Lists of interest

This section contains all the lists with information of interest for the user.

Activation System Error bits

The System Error variable is indicated by bit number 7. This bit checks whether the system is running properly. If one of certain malfunctions occur, the System Error will be set as 0 and the FTS will be activated. Otherwise, if everything is OK, it will remain as 1.

The System Error is triggered and set as 0 if one of the following unwanted events happens:

  • CIO low has a frequency lower than 10 Hz. This error is indicated with a 0 in bit 400.
  • CIO high has a frequency lower than 990 Hz. This error is indicated with a 0 in bit 402.
  • GNC is 'dead'. This event is indicated with a 0 in bit 401.
  • GNC Realtime Error because a GNC Step has been missed. This event is indicated with a 0 in bit 404.
  • System power up BIT error. The initial value of this bit depends on the values of the bits listed below and represents their state at power-up. This error is indicated with a 0 in bit 12 if any of the following errors happens:

    • RAM allocation is in error state due to trying to use more memory than available. This error is indicated with a 0 in bit 8.
    • PDI files have a wrong configuration. This is indicated by a 0 in bit 9.
    • Main Power supply A is in error state. This error is indicated with a 0 in bit 117 if any of the following errors happens:
      • Input supply voltage is not between 6.5 and 36 V. This voltage is measured by RVar 400.
      • Voltage received by Veronte through 5V port is not between 4.75 and 5.25 V. This voltage is measured by RVar 402.
      • Voltage received by Veronte through 3.6V port is not between 3.42 and 3.78V. This voltage is measured by RVar 404.
  • File system manager is in error state. This event is indicated with a 0 in bit 6.

  • Core 1 has a memory overflow allocated for local variables. This error is indicated with a 0 in bit 16.
  • Core 2 has a memory overflow allocated for local variables. This error is indicated with a 0 in bit 17.
  • Any user bit configured as safety bit is 0. User bits are 1200 to 1499.

Status Message variables

The variables contained in the Veronte Autopilot 1x status message are the following.

ID Name
0Actuator Mode
1Phase Identifier
6Yaw
7Pitch
8Roll
100Position Not Fixed
201Current Section
204Current Patchset ID (needed for guidance display)
300Relative Timestamp
505North Ground Velocity
506East Ground Velocity
507Down Ground Velocity
- Guidance calculation identifier (needed for guidance display).

It can be one of these variables depending on the guidance used:

  • ID 80: Detour calculation identifier
  • ID 81: Approach calculation identifier
  • ID 82: Climb calculation identifier
  • ID 83: Cruise calculation identifier
  • ID 84: Rendezvous calculation identifier
  • ID 85: Taxi calculation identifier
  • ID 86: VTOL calculation identifier

Extended Status Message variables

Information about the Veronte Autopilot 1x extended status message is contained in the following set of bit variables.

Note

The Extended Status Message is only sent if one of the bits changes its value.

ID Name
5Power error
6File System Error
8Memory allocation
9PDI Error
12System Power up BIT Error
14FTS-1 Feedback (>=V4.5)
15FTS-2 Feedback (>=V4.5)
16Stack C1 usage FAIL
17Stack C2 usage FAIL
49CPU temperature above 398.15K
50Sensors Error
51Sensor-Main IMU
52Sensor-Secondary IMU
53Sensor-Internal Magnetometer (LIS3MDL)
54Sensor-External magnetometer (HMR2300)
73CAN-A ERROR
74CAN-B ERROR
87GNSS1 Module Error
88GNSS2 Module Error
117Main Power Error
118SUC Power Error
400C1 Low Frequency
401GNC fail
402Acquisition step missed
403CIO Hi Overload warning

List of Addresses

Every Embention device communicate with other devices/tools using its address through VCP.

The following list contains all these addresses:

Address Recognized as Description
0 Dummy for pdi builders Dummy for pdi builder
1 Cloud Veronte Cloud address
2 Vlink Address used by Veronte Link app to communicate with Veronte units
2-3 App + Address Veronte applications addresses. App 2 is the one used by default by Veronte applications, although App 3 is also available
255-511 App dynamic + Address Dynamic addresses for Veronte applications
998 Broadcast To all devices on a network
999 Address unknown This address can be used for a device that does not have a valid address configured
1000-1777 1x v4.0 + Address Specific address of an Autopilot 1x with hardware version 4.0
1778-3999 1x v4.5 + Address Specific address of an Autopilot 1x with hardware version 4.5
4000-17999 1x v4.8 + Address Specific address of an Autopilot 1x with hardware version 4.8
18000-19899 1x BCS + Address Specific address of a BCS unit
19900-19999 1x v4.7. For internal use only + Address Specific address of an Autopilot 1x with hardware version 4.7
20000-21999 Smart Can Isolator + Address Specific address of a Smart Can Isolator unit
30000-31999 MC01 + Address Specific address of a MC01 unit
32000-34999 MC24 motor controller + Address Specific address of a MC24 unit
35000-39999 MC110 motor controller + Address Specific address of a MC110 unit
40000-41999 CEX + Address Specific address of a CEX with hardware version 1.2
42000-43999 MEX + Address Specific address of a MEX unit
44000-49999 CEX2 + Address Specific address of a CEX with hardware version 2.0
50000-51089 Arbiter v1.0 + Address Specific address of an Arbiter with hardware version 1.0
51090-51999 Arbiter v1.2 + Address Specific address of an Arbiter with hardware version 1.2
52000-59999 Arbiter v1.8 + Address Specific address of an Arbiter with hardware version 1.8
60000-65535 Reserved + Address Reserved addresses
65536-69631 Virtual v4.0 + Address Specific address of a Virtual Autopilot 1x with hardware version 4.0
69632-73727 Virtual v4.5 + Address Specific address of a Virtual Autopilot 1x with hardware version 4.5
73728-77823 Virtual v4.8 + Address Specific address of a Virtual Autopilot 1x with hardware version 4.8

Lists of Variables

This section shows all the variables employed by Veronte Autopilot 1x. All of them can be read and sent through telemetry.

These variables are classified into two main groups:

  • System variables: Non-writable by the user.
  • User variables: Writable by the user, marked in the tables below as 📝.

Important

Variables labeled as "Deprecated" are no longer used by the system.

In order to avoid system incompatibilities, deprecated variables are only written by the autopilot when migrating a configuration from a previous version in which the variable was not obsolete.
When a configuration is built from scratch, these variables must be defined by the user to be used.
Thus, users are responsible for their correct assignment.

BIT Variables

Warning

Bit Variables displayed on Veronte Ops labels will be shown as Red/Green depending on their state.
Red stands for 0 and Green for 1, changing the name displayed accordingly to the BIT value.

ID Name Description
0 Always Fail This signal is always fail - 0 for fail, 1 for OK
1 Always OK This signal is CIO always OK - 0 for fail, 1 for OK
2 License Check Pending License state - 0 for license check pending, 1 for license checked
3 System Not Ready to Start System is ready to start operating - 0 for not ready, 1 for ready
4 No Writing Telemetry Telemetry is properly sending/receiving - 0 for no, 1 for yes
5 Power Error Power supply state - It will be 0 if any of the following conditions happens:

  • Bit 117 is zero (power for Veronte has a failure)
  • Bit 118 is zero (power for SuC has a failure)
6 File System Error System file manager - Dependent on File system status (UVar 96)

  • 0 for error: if File system status > 0
  • 1 for running OK: if File system status == 0
7 System Error This bit checks whether the system is running properly. 0 for system error, 1 for system OK.
8 Memory allocation RAM allocation - 0 for trying to use more than available memory, 1 for running
9 PDI Error PDI files - Dependent on PDI Error Source (UVar 50)

  • 0 for wrong PDI configuration: if PDI Error Source > 0
  • 1 for running OK: if PDI Error Source == 0
10 CIO Low or C2 Error (Deprecated) CIO low or C2 failed. Bits 400 and 401 are recommended instead
- 0 for CIO low or C2 failed, 1 for CIO high and C2 OK

Warning
Deprecated variable
11 4X CAN failed For more information, check BIT Variables - 4x Software Manual
12 System Power up BIT Error Power up - 0 for error, 1 for OK
13 Reset and Write Disabled Reset and non-operation PDI writes are allowed - 0 for disabled, 1 for enabled
14 FTS-1 Feedback (>=V4.5) Flight Termination System 1, microcontroller state for hardware version 4.7 or higher - 0 for error, 1 for running OK
15 FTS-2 Feedback (>=V4.5) Flight Termination System 2, microcontroller state for hardware version 4.7 or higher - 0 for error, 1 for running OK
16 Stack C1 usage FAIL 0 for stack overflow of core 1, 1 for OK
17 Stack C2 usage FAIL 0 for stack overflow of core 2, 1 for OK
18 PDI disabled PDI Mode - 0 for disabled, 1 for enabled
📝
20-46
4xV Bit variables For more information, check BIT Variables - 4x Software Manual
47 4xV Watchdog Error
Note
For version 4.7 or higher

For more information, check BIT Variables - 4x Software Manual
49 CPU temperature above 398.15K CPU temperature warning - 0 for CPU temperature above 398.15K (125ºC), 1 for CPU temperature below 398.15K (125ºC)
50 Sensors Error Sensors state - 0 for error, 1 for running OK
Selected sensors are not working or, if external sensors have been selected, they are not connected
51 Sensor-Main IMU Sensor IMU 0 - 0 for disabled, 1 for enabled
52 Sensor-Secondary IMU Sensor IMU 1 - 0 for disabled, 1 for enabled
53 Sensor-Internal Magnetometer (LIS3MDL) Internal 0 Magnetometer - 0 for disabled, 1 for enabled
54 Sensor-External Magnetometer (HMR2300) External HMR2300 magnetometer - 0 for disabled, 1 for enabled
55 Sensor-External Magnetometer (LIS3MDL) External LIS3MDL magnetometer - 0 for disabled, 1 for enabled
56 Sensor-Static pressure (HSC) Static Pressure Sensor 0 - 0 for disabled, 1 for enabled
57 Sensor-Static pressure (MS56) Static Pressure Sensor 1 - 0 for disabled, 1 for enabled
58 Sensor-Dynamic pressure (HSC) Dynamic Pressure Sensor 0 - 0 for disabled, 1 for enabled
59 Sensor-External I2C devices 0 for disabled, 1 for enabled
60-64 Sensor-External I2C device 0-4 External communication I2C from device 0 to 4
65 SCI-A Transmitting (LTE/EXT. UART) Serial Communication Interface - LTE/EXT. UART transmission
66 SCI-A Receiving (LTE/EXT. UART) Serial Communication Interface - LTE/EXT. UART reception
0 for not receiving, 1 for receiving
67 SCI-B Transmitting (LOS) Serial Communication Interface - LOS transmission
68 SCI-B Receiving (LOS) Serial Communication Interface - LOS reception
0 for not receiving, 1 for receiving
69 SCI-C Transmitting (RS485) Serial Communication Interface - RS485 transmission
70 SCI-C Receiving (RS485) Serial Communication Interface - RS485 reception
0 for not receiving, 1 for receiving
71 SCI-D Transmitting (RS232) Serial Communication Interface - RS232 transmission
72 SCI-D Receiving (RS232) Serial Communication Interface - RS232 reception
0 for not receiving, 1 for receiving
73 CAN-A ERROR CAN A state - 0 for error, 1 for OK
74 CAN-B ERROR CAN B state - 0 for error, 1 for OK
75 CAN-A Warning CAN A state - 0 for warning, 1 for OK
76 CAN-B Warning CAN B state - 0 for warning, 1 for OK
77 Vectornav GPS not fixed 0 for not fixed, 1 for fix
78 Vectornav IMU error 0 for error, 1 for OK
79 Vectornav Mag/Press error 0 for error, 1 for OK
80 Vectornav GPS error 0 for error, 1 for OK
81 Vectornav Navigation Error Navigation state - 0 for error, 1 for OK
82 Sensor-External Magnetometer (HSCDTD008A) External HSCDTD008A magnetometer - 0 for error, 1 for OK
83 IMU 2 BMI088 Sensor IMU 2 - 0 for error, 1 for OK
84 Sensor-Static pressure 2 (DPS310) Static Pressure Sensor 2 - 0 for error, 1 for OK
85 Sensor-Internal Magnetometer (MMC5883MA) Internal 1 Magnetometer - 0 for error, 1 for OK
86 Sensor-External Magnetometer (MMC5883MA) External MMC5883MA magnetometer - 0 for error, 1 for OK
87 GNSS1 Module Error GPS module 1 state - 0 for error, 1 for OK
88 GNSS2 Module Error GPS module 2 state - 0 for error, 1 for OK
89 Sensor-External Magnetometer (RM3100) External RM3100 magnetometer - 0 for error, 1 for OK
90 IMU3 ADIS16505-3 (MCBSP) Sensor IMU 3 - 0 for error, 1 for OK
91 Sensor-Internal Magnetometer (RM3100) Internal 2 Magnetometer - 0 for error, 1 for OK
92 Magnetometer reserved 0 for error, 1 for OK
93 SCI Expander (v4.7+) SCI Expander for hardware version 4.7 or higher - 0 for error, 1 for OK
96 SCI-A Error (LTE/EXT. UART) SCI A (LTE/EXT. UART) state - 0 for error in this port (invalid format or configuration), 1 for OK
97 SCI-B Error (LOS) SCI B (LOS) state - 0 for error in this port (invalid format or configuration), 1 for OK
98 SCI-C Error (RS485) SCI C (RS485) state - 0 for error in this port (invalid format or configuration), 1 for OK
99 SCI-D Error (RS232) SCI D (RS232) state - 0 for error in this port (invalid format or configuration), 1 for OK
100 Position not fixed GNSS data reception - 0 for not receiving, 1 for receiving (Position fixed)
101 No valid SRTM at UAV position 0 for not valid, 1 for valid
102-103 CAN A-B Receiving CAN A to B communication - 0 for not receiving, 1 for receiving
104-105 Stick PPM 0-1 not detected Stick PPM 0 to 1 - 0 for not detecting, 1 for detecting
106 Magnetic field out of bounds (Deprecated) 0 for magnetic field out of bounds, 1 for OK

Warning
Deprecated variable
107 INS navigation OFF 0 for INS navigation OFF, 1 for INS navigation ON
113 Iridium Ready Iridium ready state - 0 for not ready, 1 for ready
114 No valid Geoid at UAV position 0 for no valid geoid at UAV position, 1 for valid geoid at UAV position
115 EKF: Condition Number Error Extended Kalman Filter state - 0 for error, 1 for running
116 Radar Altimeter CAN-RX Error Radar Altimeter State - 0 for error, 1 for running
117 Main Power Error Main power supply A. It will be 0 (indicating error state) if any of the following errors happen:

