acceleration radian/s² Acceleration around the transverse axis
33 Yaw Acceleration radian/s² Acceleration around the vertical axis
40 RSSI decimal Received Signal Strength Indicator
100 Desired IAS (Indicated Air Speed) m/s Commanded IAS from guidance
101 Desired TAS (True Air Speed) m/s Commanded TAS from guidance
102 Desired GS (Ground Speed) m/s Commanded GS from guidance
103 Desired Heading radian Commanded Heading from guidance
104 Desired Flight Path Angle radian Commanded Flight Path Angle from guidance
105 Desired Bank radian Commanded Bank from guidance
106 Desired Yaw radian Commanded Yaw from guidance
107 Desired Pitch radian Commanded Pitch from guidance
108 Desired Roll radian Commanded Roll from guidance
109 Desired Along-Track Error m Commanded Along-Track error from guidance
110 Desired Cross-Track Error m Commanded Cross-Track error from guidance
111 Desired Vertical-Track Error m Commanded Vertical-Track error from guidance
112 Desired Roll Rate rad/s (RDS) Commanded Roll rate from guidance
113 Desired Pitch Rate rad/s (RDS) Commanded Pitch rate from guidance
114 Desired Yaw Rate rad/s (RDS) Commanded Yaw rate from guidance
115 Desired Foward Acceleration – X Body Axis m/s² Commanded Forward Acceleration from guidance
116 Desired Right Acceleration – Y Body Axis m/s² Commanded Right Acceleration from guidance
117 Desired Bottom Acceleration – Z Body Axis m/s² Commanded Bottom Acceleration from guidance
118 Desired RPM rad/s (RDS) Commanded RPM from guidance
119 Desired Front GV (Ground Velocity) m/s Commanded Front GV from guidance
120 Desired Lateral GV (Ground Velocity) m/s Commanded Lateral GV from guidance
121 Desired Velocity m/s Commanded Velocity from guidance
122 Desired Forward Load Factor – X Body Axis customType Commanded Forward Load Factor from guidance
123 Desired Right Load Factor – Y Body Axis customType Commanded Right Load Factor from guidance
124 Desired Bottom Load Factor – Z Body Axis customType Commanded Bottom Load Facto from guidance
125 Desired Tangential Acceleration m/s² Commanded Tangential Acceleration from guidance
126 Desired Energy Rate customType Commanded Energy Rate from guidance
127 Desired Energy Distribution customType Commanded Energy Distribution from guidance
128 Desired co-yaw radian Commanded co-yaw from guidance
129 Desired co-pitch radian Commanded co-pitch from guidance
130 Desired co-roll radian Commanded co-roll from guidance
200 Desired North GV (Ground Velocity) m/s Commanded North (NED Coordinates system) GV from guidance
201 Desired East GV (Ground Velocity) m/s Commanded East (NED Coordinates system) GV from guidance
202 Desired Down GV (Ground Velocity) m/s Commanded Down (NED Coordinates system) GV from guidance
203 Desired 2D MSL (Heigh Above Mean Sea Level) m Commanded MSL from guidance in 2D height mode
204 Desired 2D AGL (Above Ground Level) – Height m Commanded AGL from guidance in 2D height mode
205 Desired 2D WGS84 Elevation (Height Over The Ellipsoid) m Commanded WGS84 Elevation from guidance in 2D height mode
206 Desired Longitude radian Commanded Longitude from guidance
207 Desired Latitude radian Commanded Latitude from guidance
208 Desired WGS84 Elevation (Height Over The Ellipsoid) m Commanded WGS84 Elevation from guidance
209 Desired MSL (Height Above Mean Sea Level) – Altitude m Commanded MSL Altitude from guidance
210 Desired AGL (Above Ground Level) – Height m Commanded AGL Altitude from guidance
250 Guidance north position error m Difference from Desired and actual north position
251 Guidance east position error m Difference from Desired and actual east position
252 Guidance down position error m Difference from Desired and actual down position
253 Guidance PID north desired velocity m/s Difference from Desired and actual PID north velocity
254 Guidance PID east desired velocity m/s Difference from Desired and actual PID east velocity
255 Guidance PID down desired velocity m/s Difference from Desired and actual PID down velocity
256 Desired velocity X body axis m/s Commanded velocity in X-axis from guidance
257 Desired velocity Y body axis m/s Commanded velocity in Y-axis from guidance
258 Desired velocity Z body axis m/s Commanded velocity in Z-axis from guidance
