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 Error bit. 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.

Type ID Name
UVar0Actuator Mode
UVar1Phase Identifier
RVar6Yaw
RVar7Pitch
RVar8Roll
BIT100Position Not Fixed
UVar201Current Section
UVar204Current patchset ID (needed for guidance display)
RVar300Relative Timestamp
RVar505North Ground Velocity
RVar506East Ground Velocity
RVar507Down Ground Velocity
UVars - 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 Error
9PDI Error
12System Power Up 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
51IMU 0 Error
52IMU 1 Error
53Magnetometer 0 Error
73CAN-A Error
74CAN-B Error
87GNSS1 Module Error
88GNSS2 Module Error
117Main Power Error
118SUC Power Error
400C1 Low Frequency Fail
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
35000-35299 MC110 motor controller + Address Specific address of a MC110 unit
35300-39999 MC110 v2 motor controller + Address Specific address of a MC110 v2 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 Error RAM allocation - 0 for Error, i.e. trying to use more than available memory, 1 for memory allocation ok
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 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 Fail, i.e. stack overflow of Core 1, 1 for OK
17 Stack C2 usage FAIL 0 for Fail, i.e. stack overflow of core 2, 1 for OK
18 PDI disabled PDI Mode - 0 for disabled, 1 for enabled
📝
20-46
4X Bit variables For more information, check BIT Variables - 4x Software Manual
47 4X 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 IMU 0 Error Sensor IMU 0 - 0 for Error, 1 for OK
52 IMU 1 Error Sensor IMU 1 - 0 for Error, 1 for OK
53 Magnetometer 0 Error Internal 0 Magnetometer - 0 for Error, 1 for OK
55 Sensor-External Magnetometer (LIS3MDL) External LIS3MDL magnetometer - 0 for Error, 1 for OK
56 Sensor-Static pressure 0 Static Pressure Sensor 0 - 0 for Error, 1 for OK
57 Sensor-Static pressure 1 Static Pressure Sensor 1 - 0 for Error, 1 for OK
58 Sensor-Dynamic pressure Dynamic Pressure Sensor 0 - 0 for Error, 1 for OK
59 Sensor-External I2C devices Error 0 for Error, 1 for OK
60-64 Sensor-External I2C device 0-4 Error External communication I2C device 0-4 - 0 for Error, 1 for OK
65 SCI-A Transmitting (LTE/EXT. UART) Serial Communication Interface LTE/EXT. UART transmission - 0 for Error, 1 for OK
66 SCI-A Receiving (LTE/EXT. UART) Serial Communication Interface LTE/EXT. UART reception
- 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
67 SCI-B Transmitting (LOS) Serial Communication Interface LOS transmission - 0 for Error, 1 for OK
68 SCI-B Receiving (LOS) Serial Communication Interface LOS reception
- 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
69 SCI-C Transmitting (RS485) Serial Communication Interface RS485 transmission - 0 for Error, 1 for OK
70 SCI-C Receiving (RS485) Serial Communication Interface RS485 reception
- 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
71 SCI-D Transmitting (RS232) Serial Communication Interface RS232 transmission - 0 for Error, 1 for OK
72 SCI-D Receiving (RS232) Serial Communication Interface RS232 reception
- 0 for Error, i.e. not receiving, 1 for OK, i.e. 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 fixed
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 Error Sensor IMU 2 - 0 for Error, 1 for OK
84 Sensor-Static pressure 2 Static Pressure Sensor 2 - 0 for Error, 1 for OK
85 Magnetometer 1 Error 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 Error Sensor IMU 3 - 0 for Error, 1 for OK
91 Magnetometer 2 Error Internal 2 Magnetometer - 0 for Error, 1 for OK
92 Magnetometer reserved 0 for Error, 1 for OK
93 SCI Expander (v4.8+) SCI Expander for hardware version 4.8 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 Error CAN A-B communication - 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
104-105 Stick PPM 0-1 not detected Stick PPM 0-1 - 0 for not detected, 1 for detected
📝
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
108-109 Stick PPM 2-3 not detected Stick PPM -3 - 0 for not detected, 1 for detected
📝
110
Stick Not Detected Stick detection - 0 for not detected, 1 for OK
111-112 CAN-A-B Transmitting Error CAN signals A-B - 0 for Error, i.e. not transmitting, 1 for OK, i.e. transmitting