  • Input supply voltage is not between 6.5 and 36 V. This voltage is measured by RVar 400.
  • Voltage received by Veronte through 5V port is not between 4.75 and 5.25 V. This voltage is measured by RVar 402.
  • Voltage received by Veronte through 3.6V port is not between 3.42 and 3.78V. This voltage is measured by RVar 404.
118 SUC Power Error Power supply for system on microchip. It will be 0 (indicating error state) if any of the following errors happen:

  • Voltage received by Veronte through 3.3V port is out of range. This voltage is measured by RVar 401.
  • Voltage received by Veronte SUC is out of range. This voltage is measured by RVar 403.
119 Not hovering guidance Hovering guidance state - 0 for hovering guidance disabled, 1 for enabled
120-123 Pulse 0-3 not detected Pulse 0 to 3 detection - 0 for pulse not detected, 1 for detected
📝
124-129
4xV Bit variables For more information, check BIT Variables - 4x Software Manual
130 EFK Navigation Error Extended Kalman Filter navigation state - 0 for error, 1 for running
131 No magnetic field data Bit to indicate if there is magnetic field in the SD - 0 for No Magnetic field data, 1 for Magnetic field data OK
132 Route not finished 0 for Route not finished, 1 for Route finished OK
150 External VCP Navigation Error External VCP state - 0 for error, 1 for OK
📝
160
External Var Navigation Error External Navigation state - 0 for error, 1 for running
170 Selected Accelerometer Error Selected accelerometer - 0 for error, 1 if at least one of the selected accelerometers is OK
171 Selected Gyroscope Error Selected gyroscope - 0 for error, 1 if at least one of the selected gyroscopes is OK
172 Bias Accelerometer Saturated 0 for bias saturated, 1 for OK
173 Bias Gyroscope Saturated 0 for bias saturated, 1 for OK
📝
180
External attitude Kind of attitude calculation - 0 for external, 1 for internal
182 FTS Activation (>=V4.5) Flight Termination System activation, for version 4.5 or higher - 0 for not activated, 1 for activated
183 4X Selected Current 1x Autopilot is the one selected by the arbiter - 0 when this AP is not the selected AP, 1 when this AP is the selected one
188 BIT for static pressure sensors Error 0 for static pressure sensors error, 1 for OK
189 BIT for magnetometer sensors Error 0 for magnetometer sensors error, 1 for OK
190 Internest ultrasound position status Error 0 for internest ultrasound position error, 1 for OK
191 Internest ultrasound angle status Error 0 for internest ultrasound angle error, 1 for OK
200 GNSS1 Navigation Down 0 for GNSS navigation OFF, 1 for GNSS navigation ON
201 DGNSS1 Input Off 0 for GNSS compass or RTK not activated, 1 for one of them activated
202 DGNSS1 Navigation Off 0 for GNSS compass or RTK not activated, 1 for one of them activated
203 GNSS1 Survey In Off GNSS compass survey or RTK OFF, 1 for one of them ON
204 No DGNSS1 Float Solution 0 for no DGNSS1 float solution nor RTK, 1 for DGNSS1 float solution or RTK
205 No DGNSS1 Fixed Solution 0 for no DGNSS1 fixed solution nor RTK, 1 for DGNSS1 fixed solution or RTK
206 DGNSS1 Relative Position Invalid 0 for invalid navigation position, 1 for valid navigation position
207 DGNSS1 not Moving baseline mode 0 for not moving baseline mode, 1 for moving baseline mode
210 DMA peripheral for SPIA A Error DMA peripheral for SPIA A - 0 for error, 1 for OK
211 DMA peripheral for MCBSP A Error DMA peripheral for MCBSP A - 0 for error, 1 for OK
📝
230-293
4xV Bit variables For more information, check BIT Variables - 4x Software Manual
300 GNSS2 Navigation Down 0 for GNSS navigation OFF, 1 for GNSS navigation ON
301 DGNSS2 Input Off 0 for GNSS compass or RTK not activated, 1 for one of them activated
302 DGNSS2 Navigation Off 0 for GNSS compass or RTK not activated, 1 for one of them activated
303 GNSS2 Survey In Off GNSS compass survey or RTK OFF, 1 for one of them ON
304 No DGNSS2 Float Solution 0 for no DGNSS2 float solution nor RTK, 1 for DGNSS2 float solution or RTK
305 No DGNSS2 Fixed Solution 0 for no DGNSS2 fixed solution nor RTK, 1 for DGNSS2 fixed solution or RTK
306 DGNSS2 Relative Position Invalid 0 for invalid navigation position, 1 for valid navigation position
307 DGNSS2 not Moving baseline mode 0 for not moving baseline mode, 1 for moving baseline mode
308 SCI-E Transmitting (LTE) SCI-E Transmitting (LTE)
309 SCI-E Receiving (LTE) SCI-E Receiving (LTE)
310 SCI-F Transmitting (LTE Aux.) SCI-F Transmitting (LTE Aux.)
311 SCI-F Receiving (LTE Aux.) SCI-F Receiving (LTE Aux.)
312 SCI E Error (LTE) SCI-E (LTE) - 0 for error, 1 for OK
313 SCI F Error (LTE Aux.) SCI-F (LTE Aux.) - 0 for error, 1 for OK
329 3.3V Power Source 0 for error, 1 for OK
330 Jetibox COMM Error Jetibox is communicating properly - 0 for error, 1 for OK
370-371 Smart Can Isolator A-B Domain Error 0 for error, 1 for OK
400 C1 Low Frequency C1 Low Frequency - Dependent on CIO Running Frequency (RVar 2057) (C1 low frequency)

  • 0 for error → CIO Running Frequency < 10 Hz
  • 1 for OK → CIO Running Frequency > 10 Hz
401 GNC fail 0 for error ('dead'), 1 for ok ('alive') - Dependent on Counter for C2 system (UVar 20)
402 Acquisition step missed
  • 0 for Acquisition step missed → C1 hi frequency fluctuation is higher than permitted (1%).
  • 1 for Acquisition Task OK → C1 hi frequency fluctuation is under set limits (1%).
403 CIO Hi Overload warning C1 hi Overload - Dependent on Acquisition Task Maximum CPU Ratio (RVar 2051)

  • 0 for Acquisition Task overload → Acquisition Task Maximum CPU Ratio > 90%
  • 1 for Acquisition Task usage OK → Acquisition Task Maximum CPU Ratio ≤ 90%
Note
Non-recoverable variable
404 GNC Realtime Error
  • 0 if C2 frequency < configured frequency (tolerance of 6 microseconds)
  • 1 if C2 frequency = configured frequency (tolerance of 6 microseconds)
405 Reserved 0 for error, 1 for OK
480 MC01 Stepper direction output 0 for error, 1 for OK
481 MC01 Brushless driver fault 0 for error, 1 for OK
482 MC Hall Sensor error 0 for error, 1 for OK
483 MC Sin/Cos Sensor error 0 for error, 1 for OK
484 MC general health error 0 for health error, 1 for status OK
485 MC Current sensing error 0 for error, 1 for OK
486 MC Phase U Current Calibration Error ADC phase U not calibrated - 0 for not calibrated, 1 for calibration OK
487 MC Phase V Current Calibration Error ADC phase V not calibrated - 0 for not calibrated, 1 for calibration OK
488 MC Phase W Current Calibration Error ADC phase W not calibrated - 0 for not calibrated, 1 for calibration OK
489 MC Maximum Temperature Error Maximum power module temperature exceeded - 0 for error (exceeded), 1 for OK
490 MC Phase Error Power module driver phase error reported - 0 for error, 1 for OK
491 MC General Driver Error Power module driver error reported - 0 for error, 1 for OK
492 MC Over-current AC Current AC side limit exceeded - 0 for error (exceeded), 1 for OK
493 MC Over-voltage advertisement Over-voltage DC side limit advertisement exceeded - 0 for error (exceeded), 1 for OK
494 MC Over-voltage caution Over-voltage DC side limit caution exceeded - 0 for error (exceeded), 1 for OK
495 MC Under-voltage latching Critical under-voltage DC side limit violation - 0 for error, 1 for OK
496 MC Under-voltage non latching Non critical under-voltage DC side limit violation - 0 for error, 1 for OK
497 MC RMS imbalance Current AC side imbalance - 0 for error, 1 for OK
498 MC Open DC fault Open-circuit DC side fault - 0 for error, 1 for OK
499 MC Over-current DC Current DC side limit exceeded - 0 for error (exceeded), 1 for OK
📝
500
Ground effect compensation variance disabled 0 for disabled, 1 for enabled
📝
501
Ground effect compensation measurement disabled 0 for disabled, 1 for enabled
502 No SRTM data Bit to indicate if there is SRTM in the SD - 0 for No SRTM data, 1 for SRTM data OK
503 No geoid data Bit to indicate if there is Geoid data in the SD - 0 for No geoid data, 1 for Geoid data OK
600 Wind Estimation Off 0 for disabled, 1 for enabled
📝
700-731
Servo 0-31 Saturated 0 for saturated, 1 for OK
📝
800-815
PWM 0-15 GPIO Off PWM GPIO 0-15 communication State - 0 for Off, 1 for On
📝
816-819
EQEP_A-I (GPIO 17-20) Off Input/Output State - 0 for Off, 1 for On
820-822 RSSI LED 0-2 Off Received Signal Strength Indicator led state - 0 for Off, 1 for On
📝
823
GPIO 5 (GPIO28) Off GPIO 5 Status (Low/High) - 0 for Off, 1 for On
📝
824
GPIO 6 (GPIO61) Off GPIO 6 Status (Low/High) - 0 for Off, 1 for On
📝
825
GPIO 7 (GPIO60) Off GPIO 7 Status (Low/High) - 0 for Off, 1 for On
📝
826
GPIO 8 (GPIO59) Off GPIO 8 Status (Low/High) - 0 for Off, 1 for On
📝
827
GPIO 9 (GPIO17) Off GPIO 9 Status (Low/High) - 0 for Off, 1 for On
📝
828
GPIO 10 (GPIO58) Off GPIO 10 Status (Low/High) - 0 for Off, 1 for On
📝
829
GPIO 11 (GPIO16) Off GPIO 11 Status (Low/High) - 0 for Off, 1 for On
📝
830
GPIO 12 (GPIO53) Off GPIO 12 Status (Low/High) - 0 for Off, 1 for On
📝
831
GPIO 13 (GPIO20) Off GPIO 13 Status (Low/High) - 0 for Off, 1 for On
📝
832
GPIO 14 (GPIO23) Off GPIO 14 Status (Low/High) - 0 for Off, 1 for On
📝
833
GPIO 15 (GPIO51) Off GPIO 15 Status (Low/High) - 0 for Off, 1 for On
📝
834
GPIO 16 (GPIO52) Off GPIO 16 Status (Low/High) - 0 for Off, 1 for On
📝
835
GPIO 17 (GPIO49) Off GPIO 17 Status (Low/High) - 0 for Off, 1 for On
📝
836
GPIO 18 (GPIO08) Off GPIO 18 Status (Low/High) - 0 for Off, 1 for On
📝
837
GPIO 19 (GPIO11) Off GPIO 19 Status (Low/High) - 0 for Off, 1 for On
📝
838
GPIO 20 (GPIO10) Off GPIO 20 Status (Low/High) - 0 for Off, 1 for On
📝
839
GPIO 21 (GPIO09) Off GPIO 21 Status (Low/High) - 0 for Off, 1 for On
📝
900-931
Virtual GPIO 00-31 off Virtual GPIO 00-31 Status (Low/High) - 0 for Off, 1 for On
1000-1009 Simulation BIT 00-09 Error 0 for error, 1 for OK
1010-1113 Custom msg 0-103 Rx Error Custom message timeout - 0 for error, 1 for OK
📝
1120-1121
Entrance EKF GNSS1-2 OFF GNSS 1-2 information considered in EKF Navigation - 0 for entrance EKF GNSS OFF, 1 for ON
EKF GNSS OFF may be because Position not fixed → EKF deactivated → INSS activated
📝
1122
Entrance EKF GNSS3 EXT OFF External GNSS information considered in EKF Navigation - 0 for entrance EKF GNSS EXT OFF, 1 for ON
📝
1123
Entrance EKF Internest OFF Internest information considered in EKF Navigation - 0 for entrance EKF internest OFF, 1 for ON
📝
1124
Entrance EKF GPSCOMPASS OFF GNSS Compass information considered in EKF Navigation - 0 for entrance EKF GPSCOMPASS OFF, 1 for ON
📝
1125
Entrance EKF Magnetometer OFF Magnetometer information considered in EKF Navigation - 0 for entrance EKF magnetometer OFF, 1 for ON
📝
1126
Entrance EKF Static press OFF Static Pressure sensor information considered in EKF Navigation - 0 for entrance EKF static pressure OFF, 1 for ON
📝
1127
Entrance EKF Altimeter press OFF Altimeter information considered in EKF Navigation - 0 for entrance EKF altimeter OFF, 1 for ON
📝
1128
Entrance EKF Radar-altimeter press OFF Radar Altimeter information considered in EKF Navigation - 0 for entrance EKF radar-altimeter OFF, 1 for ON
📝
1129
Entrance EKF DEM OFF DEM information considered in EKF Navigation - 0 for entrance EKF DEM OFF, 1 for ON
📝
1174
External IMU 0 accelerometer error External IMU 0 accelerometer - 0 for error, 1 for OK
📝
1175
External IMU 0 gyroscope error External IMU 0 gyroscope - 0 for error, 1 for OK
📝
1176
External IMU 1 accelerometer error External IMU 1 accelerometer - 0 for error, 1 for OK
📝
1177
External IMU 1 gyroscope error External IMU 1 gyroscope - 0 for error, 1 for OK
📝
1178
External magnetometer 0 error External magnetometer 0 - 0 for error, 1 for OK
📝
1179
External magnetometer 1 error External magnetometer 1 - 0 for error, 1 for OK
📝
1180-1181
Sniffer msg 0-1 Rx Error Sniffer receiver message 0-1 - 0 for error, 1 for OK
📝
1200-1499
User BIT 00-299 error User bit 0 to 299 - 0 for error, 1 for OK
2200 BIT Dummy Error Bit for configurable checks - 0 for error, 1 for OK