259 External yaw radian Yaw from external navigation source
260 External pitch radian Pitch from external navigation source
261 External roll radian Roll from external navigation source
262 External Roll Rate rad/s Roll rate from external navigation source
263 External Pitch Rate rad/s Pitch rate from external navigation source
264 External Yaw Rate rad/s Yaw rate from external navigation source
265 External Velocity North m/s Velocity North from external navigation source
266 External Velocity East m/s Velocity East from external navigation source
267 External Velocity Down m/s Velocity Down from external navigation source
268 External acceleration x body axis m/s² Acceleration x body axis from external navigation source
269 External acceleration y body axis m/s² Acceleration y body axis from external navigation source
270 External acceleration z body axis m/s² Acceleration z body axis from external navigation source
271 External GPS Time of Week s GNSS Time of week from external navigation source
300 Time since Hardware Start-Up sec Time spent since power-on of the system
301 Used Memory Space Byte SD used memory space
302 Free Memory Space Byte SD free memory space
303 Dynamic Pressure pascal Physical measurement from Pitot
304 Static Pressure pascal Physical measurement from Pitot
305 Internal Temperature kelvin (K) Physical measurement from internal sensors
306 External Temperature kelvin (K) Physical measurement from Veronte sensors
307 Accelerometer – X Body Axis m/s² Accelerometer measurement for X axis
308 Accelerometer – Y Body Axis m/s² Accelerometer measurement for Y axis
309 Accelerometer – Z Body Axis m/s² Accelerometer measurement for Z axis
310 Gyroscope – X Body Axis rad/s (RDS) Gyroscope measurement for X axis
311 Gyroscope – Y Body Axis rad/s (RDS) Gyroscope measurement for Y axis
312 Gyroscope – Z Body Axis rad/s (RDS) Gyroscope measurement for Z axis
313 Magnetometer – X Body Axis tesla Magnetometer measurement for X axis
314 Magnetometer – Y Body Axis tesla Magnetometer measurement for Y axis
315 Magnetometer – Z Body Axis tesla Magnetometer measurement for Z axis
322 Internal magnetometer raw X in SI tesla Magnetometer raw measurement for X axis
323 Internal magnetometer raw Y in SI tesla Magnetometer raw measurement for Y axis
324 Internal magnetometer raw Z in SI tesla Magnetometer raw measurement for Z axis
325 Internal magnetometer temperature kelvin (K) Magnetometer temperature
326 External LIS3MDL magnetometer raw X in SI tesla LIS3MDL external Magnetometer raw measurement for X axis
327 External LIS3MDL magnetometer raw Y in SI tesla LIS3MDL external Magnetometer raw measurement for Y axis
328 External LIS3MDL magnetometer raw Z in SI tesla LIS3MDL external Magnetometer raw measurement for Z axis
329 External LIS3MDL magnetometer temperature kelvin (K) LIS3MDL external Magnetometer temperature
330 IMU 0 raw accelerometer x measurement m/s² IMU 0 raw accelerometer x measurement
331 IMU 0 raw accelerometer y measurement m/s² IMU 0 raw accelerometer y measurement
332 IMU 0 raw accelerometer z measurement m/s² IMU 0 raw accelerometer z measurement
333 IMU 0 raw gyroscope x measurement rad/s (RDS) IMU 0 raw gyroscope x measurement
334 IMU 0 raw gyroscope y measurement rad/s (RDS) IMU 0 raw gyroscope y measurement
335 IMU 0 raw gyroscope z measurement rad/s (RDS) IMU 0 raw gyroscope z measurement
336 IMU 0 temperature measurement kelvin (K) IMU 0 temperature measurement
337 IMU 1 raw accelerometer x measurement m/s² IMU 1 raw accelerometer x measurement
338 IMU 1 raw accelerometer y measurement m/s² IMU 1 raw accelerometer y measurement
339 IMU 1 raw accelerometer z measurement m/s² IMU 1 raw accelerometer z measurement
340 IMU 1 raw gyroscope x measurement rad/s (RDS) IMU 1 raw gyroscope x measurement
341 IMU 1 raw gyroscope y measurement rad/s (RDS) IMU 1 raw gyroscope y measurement
342 IMU 1 raw gyroscope z measurement rad/s (RDS) IMU 1 raw gyroscope z measurement
343 IMU 1 temperature measurement kelvin (K) IMU 1 temperature measurement
344 Static pressure sensor (MS56) raw measurement pascal Static pressure sensor 1 raw measurement
345 Static pressure sensor (MS56) temperature kelvin (K) Static pressure sensor 1 temperature