113 Iridium not 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 OK
116 Radar Altimeter CAN-RX Error Radar Altimeter Reception State - 0 for Error, 1 for OK
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 if cruise guidance is not hovering, 1 if cruise guidance is hovering
120-123 Pulse 0-3 not detected Pulse 0-3 detection - 0 for pulse not detected, 1 for detected
📝
124-129
4X 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 OK
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
133 Operation Error 0 if an operation error has occurred, 1 if no operation error has occurred
137 Wind Estimation Command Already Received 0 if wind estimation was not initialized by command, 1 if wind estimation was initialized by command
140 Simulated navigation 0 for simulated navigation off, 1 for simulated navigation on
150 External VCP Navigation Error External VCP Navigation state - 0 for Error, 1 for OK
📝
160
External Var Navigation Error External Var Navigation state - 0 for Error, 1 for OK
170 Selected Accelerometer Error Selected accelerometer - 0 for Error, 1 OK, i.e. at least one of the selected accelerometers is OK
171 Selected Gyroscope Error Selected gyroscope - 0 for Error, 1 O, i.e. if at least one of the selected gyroscopes is OK
172 Bias Accelerometer Saturated 0 for bias Saturated, 1 for OK, i.e. not satured
173 Bias Gyroscope Saturated 0 for bias Saturated, 1 for OK, i.e. not satured
📝
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 Static Pressure Sensors Error Static Pressure Sensors status - 0 for Error, 1 for OK
189 Magnetometer Sensors Error Magnetometer Sensors status - 0 for Error, 1 for OK
190 Internest ultrasound position status Error Internest ultrasound position status - 0 for Error, 1 for OK
191 Internest ultrasound angle status Error Internest ultrasound angle status - 0 for Error, 1 for OK
200 GNSS1 Navigation Down GNSS1 Navigation status - 0 for GNSS Navigation Down, i.e. not used, 1 for GNSS Navigation ON, i.e. used
201 DGNSS1 Input Off DGNSS1 Input status - 0 for DGNSS1 Input Off, i.e. neither GNSS compass nor RTK activated, 1 for DGNSS1 Input ON, i.e. one of them activated
202 DGNSS1 Navigation Off DGNSS1 Navigation status - 0 for DGNSS1 Navigation Off, i.e. neither GNSS compass nor RTK used, 1 for DGNSS1 Navigation ON, i.e. one of them used
203 GNSS1 Survey In Off GNSS1 Survey In status - 0 for GNSS1 Survey In Off, i.e. neither GNSS compass survey nor RTK OFF, 1 for GNSS1 Survey In, i.e. 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
4X Bit variables For more information, check BIT Variables - 4x Software Manual
300 GNSS2 Navigation Down GNSS2 Navigation status - 0 for GNSS Navigation Down, i.e. not used, 1 for GNSS Navigation ON, i.e. used
301 DGNSS2 Input Off DGNSS2 Input status - 0 for DGNSS2 Input Off, i.e. neither GNSS compass nor RTK activated, 1 for DGNSS2 Input ON, i.e. one of them activated
302 DGNSS2 Navigation Off DGNSS2 Navigation status - 0 for DGNSS2 Navigation Off, i.e. neither GNSS compass nor RTK used, 1 for DGNSS2 Navigation ON, i.e. one of them used
303 GNSS2 Survey In Off GNSS2 Survey In status - 0 for GNSS2 Survey In Off, i.e. neither GNSS compass survey nor RTK OFF, 1 for GNSS2 Survey In, i.e. 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) - 0 for Error, 1 for OK
309 SCI-E Receiving (LTE) SCI-E Receiving (LTE) - 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
310 SCI-F Transmitting (LTE Aux.) SCI-F Transmitting (LTE Aux.) - 0 for Error, 1 for OK
311 SCI-F Receiving (LTE Aux.) SCI-F Receiving (LTE Aux.) - 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
312 SCI E Error (LTE) SCI-E (LTE) - 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
313 SCI F Error (LTE Aux.) SCI-F (LTE Aux.) - 0 for Error, i.e. not receiving, 1 for OK, i.e. receiving
329 3.3V Power Source Error 0 for Error, 1 for OK
330 Jetibox COMM Error Jetibox is communicating properly - 0 for Error, 1 for OK
331 CEX HI-3210 Error HI-3210 is working properly - 0 for Error, 1 for OK
351 Planet Satcom connection Planet Satcom is connected - 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 Fail C1 Low Frequency - Dependent on CIO Running Frequency (RVar 2057) (C1 low frequency)

  • 0 for Fail → CIO Running Frequency < 10 Hz
  • 1 for OK → CIO Running Frequency > 10 Hz