Real Variables (RVar) - 32 Bits

ID Name Units/Values Description
0 IAS (Indicated Airspeed) m/s Pitot-static measurement speed
1 TAS (True Airspeed) 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 rad Direction in which the vehicle velocity vector is pointing
4 Flight Path Angle rad Angle between velocity vector and local horizontal line
5 Bank rad Angle around the Longitudinal Euler axis
6 Yaw rad Angle around the Vertical Euler axis
7 Pitch rad Angle around the Transverse Euler axis
8 Roll rad Angle around the Longitudinal Euler axis
9 Route-Guidance Tangential deviation m Tangencial distance to the desired position (guidance)
10 Route-Guidance Horizontal deviation m Horizontal distance to the desired position (guidance)
11 Route-Guidance Perpendicular deviation m Perpendicular distance to the desired position (guidance)
12 p (Angular Velocity - X Body Axis) rad/s Angular velocity around longitudinal axis
13 q (Angular Velocity - Y Body Axis) rad/s Angular velocity around lateral axis
14 r (Angular Velocity - Z Body Axis) rad/s Angular velocity around vertical axis
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 Ground Velocity m/s GV vector X component
20 Lateral 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 Estimated air density kg/m³ Estimated air density at current altitude
28 Co-Yaw rad Acrobatic Yaw with Body Z' axis pointing to X
29 Co-Pitch rad Acrobatic Pitch with Body X' axis pointing to -Z
30 Co-Roll rad Acrobatic Roll with Y' keeping same as Y
31 Angular Acceleration - X Body Axis rad/s² Acceleration around the longitudinal axis
32 Angular Acceleration - Y Body Axis rad/s² Acceleration around the lateral axis
33 Angular Acceleration - Z Body Axis rad/s² Acceleration around the vertical axis
34 Body to NED Quaternion qs customType First component of body to NED orientation quaternion
35 Body to NED Quaternion qi customType Second component of body to NED orientation quaternion
36 Body to NED Quaternion qj customType Third component of body to NED orientation quaternion
37 Body to NED Quaternion qk customType Fourth component of body to NED orientation quaternion
40 RSSI percentage Received Signal Strength Indicator

Warning
Deprecated variable
42 SCI-A Rx Rate (LTE/EXT. UART) bytes/s Reception rate (in bytes per second) of 4G (hwv < 4.7) or external UART (hwv >=4.7) communications
43 SCI-A Tx Rate (LTE/EXT. UART) bytes/s Transmission rate (in bytes per second) of 4G (hwv < 4.7) or external UART (hwv >=4.7) communications
44 SCI-B Rx Rate (LOS) bytes/s Radio link reception byte rate
45 SCI-B Tx Rate (LOS) bytes/s Radio link transmission byte rate
46 SCI-C Rx Rate (RS485) bytes/s RS485 communication reception byte rate
47 SCI-C Tx Rate (RS485) bytes/s RS485 communication transmission byte rate
48 SCI-D Rx Rate (RS232) bytes/s RS232 communication reception byte rate
49 SCI-D Tx Rate (RS232) bytes/s RS232 communication transmission byte rate
50 CAN-A Tx Rate pkts/s CAN-A transmission packet rate
51 CAN-B Tx Rate pkts/s CAN-B transmission packet rate
52 CAN-A Tx skip Rate pkts/s CAN-A messages delayed because no mailbox is available for sending
53 CAN-B Tx skip Rate pkts/s CAN-B messages delayed because no mailbox is available for sending
56 Yaw Rate rad/s Rate of change of the yaw angle
57 Pitch Rate rad/s Rate of change of the pitch angle
58 Roll Rate rad/s Rate of change of the roll angle
59-64 COM 0-5 Parse Error Rate messages Each COM discard packages with these frequencies. Messages might be discarded because the calculated and the received CRC are different
65 GNSS Absolute Time Of Week Milliseconds as Unit32 customType Time of the week expressed with milliseconds
66 GNSS Hours in the Current Day customType Elapsed hours in the current day
67 GNSS Minutes in the Current Hour customType Elapsed minutes in the current hour
68 GNSS Seconds in the Current Minute customType Elapsed seconds in the current minute
80 Estimated gyro bias x rad/s Gyro bias estimated during IMU calibration
81 Estimated gyro bias y rad/s Gyro bias estimated during IMU calibration
82 Estimated gyro bias z rad/s Gyro bias estimated during IMU calibration
83 Estimated accelerometer bias x m/s² Accelerometer bias estimated during IMU calibration
84 Estimated accelerometer bias y m/s² Accelerometer bias estimated during IMU calibration
85 Estimated accelerometer bias z m/s² Accelerometer bias estimated during IMU calibration
90 SCI-E Rx Rate (LTE) bytes/s Reception rate (in bytes per seconds) of the first channel (port0) of the SCI expander (hwv >=4.7)
91 SCI-E Tx Rate (LTE) bytes/s Transmission rate (in bytes per seconds) of the first channel (port0) of the SCI expander (hwv >=4.7)
92 SCI-F Rx Rate (LTE Aux.) bytes/s Reception rate (in bytes per seconds) of the second channel (port1) of the SCI expander (hwv >=4.7)
93 SCI-F Tx Rate (LTE Aux.) bytes/s Transmission rate (in bytes per seconds) of the second channel (port1) of the SCI expander (hwv >=4.7)
📝
100
Desired IAS (Indicated Airspeed) m/s Commanded IAS from guidance
📝
101
Desired TAS (True Airspeed) m/s Commanded TAS from guidance
📝
102
Desired GS (Ground Speed) m/s Commanded GS from guidance
📝
103
Desired Heading rad Commanded Heading from guidance
📝
104
Desired Flight Path Angle rad Commanded Flight Path Angle from guidance
📝
105
Desired Bank rad Commanded Bank from guidance
📝
106
Desired Yaw rad Commanded Yaw from guidance
📝
107
Desired Pitch rad Commanded Pitch from guidance
📝
108
Desired Roll rad Commanded Roll from guidance
📝
112
Desired p (Angular Velocity - X Body Axis) rad/s Commanded angular velocity around longitudinal axis
📝
113
Desired q (Angular Velocity - Y Body Axis) rad/s Commanded angular velocity around lateral axis
📝
114
Desired r (Angular Velocity - Z Body Axis) rad/s Commanded angular velocity around vertical axis
📝
115
Desired Forward 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 Commanded RPM from guidance
📝
119
Desired Front Ground Velocity m/s Commanded Front GV from guidance
📝
120
Desired Lateral 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 Factor from guidance
📝
125
Desired Tangential Acceleration m/s² Commanded Tangential Acceleration from guidance
📝
126
Energy Rate Error customType Rate of change of the Total System Energy
📝
127
Energy Distribution Error customType Distribution of system energy between kinetical and geopotential energy
📝
128
Desired Co-Yaw rad Commanded co-yaw from guidance
📝
129
Desired Co-Pitch rad Commanded co-pitch from guidance
📝
130
Desired Co-Roll rad Commanded co-roll from guidance
📝
140
Climbing Initial Heading rad Heading in climbing phase (start of the route)
📝
141
Approach Initial Heading rad Heading in approach phase (end of the route)
📝
142
Headwind Direction rad Wind direction estimation
📝
143
Tailwind Direction rad Angle of the vector that would correspond to the opposite of the Headwind vector
📝
144
Runway Direction rad Runway angle
📝
145
Elevation of current route rad Elevation of tangent to current route at its closest point to desired position
📝
146
Azimuth of current route rad Azimuth of tangent to current route at its closest point to desired position
📝
147
Distance to closest obstacle m Signed distance to closest obstacle (negative means inside)
📝
148
Distance of obstacle repulsion m Distance at which the obstacles have an effect in the guidance
📝
200
Desired North Ground Velocity m/s Commanded North (NED Coordinates system) GV from guidance
📝
201
Desired East Ground Velocity m/s Commanded East (NED Coordinates system) GV from guidance
📝
202
Desired Down Ground Velocity m/s Commanded Down (NED Coordinates system) GV from guidance
📝
203
Desired 2D MSL (Height 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 rad Commanded Longitude from guidance
📝
207
Desired Latitude rad 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 rad Yaw from external navigation source
📝
260
External Pitch rad Pitch from external navigation source
📝
261
External Roll rad 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 GNSS Time of Week s GNSS Time of week from external navigation source
300 Relative Timestamp s 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 Pa Physical measurement from Pitot (dynamic pressure)
📝
304
Static Pressure (Deprecated) Pa Physical measurement from Pitot (static preassure)

Warning
Deprecated variable
305 Internal Temperature K Physical measurement from internal sensors
306 External Temperature 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 Gyroscope measurement for X axis
311 Gyroscope - Y Body Axis rad/s Gyroscope measurement for Y axis
312 Gyroscope - Z Body Axis rad/s Gyroscope measurement for Z axis
📝
313
Magnetometer - X Body Axis T Magnetometer measurement for X axis

Warning
Deprecated variable
📝
314
Magnetometer - Y Body Axis T Magnetometer measurement for Y axis

Warning
Deprecated variable
📝
315
Magnetometer - Z Body Axis T Magnetometer measurement for Z axis

Warning
Deprecated variable
322 Internal LIS3MDL Magnetometer Raw X in SI T Internal 0 Magnetometer raw measurement for X axis
323 Internal LIS3MDL Magnetometer Raw Y in SI T Internal 0 Magnetometer raw measurement for Y axis
324 Internal LIS3MDL Magnetometer Raw Z in SI T Internal 0 Magnetometer raw measurement for Z axis
325 Internal LIS3MDL Magnetometer Temperature K Internal 0 Magnetometer temperature
326 External LIS3MDL Magnetometer Raw X in SI T External LIS3MDL Magnetometer raw measurement for X axis
327 External LIS3MDL Magnetometer Raw Y in SI T External LIS3MDL Magnetometer raw measurement for Y axis
328 External LIS3MDL magnetometer raw Z in SI T External LIS3MDL Magnetometer raw measurement for Z axis
329 External LIS3MDL magnetometer temperature K External LIS3MDL 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 IMU 0 raw gyroscope x measurement
334 IMU 0 Raw Gyroscope Y Measurement rad/s IMU 0 raw gyroscope y measurement
335 IMU 0 Raw Gyroscope Z Measurement rad/s IMU 0 raw gyroscope z measurement
336 IMU 0 temperature measurement 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 IMU 1 raw gyroscope x measurement
341 IMU 1 Raw Gyroscope Y Measurement rad/s IMU 1 raw gyroscope y measurement
342 IMU 1 Raw Gyroscope Z Measurement rad/s IMU 1 raw gyroscope z measurement
343 IMU 1 temperature Measurement K IMU 1 temperature measurement
344 Static Pressure Sensor (MS56) Raw Measurement Pa Static pressure sensor 1 raw measurement
345 Static Pressure Sensor (MS56) Temperature K Static pressure sensor 1 temperature
346 Dynamic Pressure Sensor Raw Measurement Pa Dynamic pressure sensor 1 raw measurement
347 Dynamic Pressure Sensor Temperature K Dynamic pressure sensor 1 temperature
348 Static Pressure Sensor (HSC) Raw Measurement Pa Static pressure sensor 0 raw measurement
349 Static Pressure Sensor (HSC) Temperature K Static pressure sensor 0 temperature
350 Vectornav Message Frequency Hz External navigation source VectorNav sends messages with this frequency
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 rad/s Raw gyroscope X measurement from external navigation source VectorNav
355 Vectornav Raw Gyr Y Measurement rad/s Raw gyroscope Y measurement from external navigation source VectorNav
356 Vectornav Raw Gyr Z Measurement rad/s Raw gyroscope Z measurement from external navigation source VectorNav
357 External HSCDTD008A Magnetometer Raw X in SI T External HSCDTD008A Magnetometer raw measurement for X axis
358 External HSCDTD008A Magnetometer Raw Y in SI T External HSCDTD008A Magnetometer raw measurement for Y axis
359 External HSCDTD008A Magnetometer Raw Z in SI T External HSCDTD008A Magnetometer raw measurement for Z axis
360 External HSCDTD008A Magnetometer Temperature K External HSCDTD008A Magnetometer temperature
361 IMU 2 Raw Accelerometer X Measurement m/s² IMU 2 raw accelerometer x measurement
362 IMU 2 Raw Accelerometer Y Measurement m/s² IMU 2 raw accelerometer y measurement
363 IMU 2 Raw Accelerometer Z Measurement m/s² IMU 2 raw accelerometer z measurement
364 IMU 2 Raw Gyroscope X Measurement rad/s IMU 2 raw gyroscope x measurement
365 IMU 2 Raw Gyroscope Y Measurement rad/s IMU 2 raw gyroscope y measurement
366 IMU 2 Raw Gyroscope Z Measurement rad/s IMU 2 raw gyroscope z measurement
367 IMU 2 Temperature Measurement K IMU 2 temperature measurement
368 Static Pressure Sensor (DPS310) Raw Measurement Pa Static pressure sensor 2 raw measurement
369 Static Pressure Sensor (DPS310) Temperature K Static pressure sensor 2 temperature
370 Internal Magnetometer MMC5883MA Raw Measure X Converted to SI T Internal 1 Magnetometer raw measurement for X axis converted to SI
371 Internal Magnetometer MMC5883MA Raw Measure Y Converted to SI T Internal 1 Magnetometer raw measurement for Y axis converted to SI
372 Internal Magnetometer MMC5883MA Raw Measure Z Converted to SI T Internal 1 Magnetometer raw measurement for Z axis converted to SI
373 Internal Magnetometer MMC5883MA Temperature K Internal 1 Magnetometer temperature
374 External Magnetometer MMC5883MA Raw Measure X Converted to SI T External MMC5883MA Magnetometer raw measurement for X axis converted to SI
375 External Magnetometer MMC5883MA Raw Measure Y Converted to SI T External MMC5883MA Magnetometer raw measurement for Y axis converted to SI
376 External Magnetometer MMC5883MA Raw Measure Z Converted to SI T External MMC5883MA Magnetometer raw measurement for Z axis converted to SI
377 External Magnetometer MMC5883MA Temperature K External MMC5883MA Magnetometer temperature
378 External Magnetometer RM3100 Raw Measure X Converted to SI T External RM3100 Magnetometer raw measurement for X axis converted to SI
379 External Magnetometer RM3100 Raw Measure Y Converted to SI T External RM3100 Magnetometer raw measurement for Y axis converted to SI
380 External Magnetometer RM3100 Raw Measure Z Converted to SI T External RM3100 Magnetometer raw measurement for Z axis converted to SI
382 External Magnetometer HMR2300 Raw Measure X Converted to SI T External HMR2300 Magnetometer raw measurement for X axis converted to SI
383 External Magnetometer HMR2300 Raw Measure Y Converted to SI T External HMR2300 Magnetometer raw measurement for Y axis converted to SI
384 External Magnetometer HMR2300 Raw Measure Z Converted to SI T External HMR2300 Magnetometer raw measurement for Z axis converted to SI
385 External Magnetometer HMR2300 Temperature K External HMR2300 Magnetometer temperature
386 IMU 3 Raw Accelerometer X Measurement m/s² IMU 3 raw accelerometer x measurement
387 IMU 3 Raw Accelerometer Y Measurement m/s² IMU 3 raw accelerometer y measurement
388 IMU 3 Raw Accelerometer Z Measurement m/s² IMU 3 raw accelerometer z measurement
389 IMU 3 Raw Gyroscope X Measurement rad/s IMU 3 raw gyroscope x measurement
390 IMU 3 Raw Gyroscope Y Measurement rad/s IMU 3 raw gyroscope y measurement
391 IMU 3 Raw Gyroscope Z Measurement rad/s IMU 3 raw gyroscope z measurement
392 IMU 3 Temperature Measurement K IMU 3 temperature measurement
393 Internal Magnetometer RM3100 Raw Measure X Converted to SI T Internal 2 Magnetometer raw measurement for X axis converted to SI
394 Internal Magnetometer RM3100 Raw Measure Y Converted to SI T Internal 2 Magnetometer raw measurement for Y axis converted to SI
395 Internal Magnetometer RM3100 Raw Measure Z Converted to SI T Internal 2 Magnetometer raw measurement for Z axis converted to SI
400 Power Input V Voltage received by Veronte
401 Power Comicro 3.3V V Voltage received by Veronte through 3.3V port
402 Power 5V V Voltage received by Veronte through 5V port
403 SUC Power Input V Voltage received by Veronte SUC
404 Power 3.6V V Voltage received by Veronte through 3.6V port
405 CPU Temperature K Internal computer temperature
406 External IMU 0 raw accelerometer x measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
407 External IMU 0 raw accelerometer y measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
408 External IMU 0 raw accelerometer z measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
409 External IMU 0 raw gyroscope x measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
410 External IMU 0 raw gyroscope y measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
411 External IMU 0 raw gyroscope z measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
412 External IMU 0 temperature measurement K Saves the temperatures of this external sensor in raw form, as received from custom messages
413 External IMU 1 raw accelerometer x measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
414 External IMU 1 raw accelerometer y measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
415 External IMU 1 raw accelerometer z measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
416 External IMU 1 raw gyroscope x measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
417 External IMU 1 raw gyroscope y measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
418 External IMU 1 raw gyroscope z measurement m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
419 External IMU 1 temperature measurement K Saves the temperatures of this external sensor in raw form, as received from custom messages
420 External magnetometer 0 raw measurement X m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
421 External magnetometer 0 raw measurement Y m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
422 External magnetometer 0 raw measurement Z m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
423 External magnetometer 0 temperature K Saves the temperatures of this external sensor in raw form, as received from custom messages
424 External magnetometer 1 raw measurement X m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
425 External magnetometer 1 raw measurement Y m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
426 External magnetometer 1 raw measurement Z m/s² Saves the measurements of this external sensor in raw form, as received from the custom messages
427 External magnetometer 1 temperature K Saves the temperatures of this external sensor in raw form, as received from custom messages
500 Longitude rad East-West geographic coordinate
501 Latitude rad 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 North Ground Velocity m/s Ground Velocity component in the North direction (NED Coordinates system)
506 East Ground Velocity m/s Ground Velocity component in the East direction (NED Coordinates system)
507 Down Ground Velocity 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 rad Angle between reference body line and flow direction vector
510 Sideslip rad Angle between the flow direction vector and the longitudinal axis of the vehicle
511 GNSS1 MSL m Mean sea level (MSL) measurement provided by GPS 1
512 GNSS1 AGL m Above ground level (AGL level) measurement provided by GPS 1
513 GNSS2 MSL m Mean sea level (MSL) measurement provided by GPS 2
514 GNSS2 AGL m Above ground level (AGL level) measurement provided by GPS 2
📝
551
Sagetech MXS - Longitude decimal part degree Sagetech variable, used by block to parse variables for GPS Navigation Data Message