346 Dynamic pressure sensor raw measurement pascal Dynamic pressure sensor raw measurement
347 Dynamic pressure sensor temperature kelvin (K) Dynamic pressure sensor temperature
348 Static pressure sensor (HSC) raw measurement pascal Static pressure sensor 0 raw measurement
 349 Static pressure sensor (HSC) temperature kelvin (K) Static pressure sensor 0 temperature
350 Vectornav Message Frequency Hz Frequency at which external navigation source VectorNav sends messages
351 Vectornav Raw Acc x measurement m/s² Raw accelerometer X measurement from external navigation source VectorNav
352 Vectornav Raw Acc y measurement m/s² Raw accelerometer Y measurement from external navigation source VectorNav
353 Vectornav Raw Acc z measurement m/s² Raw accelerometer Z measurement from external navigation source VectorNav
354 Vectornav Raw Gyr x measurement m/s² Raw gyroscope X measurement from external navigation source VectorNav
355 Vectornav Raw Gyr y measurement m/s² Raw gyroscope Y measurement from external navigation source VectorNav
356 Vectornav Raw Gyr z measurement m/s² Raw gyroscope Z measurement from external navigation source VectorNav
 400 Power Input volts Power received by Veronte
 401 Power Comicro 3.3V volts Power received by Veronte through 3.3V port
 402 Power 5V volts Power received by Veronte through 5V port
 403 Power Comicro Regulator volts Power received by Veronte Comicro Regulator
 404 Power 3.6V volts Power received by Veronte through 3.6V port
 405 CPU Temperature kelvin (K) Internal computer temperature
 500 Longitude radian East-West geographic coordinate
 501 Latitude radian North-South geographic coordinate
 502 WGS84 Elevation (Height Over the Ellipsoid) m Elevation over WGS84 reference frame
 503 MSL (Height Above Mean Sea Level) – Altitude m Altitude over the Mean Sea Level
 504 AGL (Above Ground Level) – Height m Height Above Ground Level – Dependent on external sensors or own models with considerable error
 505 Ground Velocity North m/s Ground Velocity component in the North direction (NED Coordinates system)
 506 Ground Velocity East m/s Ground Velocity component in the East direction (NED Coordinates system)
 507 Ground Velocity Down m/s Ground Velocity component in the resultant axis from North-East (NED Coordinates system)
 508 Sensor IAS (Indicated Air Speed) m/s Pitot-static measurement speed
 509 Angle of Attack – AoA radian Angle between reference body line and flow direction vector
 510 Sideslip radian Angle between the flow direction vector and the longitudinal axis of the vehicle
 600-603 Temperature 1-4 kelvin (K) Variables to be configured with external Temperature sensors
650 Gimbal command yaw customType Yaw sent to the gimbal
651 Gimbal command pitch customType Pitch sent to the gimbal
652 Gimbal stick yaw customType Yaw received from the joystick controlling the gimbal
653 Gimbal stick pitch customType Pitch received from the joystick controlling the gimbal
654 Gimbal pitch correction 1 customType Correction calculated by the gimbal for the pitch control
655 Gimbal pitch correction 2 customType Correction calculated by the gimbal for the pitch control
656 Gimbal old joint 1 customType Auxiliar variable for Gimbal control configuration
657 Gimbal old joint 2 customType Auxiliar variable for Gimbal control configuration
658 Cos (gimbal yaw) customType Auxiliar variable for Gimbal control configuration
659 Sin (gimbal yaw) customType Auxiliar variable for Gimbal control configuration
660 Gimbal yaw radian/td> customType Auxiliar variable for Gimbal control configuration
661 Gimbal yaw output customType Yaw value the gimbal is outputting
662 Gimbal pitch output customType Pitch value the gimbal is outputting
 700-705 RPM 1-6 rad/s (RDS) RPM associated to pulse captured 1-6
 750 Selected controller time step sec PID selected time step
 751 Selected controller derivative filtered error customType PID selected derivative filtered error
 752 Selected controller proportional action customType PID selected proportional action
 753 Selected controller derivative action customType PID selected derivative action
 754 Selected controller integral input customType PID selected integral input
 755 Selected controller integral action customType PID selected integral action