401 GNC Fail 0 for Fail ('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 Error 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 calibration status - 0 for not calibrated, 1 for calibration OK
📝
487
MC Phase V Current Calibration Error ADC phase V calibration status - 0 for not calibrated, 1 for calibration OK
📝
488
MC Phase W Current Calibration Error ADC phase W calibration status - 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 V 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 ON 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 Ground effect e2 compensation status - 0 for disabled, 1 for enabled
📝
501
Ground effect compensation measurement disabled Ground effect correction limit compensation status - 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
504 Geocaging not OK Bit to indicate all geocaging polygons comply with standard - 0 for No complying, 1 for Complying
600 Wind Estimation Off 0 for disabled, 1 for enabled
📝
700-731
Servo 0-31 Saturated 0 for Saturated, 1 for OK
📝
732-733
Phase U-W Error 0 for Error, 1 for OK
📝
734
HW DC link Error 0 for Error, 1 for OK
📝
735-736
HW over-current AC-DC Error 0 for Error, 1 for OK
📝
737
HW Ground Fault Detection Error 0 for HW Ground Fault Detection Error, 1 for HW Ground Fault Detection OK
📝
738
HW Power Regulator Error 0 for HW Power Regulator error, 1 for HW Power Regulator OK
📝
739
HW trip PWM Error 0 for HW general error to trip PWM, 1 for HW general to trip PWM OK
📝
740
Disconnected HW battery 0 for Battery disconnected, 1 for Battery connected
📝
741
DC current calibration Error 0 for DC current calibration Error, 1 for DC current calibration 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
1010-1169 Custom msg 0-159 Rx Error Custom message timeout - 0 for Error, 1 for OK
📝
1170-1171
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
📝
1172
Entrance EKF GNSS EXT OFF External GNSS information considered in EKF Navigation - 0 for entrance EKF GNSS EXT OFF, 1 for ON
📝
1173
Entrance EKF Internest OFF Internest information considered in EKF Navigation - 0 for entrance EKF internest OFF, 1 for ON
📝
1174
Entrance EKF GPSCOMPASS OFF GNSS Compass information considered in EKF Navigation - 0 for entrance EKF GPSCOMPASS OFF, 1 for ON
📝
1175
Entrance EKF Magnetometer OFF Magnetometer information considered in EKF Navigation - 0 for entrance EKF magnetometer OFF, 1 for ON
📝
1176
Entrance EKF Static press OFF Static Pressure sensor information considered in EKF Navigation - 0 for entrance EKF static pressure OFF, 1 for ON
📝
1177
Entrance EKF Altimeter press OFF Altimeter information considered in EKF Navigation - 0 for entrance EKF altimeter OFF, 1 for ON
📝
1178
Entrance EKF Radar-altimeter press OFF Radar Altimeter information considered in EKF Navigation - 0 for entrance EKF radar-altimeter OFF, 1 for ON
📝
1179
Entrance EKF DEM OFF DEM information considered in EKF Navigation - 0 for entrance EKF DEM OFF, 1 for ON
📝
1183
External navigation sensor Error External navigation sensor - 0 for Error, 1 for OK
📝
1184
External IMU 0 accelerometer Error External IMU 0 accelerometer - 0 for Error, 1 for OK
📝
1185
External IMU 0 gyroscope Error External IMU 0 gyroscope - 0 for Error, 1 for OK
📝
1186
External IMU 1 accelerometer Error External IMU 1 accelerometer - 0 for Error, 1 for OK
📝
1187
External IMU 1 gyroscope Error External IMU 1 gyroscope - 0 for Error, 1 for OK
📝
1188
External magnetometer 0 Error External magnetometer 0 - 0 for Error, 1 for OK
📝
1189
External magnetometer 1 Error External magnetometer 1 - 0 for Error, 1 for OK
📝
1190-1191
Sniffer msg 0-1 Rx Error Sniffer receiver message 0-1 - 0 for Error, 1 for OK
📝
1200-2199
User BIT 00-999 error User bit 0-999 - 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) (Deprecated) m/s Speed relative to the airmass in which the vehicle is moving (IAS measurement corrected with Standard Atmosphere data)

Warning
Deprecated variable
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
27 Gravity at UAV's position m/s² Gravity at UAV's position positive down
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 (Deprecated) byte SD used memory space

Warning
Deprecated variable
302 Free Memory Space (Deprecated) byte SD free memory space

Warning
Deprecated variable
📝
303