Warning
Variable for internal use
📝
552
Sagetech MXS - Longitude fractional part degree Sagetech variable, used by block to parse variables for GPS Navigation Data Message

Warning
Variable for internal use
📝
553
Sagetech MXS - Latitude decimal part degree Sagetech variable, used by block to parse variables for GPS Navigation Data Message

Warning
Variable for internal use
📝
554
Sagetech MXS - Latitude fractional part degree Sagetech variable, used by block to parse variables for GPS Navigation Data Message

Warning
Variable for internal use
📝
555
Sagetech MXS - Ground speed m/s Sagetech variable, used by block to parse variables for GPS Navigation Data Message

Warning
Variable for internal use
📝
556
Sagetech MXS - Ground track degree Sagetech variable, used by block to parse variables for GPS Navigation Data Message

Warning
Variable for internal use
📝
560
ADS-B Out / Squawk - ADS-B Squawk code, 4 digits that allow the operator to inform about its status
600-603 Temperature 0-3 K Variables to be configured with external temperature sensors

Warning
Deprecated variables
610 North Position EKF Variance North position Extended Kalman Filter variance
611 East Position EKF Variance East position Extended Kalman Filter variance
612 Down Position EKF Variance Position variance component in the resultant axis from North-East
613 North Velocity EKF Variance m²/s² North velocity Extended Kalman Filter variance
614 East Velocity EKF Variance m²/s² East velocity Extended Kalman Filter variance
615 Down Velocity EKF Variance m²/s² Velocity variance component in the resultant axis from North-East
📝
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 0 customType Correction calculated by the gimbal for the pitch control 0
📝
655
Gimbal Pitch Correction 1 customType Correction calculated by the gimbal for the pitch control 1
📝
656
Gimbal Old Joint 0 customType Auxiliar variable 0 for Gimbal control configuration
📝
657
Gimbal Old Joint 1 customType Auxiliar variable 1 for Gimbal control configuration
📝
658
Cos (Gimbal Yaw) customType Auxiliar variable 0 for Gimbal control configuration
📝
659
Sin (Gimbal Yaw) customType Auxiliar variable 1 for Gimbal control configuration
📝
660
Gimbal Yaw Radian customType Auxiliar variable for Gimbal control configuration
📝
661
Veronte Gimbal Yaw Output customType Yaw value the gimbal is sending as output
📝
662
Veronte Gimbal Pitch Output customType Pitch value the gimbal is sending as output
📝
663
Gimbal Phi(z) customType Auxiliar variable phi for Gimbal control configuration
📝
664
Gimbal Theta(y) customType Auxiliar variable theta for Gimbal control configuration
📝
665
Gimbal Psi(x) customType Auxiliar variable psi for Gimbal control configuration
📝
666
Veronte Gimbal Roll Output (Degrees) customType Roll value the gimbal is sending as output
700-705 RPM 0-5 rad/s Angular speed associated to pulse captured 0-5
750 Selected Controller Time Step s 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 0-15 customType Pulse Width Modulation signal 0 to 15
📝
900-915
Stick Input r0 - r15 customType Raw stick measurement from r0 to r15
📝
950-981
Stick Input s0 - s31 customType
Warning
Deprecated variables
📝
1000-1031
Stick Input y0 - y31 customType Servo position commanded from stick y0 to y31
📝
1050-1069
Control Output u0-u19 Before Servo Saturation customType Commanded control output before saturation correction
1100-1104 Lidar 0-4 Distance m Variable configurable for Lidar distances 0 to 4
📝
1105-1109
External Range Sensor 0-4 Measure m Variable configurable for external range sensors
📝
1200
Route-Guidance Distance m Shortest distance to desired path (perpendicular distance)
📝
1201
Radar AGL (Above Ground Level) - Height m Radar altimeter measure
1202 Radar Speed Down m/s Radar speed
📝
1203
External Rotation for Follow Route rad Relative vector rotation when using Follow Route
1204 Time to Impact with Obstacles s Time calculated with Distance to Obstacle and travel speed
1300-1309 Timer 0-9 s Configurable timers for automations
1320-1321 ADC 3.3V Input 0-1 V CEX ADC 3.3 V inputs 0 and 1
1322-1323 ADC 5.0V Input 0-1 V CEX ADC 5.0 V inputs 0 and 1
1324-1325 ADC 12.0V Input 0-1 V CEX ADC 12.0 V inputs 0 and 1
1326-1327 ADC 36.0V Input 0-1 V CEX ADC 36.0 V inputs 0 and 1
1328-1329 ADC vIn 0-1 V CEX External power supplies 0 and 1
1330 PCB Temperature K CEX PCB Temperature (from ADC input)
1331 ADC HW Version V Hardware version of CEX ADC
📝
1350-1369
4xV Real variables - For more information, check Real Variables - 4x Software Manual
1400 Velocity - X Body Axis m/s Velocity on X-axis
1401 Velocity - Y Body Axis m/s Velocity on Y-axis
1402 Velocity - Z Body Axis m/s Velocity on Z-axis
1403 Estimated Dynamic Pressure Pa Dynamic pressure sensor raw measurement
1404 Barometric Pressure at Sea Level (QNH) Pa Introduced value for QNH
1450-1453 Captured Pulse 0-3 customType Input values from pulses
1484 External IMU 0 accelerometer reception frequency Hz Reception frequencies of measurements from External IMU 0 accelerometer
1485 External IMU 0 gyroscope reception frequency Hz Reception frequencies of measurements from External IMU 0 gyroscope
1486 External IMU 1 accelerometer reception frequency Hz Reception frequencies of measurements from External IMU 1 accelerometer
1487 External IMU 1 gyroscope reception frequency Hz Reception frequencies of measurements from External IMU 1 gyroscope
1488-1489 External magnetometer 0-1 reception frequency Hz Reception frequencies of measurements from External magnetometer 0-1
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 rad 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 rad Raw measurements for internest angle standard deviation
1497 Internest Position Update Frequency Hz Frequency to update internest position
1500 GNSS1 Absolute Time of Week s Data from GNSS1 module: Time of week
1501 GNSS1 ECEF Position X m Data from GNSS1 module: ECEF (Earth-Centered Earth-Fixed coordinate system) X position
1502 GNSS1 ECEF Position Y m Data from GNSS1 module: ECEF (Earth-Centered Earth-Fixed coordinate system) Y position
1503 GNSS1 ECEF Position Z m Data from GNSS1 module: ECEF (Earth-Centered Earth-Fixed coordinate system) Z position
1504 GNSS1 Longitude rad Data from GNSS1 module: Longitude
1505 GNSS1 Latitude rad Data from GNSS1 module: Latitude
1506 GNSS1 Height Above Ellipsoid (WGS84) m Data from GNSS1 module: Height Above Ellipsoid (WGS84)
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 rad Data from GNSS1 module: RTK Base longitude
1518 GNSS1 Related Base Latitude rad 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 rad Data from GNSS1 module: RTK Base-Rover vector azimuth (Spherical coordinates system)
1521 GNSS1 Related Base to Rover Elevation rad 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
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)
1528 GNSS1 Position Frequency Hz Data from GNSS1 module: Position frequency
1529 GNSS1 Jamming Indicator % Jamming indicator from U-Blox device 1 for GNSS
1600 GNSS2 Absolute Time of Week s Data from GNSS2 module: Time of week
1601 GNSS2 ECEF Position X m Data from GNSS2 module: ECEF (Earth-Centered Earth-Fixed coordinate system) X position
1602 GNSS2 ECEF Position Y m Data from GNSS2 module: ECEF (Earth-Centered Earth-Fixed coordinate system) Y position
1603 GNSS2 ECEF Position Z m Data from GNSS2 module: ECEF (Earth-Centered Earth-Fixed coordinate system) Z position
1604 GNSS2 Longitude rad Data from GNSS2 module: Longitude
1605 GNSS2 Latitude rad Data from GNSS2 module: Latitude
1606 GNSS2 Height Above Ellipsoid (WGS84) m Data from GNSS2 module: Height Above Ellipsoid (WGS84)
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 rad Data from GNSS2 module: RTK Base longitude
1618 GNSS2 Related Base Latitude rad 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 rad Data from GNSS2 module: RTK Base-Rover vector azimuth (Spherical Coordinates system)
1621 GNSS2 Related Base to Rover Elevation rad 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
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)
1628 GNSS2 Position Frequency H Data from GNSS2 module: Position frequency
1629 GNSS2 Jamming Indicator % Jamming indicator from U-Blox device 2 for GNSS
📝
1700-1731
Actuator Output s0 - s31 customType Configurable variable from actuator outputs to be transformed by the system
📝
1800
Distance to Object of Interest 0 m Spherical coordinate to object of interest 0: distance
📝
1801
Azimuth to Object of Interest 0 rad Spherical coordinate to object of interest 0: azimuth
📝
1802
Elevation to Object of Interest 0 rad Spherical coordinate to object of interest 0: elevation
📝
1803
Distance to Object of Interest 1 m Spherical coordinate to object of interest 1: distance
📝
1804
Azimuth to Object of Interest 1 rad Spherical coordinate to object of interest 1: azimuth
📝
1805
Elevation to Object of Interest 1 rad Spherical coordinate to object of interest 1: elevation
📝
1806
Distance to Object of Interest 2 m Spherical coordinate to object of interest 2: distance
📝
1807
Azimuth to Object of Interest 2 rad Spherical coordinate to object of interest 2: azimuth
📝
1808
Elevation to Object of Interest 2 rad Spherical coordinate to object of interest 2: elevation
📝
1809
Distance to Object of Interest 3 m Spherical coordinate to object of interest 3: distance
📝
1810
Azimuth to Object of Interest 3 rad Spherical coordinate to object of interest 3: azimuth
📝
1811
Elevation to Object of Interest 3 rad Spherical coordinate to object of interest 3: elevation
📝
1812
Distance to Object of Interest 4 m Spherical coordinate to object of interest 4: distance
📝
1813
Azimuth to Object of Interest 4 rad Spherical coordinate to object of interest 4: azimuth
📝
1814
Elevation to Object of Interest 4 rad Spherical coordinate to object of interest 4: elevation
📝
1815
Distance to Object of Interest 5 m Spherical coordinate to object of interest 5: distance
📝
1816
Azimuth to Object of Interest 5 rad Spherical coordinate to object of interest 5: azimuth
📝
1817
Elevation to Object of Interest 5 rad Spherical coordinate to object of interest 5: elevation
📝
1818
Distance to Object of Interest 6 m Spherical coordinate to object of interest 6: distance
📝
1819
Azimuth to Object of Interest 6 rad Spherical coordinate to object of interest 6: azimuth
📝
1820
Elevation to Object of Interest 6 rad Spherical coordinate to object of interest 6: elevation
📝
1821
Distance to Object of Interest 7 m Spherical coordinate to object of interest 7: distance
📝
1822
Azimuth to Object of Interest 7 rad Spherical coordinate to object of interest 7: azimuth
📝
1823
Elevation to Object of Interest 7 rad Spherical coordinate to object of interest 7: elevation
📝
1824
Distance to Object of Interest 8 m Spherical coordinate to object of interest 8: distance
📝
1825
Azimuth to Object of Interest 8 rad Spherical coordinate to object of interest 8: azimuth
📝
1826
Elevation to Object of Interest 8 rad Spherical coordinate to object of interest 8: elevation
📝
1827
Distance to Object of Interest 9 m Spherical coordinate to object of interest 9: distance
📝
1828
Azimuth to Object of Interest 9 rad Spherical coordinate to object of interest 9: azimuth
📝
1829
Elevation to Object of Interest 9 rad Spherical coordinate to object of interest 9: elevation
📝
1830
Distance to Object of Interest 10 m Spherical coordinate to object of interest 10: distance
📝
1831
Azimuth to Object of Interest 10 rad Spherical coordinate to object of interest 10: azimuth
📝
1832
Elevation to Object of Interest 10 rad Spherical coordinate to object of interest 10: elevation
📝
1833
Distance to Object of Interest 11 m Spherical coordinate to object of interest 11: distance
📝
1834
Azimuth to Object of Interest 11 rad Spherical coordinate to object of interest 11: azimuth
📝
1835
Elevation to Object of Interest 11 rad Spherical coordinate to object of interest 11: elevation
📝
1836
Distance to Object of Interest 12 m Spherical coordinate to object of interest 12: distance
📝
1837
Azimuth to Object of Interest 12 rad Spherical coordinate to object of interest 12: azimuth
📝
1838
Elevation to Object of Interest 12 rad Spherical coordinate to object of interest 12: elevation
📝
1839
Distance to Object of Interest 13 m Spherical coordinate to object of interest 13: distance
📝
1840
Azimuth to Object of Interest 13 rad Spherical coordinate to object of interest 13: azimuth
📝
1841
Elevation to Object of Interest 13 rad Spherical coordinate to object of interest 13: elevation
📝
1842
Distance to Object of Interest 14 m Spherical coordinate to object of interest 14: distance
📝
1843
Azimuth to Object of Interest 14 rad Spherical coordinate to object of interest 14: azimuth