 756 Selected controller anti-windup input customType PID selected anti-windup input
 757 Selected controller derivative error customType PID selected derivative error
 800-815 PWM 1-16 customType Pulse Width Modulation signal
 900-915 Stick Input r1 – r16 customType Raw stick measurement
 1000-1031 Stick Input y1 – y32 customType Servo position commanded from stick
 1100-1104 Lidar 1-5 Distances m Variable configurable for Lidar distances
 1105-1109 External range sensor 1-5 measurements m Variable configurable for external range sensors
 1200 Cross-track Distance customType Shortest distance to desired path (perpendicular distance)
 1201 Radar AGL (Above Ground Level) – Height m User Variable
 1202 Radar Speed Down m/s User Variable
 1203 External Rotation for Follow Route radian Relative vector rotation when using Follow Route
 1204 Time to Impact with Obstacles sec Time calculated with Distance to Obstacle and travel speed
 1300-1309 Clock 1-10 sec Configurable timers for automations – Clock 1 correspond to Timer 1, etc
 1400 Velocity – X Body Axis m/s Velocity vector X component
 1401 Velocity – Y Body Axis m/s Velocity vector Y component
 1402 Velocity – Z Body Axis m/s Velocity vector Z component
 1403 Estimated Dynamic Pressure pascal Dynamic pressure sensor raw measurement
 1404 Barometric Pressure at Sea Level (QNH) pascal Introduced value for QNH
 1450-1453 Captured pulse 1-4 customType Input values from pulses
 1490 Internest raw x distance m Raw measurements for X-axis internest distance
 1491 Internest raw y distance m Raw measurements for Y-axis internest distance
 1492 Internest raw z distance m Raw measurements for Z-axis internest distance
 1493 Internest raw angle radian Raw measurements for internest angle
 1494 Internest raw xy standard deviation m Raw measurements for XY axis internest standard deviation
 1495 Internest raw z standard deviation m Raw measurements for Z-axis internest standard deviation
 1496 Internest raw angle standard deviation radian Raw measurements for internest angle standard deviation
 1497 Internest position update frequency Hz Frequency at which Interest updates its position
 1500 GNSS1 Time of Week s Data from GNSS1 module: Time of the week
 1501 GNSS1 ECEF Position X m Data from GNSS1 module: ECEF (Earth-Centered Earth-Fixed coordinate system) position X
 1502 GNSS1 ECEF Position Y m Data from GNSS1 module: ECEF (Earth-Centered Earth-Fixed coordinate system) position Y
 1503 GNSS1 ECEF Position Z m Data from GNSS1 module: ECEF (Earth-Centered Earth-Fixed coordinate system) position Z
 1504 GNSS1 Longitude radian Data from GNSS1 module: Longitude
 1505 GNSS1 Latitude radian Data from GNSS1 module: Latitude
 1506 GNSS1 Height Above Ellipsoid (WGS84) m Data from GNSS1 module: Height Above Ellipsoid (WGS84)
 1507 GNSS1 Mean Sea Level (MSL) m Data from GNSS1 module: MSL
 1508 GNSS1 Above Ground Level (AGL) m Data from GNSS1 module: AGL
 1509 GNSS1 PDOP (Dilution of Precision of Position) customType Data from GNSS1 module: PDOP – Relation between user position error and satellite position error
 1510 GNSS1 Accuracy m Data from GNSS1 module: Accuracy
 1511 GNSS1 Horizontal Accuracy Estimate m Data from GNSS1 module: Horizontal accuracy
 1512 GNSS1 Vertical Accuracy Estimate m Data from GNSS1 module: Vertical accuracy
 1513 GNSS1 Velocity North m/s Data from GNSS1 module: Velocity in North direction (NED Coordinates system)
 1514 GNSS1 Velocity East m/s Data from GNSS1 module: Velocity in East direction (NED Coordinates system)
 1515 GNSS1 Velocity Down m/s Data from GNSS1 module: Velocity in Down direction (NED Coordinates system)
 1516 GNSS1 Speed Accuracy Estimate m/s Data from GNSS1 module: Speed accuracy
 1517 GNSS1 Related Base Longitude radian Data from GNSS1 module: RTK Base longitude
 1518 GNSS1 Related Base Latitude radian Data from GNSS1 module: RTK Base latitude
 1519 GNSS1 Related Base WGS84 Altitude m Data from GNSS1 module: RTK Base WGS84 Altitude
 1520 GNSS1 Related Base to Rover Azimuth radian Data from GNSS1 module: RTK Base-Rover vector azimuth (Spherical COordinates system)
 1521 GNSS1 Related Base to Rover Elevation radian Data from GNSS1 module: RTK Base-Rover vector elevation (Spherical COordinates system)