Dynamic Pressure (Deprecated) Pa Physical measurement from Pitot (dynamic pressure)

Warning
Deprecated variable
📝
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 Magnetometer 0 Raw X in SI T Internal 0 Magnetometer raw measurement for X axis
323 Magnetometer 0 Raw Y in SI T Internal 0 Magnetometer raw measurement for Y axis
324 Magnetometer 0 Raw Z in SI T Internal 0 Magnetometer raw measurement for Z axis
325 Magnetometer 0 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 1 Raw Measurement Pa Static pressure sensor 1 raw measurement
345 Static Pressure Sensor 1 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 0 Raw Measurement Pa Static pressure sensor 0 raw measurement
349 Static Pressure Sensor 0 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 2 Raw Measurement Pa Static pressure sensor 2 raw measurement
369 Static Pressure Sensor 2 Temperature K Static pressure sensor 2 temperature
370 Magnetometer 1 Raw Measure X Converted to SI T Internal 1 Magnetometer raw measurement for X axis converted to SI
371 Magnetometer 1 Raw Measure Y Converted to SI T Internal 1 Magnetometer raw measurement for Y axis converted to SI
372 Magnetometer 1 Raw Measure Z Converted to SI T Internal 1 Magnetometer raw measurement for Z axis converted to SI
373 Magnetometer 1 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
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 Magnetometer 2 Raw Measure X Converted to SI T Internal 2 Magnetometer raw measurement for X axis converted to SI
394 Magnetometer 2 Raw Measure Y Converted to SI T Internal 2 Magnetometer raw measurement for Y axis converted to SI
395 Magnetometer 2 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
428 External navigation yaw rad External navigation yaw
429 External navigation pitch rad External navigation pitch
430 External navigation roll rad External navigation roll
431 External navigation p rad/s External navigation p (angular speed in x body axis)
432 External navigation q rad/s External navigation q (angular speed in y body axis)
433 External navigation r rad/s External navigation r (angular speed in z body axis)
434 External navigation north velocity m/s External navigation north velocity
435 External navigation east velocity m/s External navigation east velocity
436 External navigation down velocity m/s External navigation down velocity
437 External navigation x-body acceleration m/s² External navigation x-body acceleration
438 External navigation y-body acceleration m/s² External navigation y-body acceleration
439 External navigation z-body acceleration m/s² External navigation z-body acceleration
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
800-823 PWM 0-23 customType Pulse Width Modulation signal 0-23
📝
900-915
Stick Input r0 - r15 customType Raw stick measurement r0-r15
📝
950-981
Stick Input s0 - s31 customType
Warning
Deprecated variables
📝
1000-1031
Stick Input y0 - y31 customType Servo position commanded stick y0-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 0-4
📝
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 CEX/MEX ADC 3.3V Input 0-1 V CEX/MEX ADC 3.3 V inputs 0 and 1
1322-1323 CEX/MEX ADC 5.0V Input 0-1 V CEX/MEX ADC 5.0 V inputs 0 and 1
1324-1325 CEX/MEX ADC 12.0V Input 0-1 V CEX/MEX ADC 12.0 V inputs 0 and 1
1326-1327 CEX/MEX ADC 36.0V Input 0-1 V CEX/MEX ADC 36.0 V inputs 0 and 1
1328-1329 CEX/MEX ADC vIn 0-1 V CEX/MEX External power supplies 0 and 1
1330 CEX/MEX PCB Temperature K CEX/MEX PCB Temperature (from ADC input)
1331 CEX/MEX ADC HW Version V Hardware version of CEX/MEX ADC
📝
1350-1369
4X 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
1483 External navigation sensor frequency Hz External navigation sensor frequency
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)
2058 MC 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
MC U-V-W Phase PWM Duty Cycle percentage MC 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 0-19 after servo saturation
📝
2450-2469
Inner controller output 0-19 customType Inner controller output 0-19
📝
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 Variable 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 Estimation Uncertainty (Element 0-0) (Deprecated) m/s 0-0 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2804