📝
1844
Elevation to Object of Interest 14 rad Spherical coordinate to object of interest 14: elevation
📝
1845
Distance to Object of Interest 15 m Spherical coordinate to object of interest 15: distance
📝
1846
Azimuth to Object of Interest 15 rad Spherical coordinate to object of interest 15: azimuth
📝
1847
Elevation to Object of Interest 15 rad Spherical coordinate to object of interest 15: elevation
📝
1848
Distance to Object of Interest 16 m Spherical coordinate to object of interest 16: distance
📝
1849
Azimuth to Object of Interest 16 rad Spherical coordinate to object of interest 16: azimuth
📝
1850
Elevation to Object of Interest 16 rad Spherical coordinate to object of interest 16: elevation
📝
1851
Distance to Object of Interest 17 m Spherical coordinate to object of interest 17: distance
📝
1852
Azimuth to Object of Interest 17 rad Spherical coordinate to object of interest 17: azimuth
📝
1853
Elevation to Object of Interest 17 rad Spherical coordinate to object of interest 17: elevation
📝
1854
Distance to Object of Interest 18 m Spherical coordinate to object of interest 18: distance
📝
1855
Azimuth to Object of Interest 18 rad Spherical coordinate to object of interest 18: azimuth
📝
1856
Elevation to Object of Interest 18 rad Spherical coordinate to object of interest 18: elevation
📝
1857
Distance to Object of Interest 19 m Spherical coordinate to object of interest 19: distance
📝
1858
Azimuth to Object of Interest 19 rad Spherical coordinate to object of interest 19: azimuth
📝
1859
Elevation to Object of Interest 19 rad Spherical coordinate to object of interest 19: elevation
📝
1860
Distance to Object of Interest 20 m Spherical coordinate to object of interest 20: distance
📝
1861
Azimuth to Object of Interest 20 rad Spherical coordinate to object of interest 20: azimuth
📝
1862
Elevation to Object of Interest 20 rad Spherical coordinate to object of interest 20: elevation
📝
1863
Distance to Object of Interest 21 m Spherical coordinate to object of interest 21: distance
📝
1864
Azimuth to Object of Interest 21 rad Spherical coordinate to object of interest 21: azimuth
📝
1865
Elevation to Object of Interest 21 rad Spherical coordinate to object of interest 21: elevation
📝
1866
Distance to Object of Interest 22 m Spherical coordinate to object of interest 22: distance
📝
1867
Azimuth to Object of Interest 22 rad Spherical coordinate to object of interest 22: azimuth
📝
1868
Elevation to Object of Interest 22 rad Spherical coordinate to object of interest 22: elevation
📝
1869
Distance to Object of Interest 23 m Spherical coordinate to object of interest 23: distance
📝
1870
Azimuth to Object of Interest 23 rad Spherical coordinate to object of interest 23: azimuth
📝
1871
Elevation to Object of Interest 23 rad Spherical coordinate to object of interest 23: elevation
📝
1872
Distance to Object of Interest 24 m Spherical coordinate to object of interest 24: distance
📝
1873
Azimuth to Object of Interest 24 rad Spherical coordinate to object of interest 24: azimuth
📝
1874
Elevation to Object of Interest 24 rad Spherical coordinate to object of interest 24: elevation
📝
1875
Distance to Object of Interest 25 m Spherical coordinate to object of interest 25: distance
📝
1876
Azimuth to Object of Interest 25 rad Spherical coordinate to object of interest 25: azimuth
📝
1877
Elevation to Object of Interest 25 rad Spherical coordinate to object of interest 25: elevation
📝
1878
Distance to Object of Interest 26 m Spherical coordinate to object of interest 26: distance
📝
1879
Azimuth to Object of Interest 26 rad Spherical coordinate to object of interest 26: azimuth
📝
1880
Elevation to Object of Interest 26 rad Spherical coordinate to object of interest 26: elevation
📝
1881
Distance to Object of Interest 27 m Spherical coordinate to object of interest 27: distance
📝
1882
Azimuth to Object of Interest 27 rad Spherical coordinate to object of interest 27: azimuth
📝
1883
Elevation to Object of Interest 27 rad Spherical coordinate to object of interest 27: elevation
📝
1884
Distance to Object of Interest 28 m Spherical coordinate to object of interest 28: distance
📝
1885
Azimuth to Object of Interest 28 rad Spherical coordinate to object of interest 28: azimuth
📝
1886
Elevation to Object of Interest 28 rad Spherical coordinate to object of interest 28: elevation
📝
1887
Distance to Object of Interest 29 m Spherical coordinate to object of interest 29: distance
📝
1888
Azimuth to Object of Interest 29 rad Spherical coordinate to object of interest 29: azimuth
📝
1889
Elevation to Object of Interest 29 rad Spherical coordinate to object of interest 29: elevation
📝
1890
Distance to Object of Interest 30 m Spherical coordinate to object of interest 30: distance
📝
1891
Azimuth to Object of Interest 30 rad Spherical coordinate to object of interest 30: azimuth
📝
1892
Elevation to Object of Interest 30 rad Spherical coordinate to object of interest 30: elevation
📝
1893
Distance to Object of Interest 31 m Spherical coordinate to object of interest 31: distance
📝
1894
Azimuth to Object of Interest 31 rad Spherical coordinate to object of interest 31: azimuth
📝
1895
Elevation to Object of Interest 31 rad Spherical coordinate to object of interest 31: elevation
2000 RX Packet Error Rate (on board) decimal Value rating RX packets and expected RX packets, given as % error
2001 TX Packet Error Rate (on board) decimal Value rating 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 RX packages per second received and computed 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 TX packages per second received and computed through communications
📝
2019
Stick RX Rate Hz Number of stick messages received per second
2020 Position Fix Time s Time spend with GNSS without losing fix
2040-2042 Tunnel Producer Receive Frequency 0-2 Hz Tunnel producer 0-2 receives data at this frequency
2043-2045 Tunnel Consumer Send Frequency 0-2 Hz Tunnel consumer 0-2 receives data at this frequency
2046 Max Duration of Step in CIO s Longest time duration from a step in CIO
2047 Acquisition Task Timestep s Average period to execute the acquisition thread
2048 Acquisition Task Maximum Timestep s Maximum period to execute the acquisition thread
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 CPU time spent in the acquisition thread
2051 Acquisition Task Maximum CPU Ratio percentage Maximum % of CPU time spent in the acquisition thread
2052 Acquisition Task Average Time s Average time for acquisition thread
2053 Acquisition Task Maximum Time s Maximum time for acquisition thread
2054 CIO Max Time s Maximum time of CIO thread
2055 CIO Average Time s Average and Maximum time of CIO thread
2056 Cross-Core Message Queue Usage % Percentage of communication employed between both microprocessors
2057 CIO Running Frequency Hz C1 low running frequency (Veronte Autopilot 1x and MC)

Note
Only for MC
2058 CIO Min Running Frequency Hz Minimum assured frequency of low priority task

Note
Only for MC
2094 GNC Task Average CPU Ratio percentage Average % of CPU time of GNC task
2095 GNC Task Maximum CPU Ratio percentage Maximum % of CPU time of GNC task
2096 GNC Task Average Time s Average time spent on GNC task
2097 GNC Task Maximum Time s Maximum time spent on GNC task
2098 GNC Task Maximum Timestep s Maximum execution period for GNC task
2099 Max Duration of Step in GNC s Maximum duration of one step in GNC
2100 Gyroscope Based on Accelerometer - X Body Axis rad/s Gyroscope measurements obtained from accelerometer X-axis data
2101 Gyroscope Based on Accelerometer - Y Body Axis rad/s Gyroscope measurements obtained from accelerometer Y-axis data
2102 Gyroscope Based on Accelerometer - Z Body Axis rad/s 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 length covered
2201 Curve Length m Total distance from current mission length
2202 Curve Length Pending m Total distance from current mission length not covered yet
2203 Curve Parameter Covered customType Total length covered from current mission according to parameter selected
2204 Curve Parameter Range customType Total length from current mission according to parameter selected
2205 Curve Parameter Pending customType Total length from current mission to be covered according to parameter selected yet
2206 Curve Horizontal Curvature customType Horizontal curvature of the current curve
2250-2259 Reserved 0-9 customType System reserved variables
📝2300-2302 Joint 0-2 of Gimbal 0 rad Variables for Gimbal 0 configuration - Angles sent to gimbal as Yaw (0), Pitch (1) and Roll (2)
📝2303-2305 Joint 0-2 of Gimbal 1 rad Variables for Gimbal 1 configuration - Angles sent to gimbal as Yaw (0), Pitch (1) and Roll (2)
📝2330 Control Loop Period s MC control loop period
📝2331 Control Loop Maximum Period s MC maximum control loop period
📝2332 Control Loop Duration s MC control loop average execution time
📝2333 MC Control Loop Maximum Duration s MC control loop maximum average execution time
📝2334 Control Loop CPU Usage Ratio % MC CPU usage ratio
📝2335 MC Control Loop Maximum CPU Usage Ratio % MC maximum CPU usage ratio
📝2336-2338 MC U-V-W Phase Current A MC U-V-W phase current
📝2339 MC Electrical Angle rad MC electrical angle
📝2340 MC01 Mechanical Angle rad MC01 mechanical angle
📝2341 MC Mechanical Angular Speed rad/s MC mechanical angular speed
📝2342 MC01 Desired Mechanical Angle rad MC01 desired mechanical angle
📝2343 MC01 Position Controller Output rad/s MC01 position PDI output
📝2344 MC Desired Mechanical Angular Speed rad/s MC desired mechanical angular speed
📝2345 MC Desired Mechanical Angular Speed After Speed Limiter rad/s MC desired mechanical angular speed after speed limiter
📝2346 MC Speed Controller Output A MC speed controller output
📝2347-2348 MC Alpha-Beta Current A MC alpha and beta current after Clarke transformation
📝2349-2350 MC Actual Direct Current A MC actual direct current
📝2351 MC Desired Direct Current A MC desired direct current
📝2352 MC Desired Quadrature Current A MC desired quadrature current
📝2353 MC Direct Voltage From Controller Output V MC direct voltage from controller output
📝2354 MC Quadrature Voltage From Controller Output V MC quadrature voltage from controller output
📝2355-2356 MC Alpha - Beta Voltage From Current Controller Output V MC Alpha - Beta voltage from current controller output
📝2357-2358 MC01 Desired Clarke Alpha-Beta current customType MC01 desired Clarke currents
📝
2359-2361
MC01 U-V-W Phase Space Vector Generator Output customType MC01 phase time constants
📝2362-2364 MC01 U-V-W Phase PWM Duty Cycle percentage MC01 U-V-W Phase PWM duty cycle
📝2365 MC01 Encoder Raw Angle rad MC01 encoder raw measured angle
📝2366 MC01 Stepper Output Frequency Hz MC01 stepper output frequency
📝2367 MC Mechanical Angle Error rad MC mechanical angle error
📝2368-2370 MC U-V-W Phase BEMF V MC U-V-W phase electromechanical force
📝2371 MC Input Current DC side A MC input current DC side
📝2372 MC Input Normalized Command Speed customType MC input normalized command speed
📝
2373-2374
MC ADC in 0-1 V System reserved variables
📝2375 MC Logic Board Temperature K MC logic board temperature
📝2376 MC Power Module Temperature K MC IGBT filtered temperature
📝2377 MC Motor Temperature K MC Motor temperature
📝2378 MC Input Voltage DC side V MC DC bus voltage
📝2379-2380 MC U-V Phase Hall current sensor customType System reserved variables
2381 MC Virtual and estimator angle difference rad MC Angle offset value from estimated and commanded angle to close control loop
2382 MC Low speed estimator angle rad MC Low speed observer estimated angle
2383 MC High speed estimator angle rad MC High speed observer estimated angle
2384 MC Low speed estimator speed rad/s MC Low speed observer estimated mechanical speed
2385 MC High speed estimator speed rad/s MC High speed observer estimated mechanical speed
📝2400-2419 Control Output u0-19 customType Control output 0 to 19 after servo saturation
📝2500-2519 Stick Input u0-u19 customType Intermediate values from stick used for arcade mode
📝2600-2619 Stick Input d0-d19 customType Intermediate values from stick used for arcade mode - delta values
2700-2739 Operation Guidance 00-39 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
2812 Wind Azimuth Angle degree Wind estimated azimuth
2813 Wind Velocity in North-East plane m/s Horizontal wind velocity
2813 Wind Velocity in North-East plane m/s Horizontal wind velocity
2830-2893 Setup real 00-63 customType Setup variable 00-63
📝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 s Time-lapse considered since entering the current phase
2903 GNC Timestep s Task execution period from GNC
2904 Total Flight Time s Time-lapse since the vehicle finished Standby