 1522 GNSS1 Related Base to Rover Distance m Data from GNSS1 module: RTK Base-Rover vector distance (Spherical COordinates system)
 1523 GNSS1 Related Base to Rover Accuracy m Data from GNSS1 module: RTK Base-Rover vector accuracy
 1524 GNSS1 Survey in Accuracy m Data from GNSS1 module: RTK Base accuracy when base knows it is fixed in a particular position/td>
 1525 GNSS1 Related Base to Rover North m Data from GNSS1 module: RTK Base-Rover vector North (NED Coordinate system)
 1526 GNSS1 Related Base to Rover East m Data from GNSS1 module: RTK Base-Rover vector East (NED Coordinate system)
 1527 GNSS1 Related Base to Rover Down m Data from GNSS1 module: RTK Base-Rover vector Down (NED Coordinate system)
 1600 GNSS2 Time of Week s Data from GNSS2 module: Time of the week
 1601 GNSS2 ECEF Position X m Data from GNSS2 module: ECEF (Earth-Centered Earth-Fixed coordinate system) position X
 1602 GNSS2 ECEF Position Y m Data from GNSS2 module: ECEF (Earth-Centered Earth-Fixed coordinate system) position Y
 1603 GNSS2 ECEF Position Z m Data from GNSS2 module: ECEF (Earth-Centered Earth-Fixed coordinate system) position Z
 1604 GNSS2 Longitude radian Data from GNSS2 module: Longitude
 1605 GNSS2 Latitude radian Data from GNSS2 module: Latitude
 1606 GNSS2 Height Above Ellipsoid (WGS84) m Data from GNSS2 module: Height Above Ellipsoid (WGS84)
 1607 GNSS2 Mean Sea Level (MSL) m Data from GNSS2 module: MSL
 1608 GNSS2 Above Ground Level (AGL) m Data from GNSS2 module: AGL
 1609 GNSS2 PDOP (Dilution of Precision of Position) customType Data from GNSS2 module: PDOP – Relation between user position error and satellite position error
 1610 GNSS2 Accuracy m Data from GNSS2 module: Accuracy
 1611 GNSS2 Horizontal Accuracy Estimate m Data from GNSS2 module: Horizontal accuracy
 1612 GNSS2 Vertical Accuracy Estimate m Data from GNSS2 module: Vertical accuracy
 1613 GNSS2 Velocity North m/s Data from GNSS2 module: Velocity in North direction (NED Coordinates system)
 1614 GNSS2 Velocity East m/s Data from GNSS2 module: Velocity in East direction (NED Coordinates system)
 1615 GNSS2 Velocity Down m/s Data from GNSS2 module: Velocity in Down direction (NED Coordinates system)
 1616 GNSS2 Speed Accuracy Estimate m/s Data from GNSS2 module: Speed accuracy
 1617 GNSS2 Related Base Longitude radian Data from GNSS2 module: RTK Base longitude
 1618 GNSS2 Related Base Latitude radian Data from GNSS2 module: RTK Base latitude
 1619 GNSS2 Related Base WGS84 Altitude m Data from GNSS2 module: RTK Base WGS84 Altitude
 1620 GNSS2 Related Base to Rover Azimuth radian Data from GNSS2 module: RTK Base-Rover vector azimuth (Spherical COordinates system)
 1621 GNSS2 Related Base to Rover Elevation radian Data from GNSS2 module: RTK Base-Rover vector elevation (Spherical COordinates system)
 1622 GNSS2 Related Base to Rover Distance m Data from GNSS2 module: RTK Base-Rover vector distance (Spherical COordinates system)
 1623 GNSS2 Related Base to Rover Accuracy m Data from GNSS2 module: RTK Base-Rover vector accuracy
 1624 GNSS2 Survey in Accuracy m Data from GNSS2 module: RTK Base accuracy when base knows it is fixed in a particular position/td>
 1625 GNSS2 Related Base to Rover North m Data from GNSS2 module: RTK Base-Rover vector North (NED Coordinate system)
 1626 GNSS2 Related Base to Rover East m Data from GNSS2 module: RTK Base-Rover vector East (NED Coordinate system)
 1627 GNSS2 Related Base to Rover Down m Data from GNSS2 module: RTK Base-Rover vector Down (NED Coordinate system)
 1700-1731 Actuator Output s1 – s32 customType Configurable variable from actuator outputs to be transformed by the system
 1800-1895 Distance, azimuth and elevation to Object of Interest 1-32 m, radian and m (respectively) Spherical coordinates to Object of interest
 2000 RX Packet Error Rate (on board) decimal Value relating RX packets and expected RX packets, given as % error
 2001 TX Packet Error Rate (on board) decimal Value relating TX packets and expected TX packets, given as % error
 2002 Computed RX pkt/s used for RX PER messages Packages per second received to the UAV configured in communication statistics
 2003 Remote RX pkt/s used for TX PER messages Same as Computed RX pkt/s, received through communications