Wind Velocity Estimation Uncertainty (Element 1-0) (Deprecated) m/s 1-0 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2805
Wind Velocity Estimation Uncertainty (Element 2-0) (Deprecated) m/s 2-0 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2806
Wind Velocity Estimation Uncertainty (Element 0-1) (Deprecated) m/s 0-1 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2807
Wind Velocity Estimation Uncertainty (Element 1-1) (Deprecated) m/s 1-1 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2808
Wind Velocity Estimation Uncertainty (Element 2-1) (Deprecated) m/s 2-1 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2809
Wind Velocity Estimation Uncertainty (Element 0-2) (Deprecated) m/s 0-2 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2810
Wind Velocity Estimation Uncertainty (Element 1-2) (Deprecated) m/s 1-2 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2811
Wind Velocity Estimation Uncertainty (Element 2-2) (Deprecated) m/s 2-2 element from covariance matrix in wind estimation

Warning
Deprecated variable
📝
2812
Wind Azimuth Angle (Deprecated) degree Wind estimated azimuth

Warning
Deprecated variable
📝
2813
Wind Velocity in North-East plane (Deprecated) m/s Wind velocity norm xy in North-East plane

Warning
Deprecated variable
📝
2814
Head wind velocity North m/s Head wind velocity North
📝
2815
Head wind velocity East m/s Head wind velocity East
📝
2816
Head wind velocity Down m/s Head wind velocity Down
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
2908-2928 Time in Phase 0-20 s Time-lapse spent by the vehicle within phase 0-20
📝
3000-3031
Simulation Variable 0-31 customType Variables used for Simulation data
📝
3100-4099
User Variable 00-999 (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 4X 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 4X Veronte CAP Current Autopilot 1x selected.
For more information, check Integer Variables - 4x Software Manual
📝
55-75
4X 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
116 GNSS1 Spoofing detection state GNSS1 Spoofing detection state
117 Total number of Uvars used by GNSS Total number of Uvars used by GNSS
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
166 GNSS2 Spoofing detection state GNSS2 Spoofing detection state
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
397 External navigation sensor status External navigation sensor status
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 (Extended Kalman Filter)
  • 2: Simulated navigation (IRX source)
  • 3: External navigation using VCP (IRX source)
  • 4: External navigation using dedicated variables
  • 5: External navigation from Vectornav VN-300
  • 6: External sensor navigation
402 Raw position source identifier GPS identifier selected as main
📝
403
Selected static pressure sensor (Deprecated) Static pressure sensor selection

Warning
Deprecated variable
📝
404
Selected dynamic pressure sensor (Deprecated) 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
Selected magnetometer (Deprecated) 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 0-5
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
700 Planet Satcom connection Status Planet Satcom connection Status
701 Planet Satcom signal strength Planet Satcom signal strength
📝
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
Ping1090 - Sequence number (Deprecated)
Warning
Deprecated variable
📝
741
Sagetech MXS - Hemisphere data status (Deprecated) 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
Sagetech MXS - Ground track (Deprecated) 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
Sagetech MXS - Air speed (Deprecated) 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
📝
1000-1999
User Variable 00-999 (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
3072Regvars 00[lon, lat, height][rad, rad, m]Regvar 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.
8195Value used when invalid ID is tried[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 Point 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.
29696 - 30207Waypoint 00 - 511[lon, lat, height][rad, rad, m]Route waypoints.
30720 - 30987Volume vertex 00 - 267[lon, lat, height][rad, rad, m]Volume vertices.
45056 - 45087Operation Custom Point 00 - 31[lon, lat, height][rad, rad, m]Operation custom points.
46080Home[lon, lat, height][rad, rad, m]Home position.