Warning
Deprecated variable
2905 Total Flight Distance m Distance covered by the vehicle in all mission length

Warning
Deprecated variable
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 in Phase 0-19 s Time-lapse spent by the vehicle in phase 0 to 19
📝
3000-3031
Simulation Variable 0-31 customType Variables used for Simulation data
📝
3100-3399
User Variable 00-299 (Real - 32 Bits) customType Free variables for the user to use
4100 Zero customType Constant value 0
4101 Rvar Disabled customType Disabled variable

Integer Variables (UVar) - 16 Bits

ID Name Description
0 Actuator Mode Index pointing to the flight mode in use
1 Phase Identifier Index pointing to the active phase
2 Internal ADC 0 Internal ADC pin

Warning
Variable for internal use
3-7 ADC 0-4 Direct reading of ADC pins
8-18 Internal ADC 1-11 Internal ADC pin

Warning
Variable for internal use
📝
19
Current envelope (deprecated) Index pointing to the used envelope

Warning
Deprecated variable
20 Counter for C2 system C2 counter to monitor if Core 2 is alive
21 Total memory for blocks allocation (low part) Total words available for blocks (low part).
It is stored in two parts because the size can be a number up to 32 bits, but the uvars are stored in variables of 16, so to get the true size the user would have to put together both the low and the high part.

Note
1 word = 2 bytes
22 Total memory for blocks allocation (high part) Total words available for blocks (high part).
It is stored in two parts because the size can be a number up to 32 bits, but the uvars are stored in variables of 16, so to get the true size the user would have to put together both the low and the high part.

Note
1 word = 2 bytes
23 Memory used for blocks allocation (low part) Words used for blocks in allocator (low part).
It is stored in two parts because the size can be a number up to 32 bits, but the uvars are stored in variables of 16, so to get the true size the user would have to put together both the low and the high part.

Note
1 word = 2 bytes
24 Memory used for blocks allocation (high part) Words used for blocks in allocator (high part).
It is stored in two parts because the size can be a number up to 32 bits, but the uvars are stored in variables of 16, so to get the true size the user would have to put together both the low and the high part.

Note
1 word = 2 bytes
25 SRTM source at UAV's position Index for the SRTM source type:

  • 0: Processing
  • 1: Invalid
  • 2: 90-meter resolution in equator
  • 3: 30-meter resolution in equator
50 PDI error source Index for PDI error source identification.
For further information, consult the List of PDI errors
51 Operation error source Index for operation error source identification
53 4XV Veronte ID ID of this AP in a redundant (0-3) to compare with the selected CAP.
For more information, check Integer Variables - 4x Software Manual
54 4XV Veronte CAP Current Autopilot 1x selected.
For more information, check Integer Variables - 4x Software Manual
📝
55-75
4xV Integer variables For more information, check Integer Variables - 4x Software Manual
80 Detour calculation identifier Counter of number of times a route change has been calculated
81 Approach calculation identifier Counter of number of times Approach guidance has been calculated
82 Climb calculation identifier Counter of number of times Climb guidance has been calculated
83 Cruise calculation identifier Counter of number of times Cruise guidance has been calculated
84 Rendezvous calculation identifier Counter of number of times Rendezvous guidance has been calculated
85 Taxi calculation identifier Counter of number of times Taxi guidance has been calculated
86 VTOL calculation identifier Counter of number of times VTOL guidance has been calculated
90 Version Major Major software version
91 Version Minor Minor software version
92 Version Revision Revision software version
95 UAV address UAV address
96 File system status State error for DFS2 FS
For further information, consult the List of File system errors
97 Number of registered partitions on DFS2 File System Number of registered partitions on DFS2 File System
100 GNSS1 Number of Satellites Used in Solution Number of satellites used in solution
101-102 GNSS1 rejected-accepted RTCM 1005 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1005
103-104 GNSS1 rejected-accepted RTCM 1077 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1077
105-106 GNSS1 rejected-accepted RTCM 1087 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1087
107-108 GNSS1 rejected-accepted RTCM 1127 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1127
109-110 GNSS1 rejected-accepted RTCM 1230 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1230
111-112 GNSS1 rejected-accepted RTCM 4072 Number of RTCM rejected by wrong CRC - correctly received by Ublox 4072
113 GNSS1 rejected RTCM unknown type Number of RTCM unknown rejected by wrong CRC
114 GNSS1 week GNSS1 week
115 GNSS1 Jamming Status Output from GPS 1 jamming/interference monitor:

  • 0 = unknown or feature disabled
  • 1 = ok ⇒ no significant jamming
  • 2 = warning ⇒ interference visible but fix Ok
  • 3 = critical ⇒ interference visible and no fix
150 GNSS2 Number of Satellites Used in Solution Number of Satellites Used in Solution
151-152 GNSS2 rejected-accepted RTCM 1005 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1005
153-154 GNSS2 rejected-accepted RTCM 1077 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1077
155-156 GNSS2 rejected-accepted RTCM 1087 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1087
157-158 GNSS2 rejected-accepted RTCM 1127 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1127
159-160 GNSS2 rejected-accepted RTCM 1230 Number of RTCM rejected by wrong CRC - correctly received by Ublox 1230
161-162 GNSS2 rejected-accepted RTCM 4072 Number of RTCM rejected by wrong CRC - correctly received by Ublox 4072
163 GNSS2 rejected RTCM unknown type Number of RTCM unknown rejected by wrong CRC
164 GNSS2 week GNSS2 week
165 GNSS2 Jamming Status Output from GPS 2 jamming/interference monitor:

  • 0 = unknown or feature disabled
  • 1 = ok ⇒ no significant jamming
  • 2 = warning ⇒ interference visible but fix Ok
  • 3 = critical ⇒ interference visible and no fix
200 Radar Altimeter State Index for the radar altimeter state
201 Current Section ID of current patch being executed by the autopilot
202 Last Achieved Section ID of last patch completed by the autopilot
203 Track Stage Index of type of tracked route:

  • 0: No route
  • 1: Route from mission
  • 2: Commanded route
204 Current patchset ID Index showing the patchset:

  • 0: Approach
  • 1: Climb
  • 2: Route
  • 3: Taxi
  • 4: VTOL
  • 5: Rendezvous
  • 6: Detour
205 Amount of laps done Number of laps completed on the route
310-311 Iridium sent-received Number of packets successfully sent/received
398 VectorNav Mode Index showing external source VectorNav mode
399 Identifier of max duration step in acquisition Identifier of maximum duration step in CIO

Warning
Variable for internal use
400 Internest raw status Internest raw status
401 Navigation source Index pointing to the primary navigation source:

  • 1: Internal navigation
  • 2: Simulated navigation (IRX source)
  • 3: External navigation using VCP
  • 4: External navigation using dedicated variables
  • 5: External navigation from Vectornav VN-300
402 Raw position source identifier GPS identifier selected as main
📝
403
(Deprecated) Selected static pressure sensor Static pressure sensor selection

Warning
Deprecated variable
404 Selected dynamic pressure sensor Dynamic pressure sensor selection
405 Selected primary accelerometer (deprecated) Primary accelerometer selection

Warning
Deprecated variable
406 Selected primary gyroscope (deprecated) Primary gyroscope selection

Warning
Deprecated variable
📝
409
(Deprecated) Selected magnetometer Magnetometer selection

Warning
Deprecated variable
410 Selected stick priority table Stick priority table selection
425 Identifier of max duration step in GNC Step with maximum duration
426 Group of user bits selected for CBIT Index pointing to the selected list of safety bits.
This is the group of user bits selected to be computed with system CBIT.
449 Configured system errors that had triggered Bitarray containing the errors that can trigger the System Error.
450 CAN-A Tx errors CAN A communication errors in transmission
451 CAN-A Rx errors CAN A communication errors in reception
452 CAN-B Tx errors CAN B communication errors in transmission
453 CAN-B Rx errors CAN B communication errors in reception
454-459 CAN to Serial 0-5 frames dropped Lost messages during CAN to Serial transformations
460-461 First-Last file Periodic log First-Last file of the periodic log
462-463 First-Last file Event log First-Last file of the event log
464-465 First-Last file Fast log First-Last file of the fast log
480-485 COM0-5 packet discarded Discarded packets at COM 0 to 5
490 Number of moving obstacles detected Number of moving obstacles detected
491-492 Veronte static cfg CRC(no Operation) of files (Higher-Lower 16 bits) Veronte static cfg CRC (no Op.) of files
493-494 Veronte static cfg CRC(no Operation) of memory (Higher-Lower 16 bits) Veronte static cfg CRC (no Op.) of memory
495-496 Global configuration state (crc) of files-memory (Higher-Lower 16 bits) Global configuration state (crc) of files and memory
497 Config manager status (flash / sd / maintenance mode) Configuration manager status
498-499 Global configuration state (crc) of files-memory Global configuration state (crc) of files and memory
📝
550-557
Reserved 0-7 System reserved variables for Gimbal
600-615 PPM channel 0-15 output CEX PPM channel outputs
620 Jetibox max successfully parsed message
Note
CEX variable
710 ADS-B OUT - Squawk Code ADS-B Squawk code, 4 digits that allow the operator to inform about its status.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Deprecated variable
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
711 ADS-B OUT - ICAO ADS-B ICAO, 4 ASCII characters assigned by aircraft authority as an identifier.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Deprecated variable
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
712 ADS-B OUT - Ident Index indicating whether the identification is enabled or disabled.
This is the identification of the UAV at the request of ATC.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Deprecated variable
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
713 ADS-B OUT - Mode Index of ADS-B mode: IN, OUT or BOTH.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Deprecated variable
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
714-721 ADS-B OUT - Call sign 0-7 ADS-B Call sign, 9 ASCII characters used by the operator to be identified during communication.
These variables are closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Deprecated variables
  • If the user modifies these variables, it is not guaranteed that the transponder will continue to function correctly
730 (Deprecated) Ping1090 - Sequence number
Warning
Deprecated variable
741 (Deprecated) Sagetech MXS - Hemisphere data status Sagetech variable, used by block to parse variables for GPS Navigation Data Message.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
742 (Deprecated) Sagetech MXS - Ground track Sagetech variable, used by block to parse variables for GPS Navigation Data Message.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
743 (Deprecated) Sagetech MXS - Air speed Sagetech variable, used by block to parse variables for GPS Navigation Data Message.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
750 ADS-B Out / ICAO High ADS-B ICAO, 4 ASCII characters assigned by aircraft authority as an identifier.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
751 ADS-B Out / ICAO Low ADS-B ICAO, 4 ASCII characters assigned by aircraft authority as an identifier.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
752 ADS-B Out / Emitter Type Type/category of ADS-B emitter.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
753-760 ADS-B Out / Call Sign 0-7 ADS-B Call sign, 9 ASCII characters used by operator to be identified during communication.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variabled for internal use (custom message for transponder)
  • If the user modifies these variables, it is not guaranteed that the transponder will continue to function correctly
761 ADS-B Out / Type Model of ADS-B transponder.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
762 ADS-B Out / Control Index of ADS-B control: OFF, ADS-B IN, ADS-B OUT or BOTH (ADS-B IN and OUT).
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
763 ADS-B Out / Squawk ADS-B Squawk code, 4 digits that allow the operator to inform about its status.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
764 ADS-B Out / Ident Index indicating whether the identification is enabled or disabled.
This is the identification of the UAV at the request of ATC.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
765 ADS-B Out / Custom Variable for internal use for ADS-B Out.
This variable is closely related to the management of communications between transponders and Veronte Autopilot 1x.

Warning
  • Variable for internal use (custom message for transponder)
  • If the user modifies this variable, it is not guaranteed that the transponder will continue to function correctly
800 MC Fault Id Index of the MC error

Warning
Deprecated variable
801 MC Input Control Mode Index of the MC control input mode:

  • 1: PPM
  • 2: CAN
  • 3: both modes active (CAN priority)
802 MC Actual Control Machine State State of motor controller:

  • 0: Motor stop and driver disabled
  • 1: Calibration of ADC reading
  • 2: Initial alignment procedure
  • 3: Open loop procedure
  • 4: Speed mode
📝
900-909
Simulation variable 00-09 Variables used for simulation data
📝
1000-1299
User Variable 00-299 (Unsigned Integer - 16 bits) Free variables for user
2000 Uvar Disabled Disabled variable
2001 Zero Variable with constant 0 value

Features Variables - 64 Bits

Landing route - Features variables
ID Name Form Units Description
0 Approach Initial Point [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 0 in Landing capture.
1 Approach Loiter Start [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 1 in Landing capture.
2 Approach Loiter Center [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 2 in Landing capture.
3 Approach Loiter Finish [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 3 in Landing capture.
4 Approach Headturn Start [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 4 in Landing capture.
5 Approach Headturn Center [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 5 in Landing capture.
6 Approach Headturn Finish [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 6 in Landing capture.
7 Approach Touch Point [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 7 in Landing capture.
8 Approach Runway End [lon, lat, height] [rad, rad, m] Landing Guidance Variable. Point 8 in Landing capture.


Note

For further information regarding Landing guidance, please refer to Landing - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.