 2004 Computed TX pkt/s used for TX PER messages Packages per second transmitted to the UAV configured in communication statistics
 2005 Remote TX pkt/s used for RX PER messages Same as Computed TX pkt/s, received through communications
 2019 Stick RX rate Hz Stick messages received per second
 2020 Position fix Time sec Time spend with GNSS not losing fix
2040 Tunnel producer receive frequency 1 Hz Frequency at which the Tunnel producer receives data
2041 Tunnel producer receive frequency 2 Hz Frequency at which the Tunnel producer receives data
2042 Tunnel producer receive frequency 3 Hz Frequency at which the Tunnel producer receives data
2043 Tunnel consumer send frequency 1 Hz Frequency at which the Tunnel consumer sends data
2044 Tunnel consumer send frequency 2 Hz Frequency at which the Tunnel consumer sends data
2045 Tunnel consumer send frequency 3 Hz Frequency at which the Tunnel consumer sends data
 2046 Max duration of step in acquisition sec Longest time duration from a step in CIO
 2047 Acquisition task timestep sec Average period for executing the acquisition task
 2048 Acquisition task maximum timestep sec Maximum period for executing the acquisition task
 2049 Cross core message queue CPU ratio percentage % of time of CPU that CIO waits for  inter-core communications queue to be emptied
 2050 Acquisition task average CPU ratio percentage Average % of time of CPU from the acquisition task
 2051 Acquisition task maximum CPU ratio percentage Maximum % of time of CPU from the acquisition task
 2052 Acquisition task average time sec Average time acquisition task has used
 2053 Acquisition task maximum time sec Maximum time acquisition task has used
2054 CIO Max time sec Maximum time in acquisition from Core Input/Output
2055 CIO average time sec Average time in acquisition from Core Input/Output
 2094 GNC task average CPU ratio percentage Average % of time of CPU from GNC task
 2095 GNC task maximum CPU ratio percentage Maximum % of time of CPU from GNC task
 2096 GNC task average time sec Average time spent on GNC task
 2097 GNC task maximum time sec Maximum time spent on GNC task
 2098 GNC task maximum timestep sec Maximum execution period for GNC task
 2099 Max duration of step in GNC sec Maximum duration of one step in GNC
 2100 Gyroscope Based on Accelerometer – X Body Axis rad/s (RDS) Gyroscope measurements obtained from accelerometer X-axis data
 2101 Gyroscope Based on Accelerometer – Y Body Axis rad/s (RDS) Gyroscope measurements obtained from accelerometer Y-axis data
 2102 Gyroscope Based on Accelerometer – Z Body Axis rad/s (RDS) Gyroscope measurements obtained from accelerometer Z-axis data
 2103 Acceleration North m/s² Acceleration in the North direction (NED Coordinates System)
 2104 Acceleration East m/s² Acceleration in the East direction (NED Coordinates System)
 2105 Acceleration Down m/s² Acceleration in the Down direction (NED Coordinates System)
 2112 Estimated Dem m Altitude given by the estimated Digital Elevation Model
 2200 Curve Length Covered m Total distance from current mission leg covered
 2201 Curve Length m Total distance from current mission leg
 2202 Curve Length Pending m Total distance from current mission leg to be covered yet
 2203 Curve Parameter Covered customType Total amount from current mission leg covered according to parameter selected
 2204 Curve Parameter Range customType Total distance from current mission leg according to parameter selected
 2205 Curve Parameter Pending customType Total distance from current mission leg to be covered according to parameter selected yet
 2250-2259 Reserved 1-10 customType System reserved variables
 2300-2302 Joint 1-3 of Gimbal 1 radian Variables for Gimbal 1 configuration – Angles sent to gimbal as Yaw (1), Pitch (2) and Roll (3)
 2303-2305 Joint 1-3 of Gimbal 2 radian Variables for Gimbal 2 configuration – Angles sent to gimbal as Yaw (1), Pitch (2) and Roll (3)
 2400-2419 Control Output u1 – u20 customType PID Output values that are transformed into Actuators Output through SU matrix
 2500-2519 Stick Input u1-u20 customType Intermediate values from stick used for arcade mode
 2600-2619 Stick Input d1-d20 customType Intermediate values from stick used for arcade mode – delta values