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

Type ID Name
Bit Variables101No valid SRTM at UAV position
114No valid Geoid at UAV position
Real Variables2GS (Ground Speed)
3Heading
4Flight Path Angle
5Bank
6Yaw
7Pitch
8Roll
12p (Angular Velocity - X Body Axis)
13q (Angular Velocity - Y Body Axis)
14r (Angular Velocity - Z Body Axis)
15Forward Acceleration - X Body Axis
16Right Acceleration - Y Body Axis
17Bottom Acceleration - Z Body Axis
18RPM
19Front Ground Velocity
20Lateral Ground Velocity
21Velocity
12Forward Load Factor - X Body Axis
23Right Load Factor - Y Body Axis
24Bottom Load Factor - Z Body Axis
25Tangential Acceleration
26Estimated air density
27Gravity at UAV's position
28Co-Yaw
29Co-Pitch
30Co-Roll
31Angular Acceleration - X Body Axis
32Angular Acceleration - Y Body Axis
33Angular Acceleration - Z Body Axis
34Body to NED Quaternion qs
35Body to NED Quaternion qi
36Body to NED Quaternion qj
37Body to NED Quaternion qk
56Yaw Rate
57Pitch Rate
58Roll Rate
80Estimated gyro bias x
81Estimated gyro bias y
82Estimated gyro bias z
83Estimated accelerometer bias x
84Estimated accelerometer bias y
85Estimated accelerometer bias z
500Longitude
501Latitude
502WGS84 Elevation (Height Over the Ellipsoid)
503MSL (Height Above Mean Sea Level) - Altitude
504AGL (Above Ground Level) - Height
505North Ground Velocity
506East Ground Velocity
507Down Ground Velocity
1400Velocity - X Body Axis
1401Velocity - Y Body Axis
1402Velocity - Z Body Axis
2103Acceleration North
2104Acceleration East
2105Acceleration Down
Integer Variable25SRTM source at UAV's position
Feature Variable8192UAV position

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.

CodeExplanation
err_ok0No errors detected
err_gpio1GPIOs function configuration
err_odt_pool_sz2Incorrect pool size in on-demand telemetry
err_telemetry_alloc3Could not allocate new telemetry vector
err_patch_type4Incorrect patch type
err_patch_needs_next5Selected type of patch needs a next
err_max_poly_evt6Maximum limit of polygon events reached
err_channelmgr10Channel manager configuration
err_blk_cmp_pdi11Incorrect deserialization of compiled block data
err_blk_cmp12Incorrect output in compiled block
err_blk_cmp_desc13Invalid pin description in compiled block
err_sara15SARA sim type oor.
err_vblk_sensrtm16Block for SRTM sensor
err_arcx23Arcade axis set of options.
err_msg8_consumer_hi24Custom message consumer cannot be used in HI unless it is an external sensor
err_can_consumer_hi25CAN Custom message consumer cannot be used in HI unless it is an external sensor
err_modes27Stick configuration modes
err_blkekfstp41Static pressure to EKF adapter block
err_gnss_blocks45GNSS constellations configuration (more than allowed)
err_cansuite_gpio47CAN suite gpio
err_vrng48Range sensors
err_fmset50Custom message set
err_pwm54Pwm configuration
err_sniffer63Sniffer wires configuration
err_sniffer_read_only64Read-only variable selected in sniffer
err_fmsgc_read_only65Read-only variable selected in serial message consumer
err_canmsgc_read_only66Read-only variable selected in CAN message consumer
err_vref_read_only67Read-only vref variable
err_obstacle68Incorrect type of obstacle.
err_obsense69Obstacle sensing mode or type oor.
err_marks71Incorrect type of mark.
err_ext_nav_sen72Incorrect external navigation sensor configuration.
err_fmsg_p74Custom message producers msg id oor.
err_fmsg_c75Custom message consumers process parser oor.
err_fmsgcan_c76CAN custom msg consumer msg id oor.
err_telem77Telemetry configuration
err_fmsg_p_sz78Custom message producer occupancy is higher than allowed
err_fmsg_c_sz79Custom message consumer occupancy is higher than allowed
err_sci81SCI config error
err_events82Invalid event
err_actions83Actmgr - List of actions.
err_evact84Actmgr - List of related events and actions.
err_cmd_not_allowed85Commands not allowed
err_xpc_can_in87XPC for CAN messages input filters size ok
err_xpc_can_out88XPC for CAN messages output filters size ok
err_xpc_can_ser89XPC for CAN messages serialtocan size ok
err_xpc_can_gpio90XPC for CAN messages virtual gpios size ok
err_xpc_can_map91XPC for CAN messages and check their priority and connections.
err_xpc_u8_map92XPC for u8 messages and check their priority and connections.
err_internest93Internest version in rage
err_internest194Internest max_range_vbase in rage
err_internest295Internest max_range_vexplore in rage
err_gravity_ext96Incorrect gravity extractor for AHRS configuration
err_u8pkrsarray_size97Incorrect size for U8pkrsarray
err_ecap101Capture.