Climbing route - Features variables
ID Name Form Units Description
1025 Climb First Loiter Point [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1025 in Climbing capture.
1026 Climb Loiter Center [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1026 in Climbing capture.
1027 Climb Start Loiter [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1027 in Climbing capture.
1028 Climb Finish Headturn [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1028 in Climbing capture.
1029 Climb Headturn Center [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1029 in Climbing capture.
1030 Climb Start Headturn [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1030 in Climbing capture.
1031 Climb Initial Point [lon, lat, height] [rad, rad, m] Climbing Guidance Variable. Point 1031 in Climbing capture.


Note

For further information regarding Climbing guidance, please refer to Climb - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.

Taxi route - Features variables
ID Name Form Units Description
2048 Taxi Initial Point [lon, lat, height] [rad, rad, m] Taxi Guidance Variable. Point 2048 in Taxi capture.
2049 Taxi Runway First Point [lon, lat, height] [rad, rad, m] Taxi Guidance Variable. Point 2049 in Taxi capture.
2050 Taxi Runway Final Point [lon, lat, height] [rad, rad, m] Taxi Guidance Variable. Point 2050 in Taxi capture.


Note

For further information regarding Taxi guidance, please refer to Taxi - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.

VTOL route - Features variables
ID Name Form Units Description
4096 Vtol 00 [lon, lat, height] [rad, rad, m] VTOL Initial point. Point 4096 in VTOL route capture.
4097 Vtol 01 [lon, lat, height] [rad, rad, m] VTOL Translate Start. Point 4097 in VTOL route capture.
4098 Vtol 02 [lon, lat, height] [rad, rad, m] VTOL Translate End. Point 4098 in VTOL route capture.
4099 Vtol 03 [lon, lat, height] [rad, rad, m] VTOL End point. Point 4099 in VTOL route capture.


Note

For further information regarding VTOL guidance, please refer to VTOL - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.


ID Name Form Units Description
3072 - 3075Smooth 00 - 03[lon, lat, height][rad, rad, m]Smooth Feature Variable.
5120 - 5124Detour 00 - 04[lon, lat, height][rad, rad, m]Detour Feature Variables.
6144Runway Loiter[lon, lat, height][rad, rad, m]Runway Guidance Variable.
6145Runway Touch Point[lon, lat, height][rad, rad, m]Runway Guidance Variable.
6146Runway End Position[lon, lat, height][rad, rad, m]Runway Guidance Variable.
7168 - 7169Gimbal Pointing 00 - 01[lon, lat, height][rad, rad, m]Gimbal Pointing.
8192UAV position[lon, lat, height][rad, rad, m]UAV position.
8193Current phase[lon, lat, height][rad, rad, m]Current phase.
8194Desired position[lon, lat, height][rad, rad, m]Desired position.
8195Invalid ID attempted[lon, lat, height][rad, rad, m]Auxiliar feature - Not valid for users.
8196Track position[lon, lat, height][rad, rad, m]Closer point in route to the current desired position.
8197Operator position[lon, lat, height][rad, rad, m]Operator position.
8198Start waypoint in current route[lon, lat, height][rad, rad, m]Start waypoint in current route.
8199End waypoint in current route[lon, lat, height][rad, rad, m]End waypoint in current route.
9216 - 9235Phase 00 - 19[lon, lat, height][rad, rad, m]Phase.
10240 - 10247Inflight Reference 00 - 07[lon, lat, height][rad, rad, m]Absolute or relative reference position useful during mission.
11264 - 11327Obstacle Sensor 00 - 63[lon, lat, height][rad, rad, m]Obstacle Sensor.
12288 Rendezvous 00 [lon, lat, height] [rad, rad, m] Start point.
For further information, please refer to Rendezvous - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.
12289 Rendezvous 01 [lon, lat, height] [rad, rad, m] Rendezvous relative point.
For further information, please refer to Rendezvous - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.
12290 Rendezvous 02 [lon, lat, height] [rad, rad, m] Docking relative point.
For further information, please refer to Rendezvous - Guidance blocks of Block Programs section of the 1x PDI Builder user manual.
13312 - 13327Moving Obstacles 00 - 15[lon, lat, height][rad, rad, m]Moving Obstacle.
14336 - 14353 Fixed runway features 00 - 17 [lon, lat, height] [rad, rad, m] 1x PDI Builder allows the configuration of up to 6 runways.

Each runway has 3 main points, Initial point, End point, and Loiter Center, which are repeated every three IDs.

E.g. Initial point for Runway 0 is 14336, for Runway 1 is 14339, for Runway 2 is 14342, etc.
15360 - 15371 Fixed spot features 00 - 11 [lon, lat, height] [rad, rad, m] 1x PDI Builder allows the configuration of up to 6 spots.

Each spot has 2 main points, Spot coordinates and Loiter Center, which are repeated every two IDs.

E.g. Spot coordinates for Spot 0 is 15360, for Spot 1 is 15362, for Spot 2 is 15364, etc.
28672 - 28703Moving Objects 00 - 31[lon, lat, height][rad, rad, m]Moving Objects.

The following variables of the Autopilot 1x take part in the navigation performance.

List of PDI Errors

The following table explains the list of possible errors from Veronte applications.

Note

The decimal value of the PDI Error Source (UVar 50) represents the PDI error ID listed in the following table.