 2700-2712 Operation Guidance 1-13 customType Configurable values used in different guidances – Position or values or vectors
 2800 Wind Velocity North m/s Wind velocity vector pointing North direction (NED Coordinate system)
 2801 Wind Velocity East m/s Wind velocity vector pointing East direction (NED Coordinate system)
 2802 Wind Velocity Down m/s Wind velocity vector pointing Down direction (NED Coordinate system)
 2803 Wind Velocity North Estimation Covariance m/s Wind velocity vector pointing North direction (NED Coordinate system) estimation covariance
 2804 Cross North-East Wind Velocity Estimation Covariance m/s Wind velocity vector pointing cross North-East direction (NED Coordinate system) estimation covariance
 2805 Wind Velocity Estimation Uncertainty (Element 2-0) m/s 2-0 element from covariance matrix in wind estimation
 2806 Wind Velocity Estimation Uncertainty (Element 0-1) m/s 0-1 element from covariance matrix in wind estimation
 2807 Wind Velocity Estimation Uncertainty (Element 1-1) m/s 1-1 element from covariance matrix in wind estimation
 2808 Wind Velocity Estimation Uncertainty (Element 2-1) m/s 2-1 element from covariance matrix in wind estimation
 2809 Wind Velocity Estimation Uncertainty (Element 0-2) m/s 0-2 element from covariance matrix in wind estimation
 2810 Wind Velocity Estimation Uncertainty (Element 1-2) m/s 1-2 element from covariance matrix in wind estimation
 2811 Wind Velocity Estimation Uncertainty (Element 2-2) m/s 2-2 element from covariance matrix in wind estimation
 2900 MSL Right from Actual QNH and Pressure Measurement m Mean Sea Level obtained from Actual QNH and current Pressure Measurement
 2901 MSL for ISA and Pressure Measurement m Mean Sea Level calculated for ISO International Standard Atmosphere and Pressure Measurement
 2902 Time Since Entering Current Phase sec Time-lapse considered since entering the current phase
 2903 GNC Timestep sec Task execution period from GNC
 2904 Total Flight Time s Time-lapse since the vehicle exited Standby
 2905 Total Flight Distance m Distance covered by the vehicle in all mission length
 2906 Reception Frequency of Simulated Navigation Data Hz Frequency at which the system receives Simulation Navigation Data
 2907 Reception Frequency of External Navigation Data Hz Frequency at which the system receives External Navigation Data
 2908-2927 Time Spent Within Phase 1-20 sec Time-lapse spent by the vehicle in any phase
 3000-3031 Simulation Variable 1-32 customType Variables used for Simulation data
4100 Zero customType Constant value 0
4101 Rvar disabled customType Disabled variable
BIT 0-2 Initialisation values Bit for fail, ok and license – 0 for error, 1 for running
3 System Readiness System is ready to start operating – 0 for not ready, 1 for ready
4 Writing telemetry Telemetry is properly sending/receiving – 0 for no, 1 for yes
5 Readiness to flight System is ready to start operation/flight – 0 for no, 1 for yes
6 File System state System file manager is working – 0 for error, 1 for running
7 System state System is working – 0 for error, 1 for running
8 Memory Allocation Memory allocation is working – 0 for error, 1 for running
9 PDI State PDI files are working – 0 for error, 1 for running
10 4X Arbiter state Arbiter is working for 4xVeronte – 0 for error, 1 for running
50 Sensors error Error/Running
51 Sensors-Main IMU 0 for not enable, 1 for enable
52 Sensors-Secondary IMU 0 for not enable, 1 for enable
53 Sensors-Magnetometer Internal magnetometer – 0 for not enable, 1 for enable
54 Sensors-External magnetometer (HMR2300) HMR2300 External magnetometer – 0 for not enable, 1 for enable
55 Sensors-External Magnetometer (LIS3MDL) LIS3MDL External magnetometer – 0 for not enable, 1 for enable
56 Sensors-Static pressure (HSC) HSC Static Pressure Sensor – 0 for not enable, 1 for enable
57 Sensors-Static pressure (MS56) MS56 Static Pressure Sensor – 0 for not enable, 1 for enable
58 Sensors-Dynamic pressure (HSC) HSC Dynamic Pressure Sensor – 0 for not enable, 1 for enable
59 Sensors-External I2C devices 0 for not enable, 1 for enable
60-64 Sensors-External I2C 0-4 External communication I2C – 0 for not enable, 1 for enable
65-72 SCI A-D Serial Communication Interface – 0 for transmission, 1 for reception