err_cappulse116ECAP pulse consumers
err_i2cdevs117I2C external devices
err_lossy_resize120Lossy resize error
err_rvector_resize121Rvector resize error
err_asciiparser122ASCII parser invalid configuration
err_telemetry_exceeded123Telemetry size exceeded
err_hi_3210_rx_tout154HI-3210 rx cannot be configured
err_hi_3210_tx_tout155HI-3210 tx cannot be configured
err_arbiter_cfg156Arbiter production configurable invalid
err_can_arbiter_cfg157CAN Arbiter configuration has not consistency with production file or/and it is invalid
err_cmd_rdvzset176Rendezvous command base_yaw oor
err_cmd_taxiget183Taxi guidance request command.
err_cmd_gtrack1188Invalid detour command
err_cmd_gtrack2189Invalid guidance block configuration.
err_cmd_speed192Cruise speed command
err_cmd_gtrack193Invalid detour command
err_cmd_gtrkset194Track request command
err_cmd_stksrcr208Get stick raw channels from selected source
err_cmd_vtolset212VTOL request command
err_ini_nok213Cannot change to a phase different from INI with System BIT not OK and out of PDI mode
err_cmd_nav215Navigation command
err_cmd_gpio218GPIO command
err_cmd_gpio1219GPIO command
err_cmd_gpio2220GPIO command
err_cmd_gpio3221GPIO command
err_cmd_phase222Commanded phase is out of range
err_cmd_gimbal1224Gimbal commands
err_cmd_gimbal225Gimbal commands
err_cmd_var235Variable set command
err_reset239Reset CPU IRX
err_acc2filt257Bosch IMU BMI088 (IMU2) Accelerometer filter
err_imu3_filter258ADIS16505 IMU filter not in range [0,6]
err_imu3_filter_bw259ADIS16505 IMU filter not compatible with Bandwidth limit
err_imu3_delta260ADIS16505 IMU invalid rate limit
err_imu2_delta261Bosch IMU BMI088 (IMU2) invalid rate limit
err_cansuite_in288CAN suite producer for veronte
err_cansuite_out289CAN suite consumer for veronte
err_cfg_can290CAN cfg
err_resize_can_cex291CEX CAN cfg
err_resize_can_commex292COMMEX CAN cfg
err_jeti_and_lift293Trying to configure jeti and lift (not enough memory)
err_relf500Tried to set feature relative to invalid feature, or set relative an "absolute-only" feature
err_jid501Invalid feature
err_canid502Invalid CAN id
err_cfgid_mode0503Invalid Cfgid PDI (number of PDIs does not match)
err_cfgid_mode1504Invalid Cfgid PDI mode
err_cmd_mgr505Expected command size does not match
err_cmd_mgr1506Expected command size does not match
err_cancfg507Invalid CAN configuration
err_decimator508Invalid decimator
err_sci_cfg509Invalid SCI configuration
err_field1510Maximum ID of real variable exceeded
err_field2511Maximum ID of user variable exceeded
err_field3512Maximum ID of bit variable exceeded
err_field4513Maximum number of decimals for real variable exceeded
err_field5514Overflow for real variable detected
err_field6515Incorrect CRC field
err_field7516Field matcher number of bits outside range
err_field8517Field maximum skippable bits exceeded
err_field9518Maximum ID of real variable saved as string exceeded
err_field10519Field type out of range
err_flogic520Invalid event composition (Flogic)
err_flogic1521Invalid event composition (Flogic)
err_flogic2522Invalid event composition type
err_fref523Invalid type of position reference
err_irxtable524Invalid 3Dtable mode or vector is non-decreasing
err_limit525Invalid limit event type
err_lsm6ds3_cfg526Accelerometer/Gyroscope settings outside range
err_pdi_ver527Incompatible PDI version, there are some PDI files in Veronte from a different version. Try migrating offline and uploading a complete migrated configuration
err_rvarsensor528Id for Rvar out of range for Rvarsensor
err_stickrawtrans0529K value in stick outside range [-100, 100] or 0
err_stickrawtrans1530Maximum value read from stick for Configured range exceeded [4095]
err_stickrawtrans2531Maximum value read from stick for Raw stick trim exceeded [4095]
err_stickrawtrans3532Invalid transformation type for stick
err_inc_counter533Invalid ID for incremental counter
err_stickcfg3536Invalid destination of stick device data
err_tllhcompressed537Longitude/Latitude outside range [-pi, pi]/[-0.5pi, 0.5pi]