Code Explanation
pdi_ok0No errors detected
pdi_gpio1GPIOs function configuration
pdi_odt_pool_sz2Incorrect pool size in on-demand telemetry
pdi_telemetry_alloc3Could not allocate new telemetry vector
pdi_channelmgr10Channel manager configuration
pdi_sara15SARA sim type oor
pdi_vblk_sensrtm16Block for SRTM sensor
pdi_arcx23Arcade axis set of options
pdi_msg8_consumer_hi24Custom message consumer cannot be used in HI unless it is an external sensor
pdi_modes27Stick configuration modes
pdi_blkekfstp41Static pressure to EKF adapter block
pdi_gnss_blocks45GNSS constellations configuration (more than allowed)
pdi_cansuite_gpio47CAN suite gpio
pdi_vrng48Range sensors
pdi_fmset50Custom message set
pdi_pwm54PWM configuration
pdi_sniffer63Sniffer wires configuration
pdi_sniffer_read_only64Read-only variable selected in sniffer
pdi_fmsgc_read_only65Read-only variable selected in serial message consumer
pdi_canmsgc_read_only66Read-only variable selected in CAN message consumer
pdi_vref_read_only67Read-only vref variable
pdi_obstacle68Incorrect type of obstacle
pdi_obsense69Obstacle sensing mode or type oor
pdi_marks71Incorrect type of mark
pdi_fmsg_p74Custom message producers msg id oor
pdi_fmsg_c75Custom message consumers process parser oor
pdi_fmsgcan_c76CAN custom msg consumer msg id oor
pdi_telem77Telemetry configuration
pdi_sci81SCI config error
pdi_events82Invalid event
pdi_actions83Actmgr - List of actions
pdi_evact84Actmgr - List of related events and actions
pdi_cmd_not_allowed85Commands not allowed
pdi_wrapper86Wrapper range configuration incorrect
pdi_xpc_can_in87XPC for CAN messages input filters size ok
pdi_xpc_can_out88XPC for CAN messages output filters size ok
pdi_xpc_can_ser89XPC for CAN messages serialtocan size ok
pdi_xpc_can_gpio90XPC for CAN messages virtual gpios size ok
pdi_xpc_can_map91XPC for CAN messages and check their priority and connections
pdi_xpc_u8_map92XPC for u8 messages and check their priority and connections
pdi_internest93Internest version in range
pdi_internest194Internest max_range_vbase in range
pdi_internest295Internest max_range_vexplore in range
pdi_ecap101Capture
pdi_cappulse116ECAP pulse consumers
pdi_i2cdevs117I2C external devices
pdi_lossy_resize120Lossy resize error
pdi_rvector_resize121Rvector resize error
pdi_asciiparser122ASCII parser invalid configuration
pdi_telemetry_exceeded123Telemetry size exceeded
pdi_hi_3210_rx_tout154HI-3210 rx cannot be configured
pdi_hi_3210_tx_tout155HI-3210 tx cannot be configured
pdi_cmd_rdvzset176Rendezvous command base_yaw oor
pdi_cmd_taxiget183Taxi guidance block error. Could be invalid runway or invalid initial point
pdi_cmd_gtrack1188Invalid detour command
pdi_cmd_gtrack2189Invalid guidance block configuration
pdi_cmd_speed192Cruise speed command
pdi_cmd_gtrack193Invalid detour command
pdi_cmd_gtrkset194Track request command
pdi_cmd_stksrcr208Get stick raw channels from selected source
pdi_cmd_vtolset212VTOL request command
pdi_ini_nok213Cannot change to a phase different from INI with System BIT not OK and out of PDI mode
pdi_cmd_nav215Navigation command
pdi_cmd_gpio218GPIO command
pdi_cmd_phase222Commanded phase is out of range
pdi_cmd_gimbal225Gimbal commands
pdi_cmd_var235Variable set command
pdi_reset239Reset CPU IRX
pdi_acc2filt257 Bosch IMU BMI088 (IMU2) Accelerometer filter
pdi_imu3_filter258 ADIS16505 IMU filter not in range [0,6]
pdi_imu3_filter_bw259 ADIS16505 IMU filter not compatible with Bandwidth limit
pdi_cansuite_in288 CAN suite producer for Veronte
pdi_cansuite_out289 CAN suite consumer for Veronte
pdi_cfg_can290 CAN cfg
pdi_resize_can_cex291 CEX CAN cfg
pdi_resize_can_commex292 COMMEX CAN cfg
pdi_jeti_and_lift293 Trying to configure jeti and lift (not enough memory)
pdi_srtm_calib500 Tried to calibrate SRTM without valid SRTM data for current point
pdi_jid501 Invalid feature
pdi_canid502 Invalid CAN id
pdi_cfgid_mode0503 Invalid Cfgid PDI (number of PDIs does not match)
pdi_cfgid_mode1504 Invalid Cfgid PDI mode
pdi_cmd_mgr505 Expected command size does not match
pdi_cmd_mgr1506 Expected command size does not match
pdi_cancfg507 Invalid CAN configuration
pdi_decimator508 Invalid decimator
pdi_sci_cfg509 Invalid SCI configuration
pdi_field1510 Maximum ID of real variable exceeded
pdi_field2511 Maximum ID of user variable exceeded
pdi_field3512 Maximum ID of bit variable exceeded
pdi_field4513 Maximum number of decimals for real variable exceeded
pdi_field5514 Overflow for real variable detected
pdi_field6515 Incorrect CRC field
pdi_field7516 Field matcher number of bits outside range
pdi_field8517 Field maximum skippable bits exceeded
pdi_field9518 Maximum ID of real variable saved as string exceeded
pdi_field10519 Field type out of range
pdi_flogic520 Invalid event composition (Flogic)
pdi_flogic1521 Invalid event composition (Flogic)
pdi_flogic2522 Invalid event composition type
pdi_fref523 Invalid type of position reference
pdi_irxtable524 Invalid 3Dtable mode or vector is non-decreasing
pdi_limit525 Invalid limit event type
pdi_lsm6ds3_cfg526 Accelerometer/Gyroscope settings outside range
pdi_pdi_ver527 Incompatible PDI version, try migrating offline and uploading a complete migrated configuration
pdi_rvarsensor528 Id for Rvar out of range for Rvarsensor
pdi_stickrawtrans0529 K value in stick outside range [-100, 100] or 0
pdi_stickrawtrans1530 Maximum value read from stick for Configured range exceeded [4095]
pdi_stickrawtrans2531 Maximum value read from stick for Raw stick trim exceeded [4095]
pdi_stickrawtrans3532 Invalid transformation type for stick
pdi_stickcfg3536 Invalid destination of stick device data
pdi_tllhcompressed537 Longitude/Latitude outside range [-π,π]/[-0.5π,0.5π]
pdi_tunpatchset0538 Patch selected as first has not been enabled
pdi_tunpatchset1539 Patch selected as next has not been enabled
pdi_tunpatchset2540 Patchtype point has not been enabled
pdi_tunpatchset3541 Patchtype line has not been enabled
pdi_tunpatchset4542 Patchtype orthodrome has not been enabled
pdi_tunpatchset5543 Patchtype arc has not been enabled
pdi_tunpatchset6544 Patchtype ellipse has not been enabled
pdi_tunpatchset8546 No patchtype has been enabled
pdi_Ubxcfgnav5547 Dynmodel out of range or incorrect UTC time
pdi_Ubxcfgnavx5548 Maximum acceptable AssistNow Autonomous orbit error outside range [5, 1000]
pdi_Ubxcfgport549 Port (for Ubx?) is neither SPI nor SCI
pdi_Ubxcfgrate550 Invalid Ublox configuration rate
pdi_Ubxcfgsbas551 Maximum number of SBAS prioritized tracking channels exceeded [3]
pdi_atunarray0552 Invalid Tunarray index
pdi_atunarray1553 Invalid Tunarray size
pdi_Ubxcfgtmode3554 Error in receiver mode, neither enabled nor disabled
pdi_Uclk555 Invalid chrono event
pdi_Uvarsensor556 Id for Uvar out of range for Uvarsensor, or desired frequency too low ( <1Hz)
pdi_Uclkmgr557 Maximum number of event user chronos exceeded
pdi_varinit0558 Maximum array size exceeded on initial values for user variables
pdi_varinit1559 Initialized variable is unwritable
pdi_vref0560 Maximum ID of Rvar variable exceeded in Vref
pdi_vref1561 Maximum ID of Uvar variable exceeded in Vref
pdi_vref2562 Maximum ID of Bvar variable exceeded in Vref
pdi_vref3563 Invalid type of variable in Vref
pdi_xclkcfg0564 Period time non-positive in event
pdi_xclkcfg1565 Invalid period mode
pdi_xclkcfg2566 Chrono position direction not correctly normalized
pdi_xclkcfg3567 Invalid type of chrono
pdi_blk_batch570 Maximum allowed block nesting depth exceeded [6] or incorrect number of inputs/outputs for block Patch
pdi_blk_ifelse571 Error in the connections for block if/else
pdi_blk_switch572 Error in the connections for block switch
pdi_blk_switch0573 Invalid switch/ifelse/phase block configuration
pdi_blkmgr574 Invalid block manager configuration
pdi_pinmux576 Invalid switch/ifelse/phase block output configuration
pdi_blk_switchmap577 Invalid mapping to cases in switch/phase block
pdi_accellimit579 Envelope’s falling or rising edge is out of accepted limits
pdi_circle583 Circle radius is less than or equal to 0
pdi_height584 Height type is neither relative nor absolute
pdi_heightabs585 Invalid absolute height type
pdi_rwy586 Invalid runway preferred type
pdi_driver588 Problem in Driver block configuration
pdi_mwk592 Gyroscope measurement error
pdi_opinctrl593 Invalid PID controller input type
pdi_pid594 Invalid PID integral configuration (tau must be ≥ 0)
pdi_prediction595 Error in the Model Prediction Control algorithm. Prediction Horizon out of range or zero diagonal matrix R
pdi_sysid596 Error ID for given pdi check
pdi_tsched597 Error ID for given pdi check
pdi_dwma598 Error ID for given pdi check
pdi_iir599 Error ID for given pdi check
pdi_butterworth600 Error ID for given pdi check
pdi_usre2601 Error incorrect user sensor variance
pdi_ubxcfgtp5603 Ublox time pulse configuration
pdi_cfgmgr_load_secure604 Error loading secure mode
pdi_cfgmgr_finit605 Error PDI files
pdi_cfgmgr_timeout606 Error, timeout while loading PDIs
pdi_invalidrotmat607 Invalid rotation matrix (cannot be inverted)
pdi_apsel608 Number of autopilots for redundancy less than 3
pdi_vblk_apsel609Invalid block AP selection configuration channel exceeds maximum number
pdi_vblk_arcade_bounce610 Error in the connections for block Arcade Bounce
pdi_vblk_arcade_extend611 Error in the connections for block Arcade Extend
pdi_vblk_btor612 Error in the connections for bool to real block
pdi_vblk_bound613 Error in the connections for block Bound
pdi_rldcfg0614 Invalid dynamic pressure EKF entrance configuration
pdi_smoothvar615 Smoother error
pdi_ubx_tout0616 Could not receive ACKs from UBlox
pdi_ubx_tout1617 Could not receive polling from Ublox
pdi_ubx_nack618 A Ublox configuration message was rejected by a Ublox device (GNSS)
pdi_guid_pid619 Invalid type of guidance controller
pdi_cmd_leg620 Guidance uses an invalid runway or site
pdi_mixarray622 Error in mixarray construction (possibly there is not enough RAM memory to store all the blocks)
pdi_xrtable623 Invalid number of entries for XrTable
pdi_blk_varset624 Block trying to write in an invalid variable, possibly the selected variable is not user writable
pdi_tuntrait625 Error trying to resize an array out of its maximum size
pdi_asuite626 Selected dynamic pressure sensor is not valid in this hardware version
pdi_xpcmap627 Invalid producer/consumer in I/O connections
pdi_blk_arraysplit628 Invalid block: array of less than 2 elements cannot be split
pdi_blk_array629 Bundle block error, it must have more than one input and the input sizes must be one
pdi_vblk_varget630 Invalid ID for block Read Real
pdi_vblk_vec_ops631 Error in either Vector: Add, Subtract, Cross product, Matrix rotation or Matrix product
pdi_autotune633 Invalid maximum duration of autotuning process or invalid number of stages for FFT
pdi_vblk_azeld1634 Error in the connections for block azeld → xyz
pdi_vblk_azeld635 Error in the connections for block xyz → azeld
pdi_vblk_dot636 Error in the connections for block Dot Product
pdi_vblk_enctrl637 Error in the connections for block Energy Control or invalid conversion factor from speed difference to desired acceleration
pdi_vblk_bnxb1638 Error in the connections for block(s) AND/OR
pdi_vblk_r1xr1639 Error in the connections for block x or invalid subfunction for the block
pdi_vblk_r2xr1640 Error in the connections for block x+y or invalid subfunction for the block
pdi_vblk_rnxr1641 Error in the connections for block(s) Multiply/Add Elements/Norm or invalid subfunction for the block(s)
pdi_vblk_iir642 Error in the connections for block IIR Filter or invalid parameters for the transfer function
pdi_vblk_kmultvec643 Error in the connections for block Scale
pdi_vblk_manual644 Error in the connections for block Manual or invalid stick control channel
pdi_vblk_minmax645 Error in the connections for block(s) Min/Max
pdi_vblk_mix646 Error in the connections for block MIX or invalid mix control channel
pdi_vblk_movern647 Error in the connections for block MIX Move
pdi_vblk_not648 Error in the connections for block NOT
pdi_vblk_phase649 Default case does not exist for block Phase Switch
pdi_vblk_tsched651 Error in the connections for block T-Sched PID
pdi_vblk_pid652 Invalid configuration or connection of a PID block
pdi_vblk_poly653 Error in the connections for block Polynomial
pdi_vblk_posset654 Error in the connections for block Write Feature or Fid is not user writable
pdi_vblk_predictive655 Error in the connections for block Predictive Control or number of elements for numerator/denominator unmatched to the expected input size
pdi_vblk_ramp656 Error in the connections for block Ramp or rise time/settling time less than (or equal to) 0
pdi_vblk_matvec657 Error in the connections for block Linear Transformation or matrix size unmatched to the expected input size
pdi_vblk_rtable3d658 Error in the connections for block 3D Table Interpolation
pdi_vblk_rtob659 Error in the connections for block Real to Bool
pdi_vblk_rtou660 Error in the connections for block Real to Integer
pdi_vblk_runwrap661 Error in the connections for block [-π,π] Unwrap
pdi_vblk_utor662 Error in the connections for block Integer to Real
pdi_vblk_relthis663 Error in the connections for block Relative Vector
pdi_cancfg1664 Number of mailboxes dedicated to rx exceeds maximum [32] or the filter applied to mailbox subset exceeds maximum filter id
pdi_stickvar_cfg665 Decimate time is higher than the minimum period or number of stick virtual inputs exceeds maximum configured for block Virtual stick
pdi_vblk_gimbal666 Error in the connections for block Gimbal
pdi_vblk_hysteresis667 Error in the connections for block Hysteresis
pdi_vblk_arctrim668 Error in the connections for block Arc Trim or control vector unmatched to expected size
pdi_blockprog669 Incomplete set of LSB bits or with bit holes for execution mask or slot is not within the mask
pdi_vblk_n2b670 Error in the connections for block NED to Body/Body to NED
pdi_vblk_pwm671 Error in the connections for block PWM or PWM id exceeds maximum
pdi_vblk_stick672 Error in stick block, connections, dimensions of matrices or stick sources could be wrong
pdi_vblk_u2s673 Error in actuator block, connections or dimensions of matrices could be wrong
pdi_vblk_interp674 Error in vector interpolation block, connections or sizes could be wrong, also the points in the table must be sorted in increasing order of x
pdi_vblk_ratelim678 Error in the connections for block Rate limiter
pdi_vblk_clock679 Unable to reset the clock timer in block Clock
pdi_vblk_mult_varget680 Unable to initialize output vector or invalid variable id in block Read Multiple Reals
pdi_vblk_mult_varset681 Error in the connections for block Write Multiple Bits/Write Multiple Reals or input vector different from input variables or variable not user writable
pdi_vblk_pid_static682 Unable to subscribe autotune in block PID
pdi_vblk_quatctrl683 Set of configurable variables cannot be 0 or outside their range in block Quaternion Control
pdi_vblk_senstp685 Error in pressure sensor block, could be that the selected pressure sensor in invalid in the current hardware or that the configured variance is negative or zero
pdi_vblk_sengnss686 Error for block GNSS sensor
pdi_vblk_ekfpos687 Error for block EKF position
pdi_vblk_ekfvel688 Error for block EKF Velocity
pdi_vblk_ekfmis689 Error for block EKF Misalignment
pdi_vblk_drnmis690 Error for block EKF GNSS compass
pdi_vblk_senrel691 Error for block Relative position (Sensors)
pdi_vblk_ekfdem692 Error for block EKF Terrain Height
pdi_vblk_senmag693 Error in magnetometer sensor block, the selected might be invalid in your current hardware or the configured variance is negative or zero
pdi_mdg_gain694 Error for block Madgwick Gain Computer
pdi_vblk_senalt696 Error for block Altimeter
pdi_vblk_ekfalt697 Error for block EKF Altitude
pdi_vblk_ekfvdn698 Error for block EKF Velocity Down
pdi_vblk_nav699 Error for block Navigation
pdi_e2acc700 Error for variance increment due to high acceleration
pdi_vblk_ekfsplit701 Error for block EKF Split
pdi_vblk_fft703 Error ID for block FFT
pdi_vblk_ecu705 Error ID for block ECU control
pdi_vblk_fuzzy706 Error ID for block Fuzzy Logic Controller
pdi_vblk_guidance707 Input of guidance block could not be connected
pdi_vblk_sysid709 Error ID for block System Identification
pdi_cex_pwm710 Error ID for CEX pwm arbitration, src ID greater than pulses array
pdi_cex_esc_tm711 Error ID for CEX ESC period
pdi_cex_mcu_tm712 Error ID for CEX MCU period
pdi_vblk_climb713 Incorrect climb block operation
pdi_vblk_leg714 Incorrect leg block operation
pdi_flyto715 Incorrect fly to command (non-existing patch)
pdi_vblk_approach716 Incorrect approach block operation
pdi_vblk_yawing717 Incorrect yawing block configuration
pdi_vblk_siggen718 Incorrect signal generation configuration
pdi_vblk_pnav719 Incorrect PNAV guidance configuration
pdi_vblk_genex720 Incorrect GENEX guidance configuration
pdi_vblk_modpnav721 Incorrect ModPNAV guidance configuration
pdi_blk_lib722 Incorrect library
pdi_vblk_ewma723 Incorrect EWMA block configuration
pdi_uarray_resize724 Incorrect uarray resize
pdi_oprvar725 Incorrect operation/setup rvar configuration
pdi_block_const726 Error in block const
pdi_block_posget727 Error in block posget
pdi_block_pnavbase728 Error in block pnav base
pdi_block_arcade0729 Error in block arcade
pdi_unescape730 Error in escape itport
pdi_initial_alignment731 The internal AHRS or EKF navigation estimation algorithm could not compute an initial orientation. Try commanding an initial yaw or adding an automation to do so
pdi_fft_block_disable732 The FFT block is temporarily disabled in this version
pdi_vblk_acclim733 Error in block acceleration limiter
pdi_ewma_avgvar734 Error in EWMA average/variance time constants
pdi_sensor_fusion735 Time constants for sensor fusion algorithm are incorrect
pdi_oprng736 Error in operation range configuration
pdi_oprng_check737 Error in operation range check
pdi_vgeoref738 Error in vgeoref configuration
pdi_notch_filter739 Incorrect notch filter parameters
pdi_notch_frequency740 Incorrect notch filter frequency
pdi_geoid_version741 Incorrect geoid version in SD
pdi_vblk_integrator742 Error in the connections for block Integrator
pdi_vblk_derivative743 Error in the connections for block Derivative
pdi_wrapper_ref744 Incorrect envelope range (minimum must be less or equal than maximum)
pdi_sensor_fusion_sel745 Selected gyroscopes or accelerometers are invalid in this hardware or the default sensor is not active
pdi_volume_id746 Incorrect volume identifier
pdi_fload_missing747 Missing file from file system
pdi_event_log770 Maximum number of fields reached
pdi_onboard_log771 Maximum number of fields reached
pdi_fast_log772 Maximum number of fields reached
pdi_arbitration10000 Error ID for Arbitration cfg
pdi_arbitration_can10001 Error ID for Arbitration_can cfg
pdi_arbitration_can110002 Error ID for Arbitration_can cfg
pdi_arb_cfg010003 Error ID for Arb cfg preferred ap oor
pdi_arb_cfg110004 Error ID for Arb cfg method oor (out of range)
pdi_arb_cfg210005 Error ID for Arb cfg tmin oor
pdi_arb_cfg310006 Error ID for Arb cfg hysteresis oor
pdi_ap_nvars10007 Error ID for Autopilot nvars oor
pdi_apcfg_nvars10008 Error ID for Autopilot cfg nvars oor
pdi_jetibox10009 Error ID for sci identifier of Jetibox cfg oor
pdi_jetibox_fmsgcmd10010 Error ID for jetibox fmsg cmd oor
pdi_arb_init_time10011 Error ID for Arbiter Power Init Time less than 0
pdi_arb_varcfg10013 Incorrect arbiter variable configuration
pdi_hs_base_can_id15000 High speed telemetry invalid Base CAN Id
pdi_hs_tm_nvars15001 High speed telemetry number of variables too big
pdi_vmc_motor20000 Motor cfg is not valid
pdi_vmc_control_mode20001 Control mode is invalid
pdi_vmc_encoder_nbits20002 Number of bits for encoder is invalid
pdi_mc_vmotor20003 Virtual motor cfg invalid
pdi_mc_smo20004 Slide Mode Observer cfg invalid
pdi_mc_control20005 Control cfg invalid
pdi_mc_fault_detection20006 Fault detection cfg invalid
pdi_mangle_rate20007 Invalid filter time constant
pdi_low_pll20008 Invalid cut-off frequency
pdi_ex_ussa76_cmd20009 Invalid period to send external USSA76 calibration command
pdi_cfgmr_length31999 Unexpected size of PDI or command
pdi_cfg_file32000 Error on PDI or command (subtract 32000 to know the Id)
pdi_check_test0xFFFFError ID for given PDI check.

List of File System Errors

Integer variable File system status (UVar 96) represents several DFS2 FS-related error states, as each of its 16 bits indicates a specific error condition.

File system status

Below is a list of potential error conditions associated with each bit:

ID Error description
0Index sector is not correct (1 if not correct - 0 if correct)
1Error initializing SD (1 if not correct - 0 if correct)
2Nun& partition bigger than allowed (1 if bigger - 0 if not)
3No more descriptor available (1 if not available - 0 if available)
4The descriptor of a file was not correct (CRC failed) (1 if fail - 0 if not)
5The new descriptor couldn't be created (1 if not created - 0 if created)
6Error updating the file size (1 if error updating - 0 if no error)
7Error formatting because of system description size (1 if error formatting - 0 if not)
8Error formatting driver not initialized (1 if error formatting - 0 if not)
9Error formatting maximum partition number overpassed (1 if error formatting - 0 if not)
10Error formatting not able to write index sector (1 if error formatting - 0 if not)
11Error formatting partition not enabled (1 if error formatting - 0 if not)
12Error writing the index for the log controller (1 if error formatting - 0 if not)
13File was destroyed but was not closed or had pending requests (1 if not closed or pending requests - 0 if closed or had no pending requests)
14Unable to read a sector (1 if unable - 0 if able)

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