73-76 CAN A-B CAN Bus communication – 0 for error, 1 for running
77 Vectornav States for GPS Fix, IMU, Mag/Press, GPS Error, Navigation-Vectornav state 0 for error, 1 for running
100 Position not Fixed GNSS data reception – 0 for not receiving, 1 for receiving
101 Georeferenced Area 0 for being outside a Georeferenced area, 1 for being inside
102-103 CAN A-B CAN A or B communication – 0 for not receiving, 1 for receiving
104-105 Stick PPM 1-2 detection Stick PPM (1 or 2) – 0 for not detecting, 1 for detecting
106-108 SCI A-C State Defines the state of the Serial Communication Interface bus – 0 for error, 1 for running
109 MCBSP Defines the state of the Multichannel Buffered Serial Port – 0 for error, 1 for running
110 Stick state Show if the stick is being detected – 0 for error, 1 for running
111-112 CAN A-B CAN A or B communication – 0 for not Transmitting, 1 for transmitting
113 Iridium Readiness Iridium ready state – 0 for not ready, 1 for ready
114-115 EKF Extended Kalman Filter working – 0 for error, 1 for running
116 Radar Altimeter CAN-RX Radar Altimeter State – 0 for error, 1 for running
117-118 Power A-B State Power A-B State – 0 for error, 1 for running
130 EFK Navigation State Extended Kalman Filter Navigation State – 0 for error, 1 for running
150 External VCP State External VCP State – 0 for error, 1 for running
160 External var Navigation Error External Navigation State – 0 for error, 1 for running
180 Attitude Kind of attitude calculation – 0 for external, 1 for internal
181 Reserved State System Bit
190 Internest ultrasound position status 0 for error, 1 for running
191 Internest ultrasound angle status 0 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, 403-405 Reserved System Bit
401 GNC progress GNC Step Missed (0) and GNC Task ok (1)
402 Acquisition progress Acquisition Step Missed (0) and Acquisition Task ok (1)
500 Ground effect compensation Ground effect compensation effect – 0 for disabled, 1 for enabled
700-731 Servo 1-32 state Servos state – 0 for saturated, 1 for Ok
800-815 PWM GPIO State PWM GPIO communication Sate – 0 for Off, 1 for On
816-819 IO 1-4 State Input/Output State – 0 for Off, 1 for On
820-822 RSSI LED 1-3 State Received Signal Strength Indicator led state – 0 for Off, 1 for On
1000-1009 Simulation BIT 1-10 State Variables used for Simulation data – 0 for error, 1 for running
1200-1299 User BIT 1-100 Free bits for the user to use – 0 for error, 1 for running
2200 BIT Dummy Bit for configurable checks – 0 for error, 1 for running
16 VAR
0 Control Mode Index pointing to the Control mode in use
1 Mission Phase ID Phase Identifier
2 -18 ADC Channel 1-17 Internal ADC 1, 7-8 ADC 1-5
19 Current envelope Index pointing to the envelope in use
20 Counter for C2 system BIT Index for number of cycles from Core 2
80 Detour calculation identifier Index for a route change
100-101 GNSS1-2 Satellites Number Information Number of Satellites Used in Solution
200 Radar Altimeter State Index for the radar altimeter state
201 Current Section Index showing section
202 Last Achieved Section Index showing sections achieved
203 Track Stage Index showed when a route change happens
204 Current patchset ID Index showing the patchset
303-305 HMR2300 Magnetometer Raw Measurement X, Y & Z
310-311 Iridium Sent & Received
398 VectorNav Mode Index showing external source VectorNav mode
399 Identifier of max duration step in acquisition Index
400 Internest raw status Index
401 Navigation source Index pointing to the primary navigation source
402 Raw position source identifier Index
403-410 Sensor selection Static & Dynamic Pressure, Primary accelerometer & gyroscope, magnetometer and stick priority table
425 Step in GNC max duration Identifier for the step with maximum duration
450-453 CAN errors Tx & Rx
490 Number of moving objects detected Index
497-499 Configuration Config manager status, global configuration state of files & memory
500 Transponder sequence number Value of the transponder sequence number
501 System Reserved System variables not configurable
550-553 Command 1-4 gimbal Index
900-909 Simulation variables Variables used for Simulation data
1000-1099 User Variables Free variables for the user to use
2000 Uvar State Index
2001 Zero Uvar with constant 0 value