err_tunpatchset0538Patch selected as first has not been enabled
err_tunpatchset1539Patch selected as next has not been enabled
err_tunpatchset2540Patch type does not exist
err_tunpatchset3541The route cannot have two consecutive patches of type point
err_tunpatchset4542Patchtype orthodrome has not been enabled
err_tunpatchset5543Patchtype arc has not been enabled
err_tunpatchset6544Patchtype ellipse has not been enabled
err_tunpatchset8546No patchtype has been enabled
err_Ubxcfgnav5547Dynmodel out of range or incorrect UTC time
err_Ubxcfgnavx5548Maximum acceptable AssistNow Autonomous orbit error outside range [5, 1000]
err_Ubxcfgport549Port (for Ubx?) is neither SPI nor SCI
err_Ubxcfgrate550Invalid Ublox configuration rate
err_Ubxcfgsbas551Maximum number of SBAS prioritized tracking channels exceeded [3]
err_atunarray0552Invalid Tunarray index
err_atunarray1553Invalid Tunarray size
err_Ubxcfgtmode3554Error in receiver mode, neither enabled nor disabled
err_Uclk555Invalid chrono event
err_Uvarsensor556Id for Uvar out of range for Uvarsensor, or desired frequency too low (<1Hz)
err_Uclkmgr557Maximum number of event user chronos exceeded
err_varinit0558Maximum array size exceeded on initial values for user variables
err_varinit1559Initialized variable is unwritable
err_vref0560Maximum ID of Rvar variable exceeded in Vref
err_vref1561Maximum ID of Uvar variable exceeded in Vref
err_vref2562Maximum ID of Bvar variable exceeded in Vref
err_vref3563Invalid type of variable in Vref
err_xclkcfg0564Period time non positive in event
err_xclkcfg1565Invalid period mode
err_xclkcfg2566Chrono position direction not correctly normalized
err_xclkcfg3567Invalid type of chrono
err_blk_batch570Maximum allowed block nesting depth exceeded [6] or incorrect number of inputs/outputs for block Patch
err_blk_ifelse571Error in the connections for block if/else
err_blk_switch572Error in the connections for block switch
err_blk_switch0573Invalid switch/ifelse/phase block configuration
err_blkmgr574Invalid block manager configuration
err_pinmux576Invalid switch/ifelse/phase block output configuration
err_blk_switchmap577Invalid mapping to cases in switch/phase block
err_accellimit579Envelope's falling or rising edge is out of accepted limits
err_polygrp581Index of polygon for group outside of range
err_polygon582Less than 3 polygon vertices
err_circle583Circle radius is less than or equal to 0
err_height584Height type is neither relative nor absolute
err_heightabs585Invalid absolute height type
err_rwy586Invalid runway preferred type
err_driver588Problem in Driver block configuration
err_mwk592Gyroscope measurement error
err_opinctrl593Invalid PID controller input type
err_pid594Invalid PID integral configuration (tau must be >= 0)
err_prediction595Error in the Model Prediction Control algorithm. Prediction Horizon out of range or zero diagonal matrix R
err_sysid596Error ID for given pdi check
err_tsched597Error ID for given pdi check
err_dwma598Error ID for given pdi check
err_iir599Error ID for given pdi check
err_butterworth600Error ID for given pdi check
err_usre2601Error incorrect user sensor variance
err_ubxcfgtp5603Ublox time pulse configuration
err_cfgmgr_load_secure604Error loading secure mode
err_cfgmgr_finit605Error PDI files
err_cfgmgr_timeout606Error; timeout while loading PDIs
err_invalidrotmat607Invalid rotation matrix (cannot be inverted)
err_flyto_setup608Error in fly to waypoint action
err_vblk_apsel609Invalid block AP selection configuration, channel exceeds maximum number
err_vblk_arcade_bounce610Error in the connections for block Arcade Bounce
err_vblk_arcade_extend611Error in the connections for block Arcade Extend
err_vblk_btor612Error in the connections for bool to real block
err_vblk_bound613Error in the connections for block Bound
err_rldcfg0614Invalid dynamic pressure EKF entrance configuration
err_ubx_tout0616Could not receive ACKs from UBlox
err_ubx_tout1617Could not receive polling from Ublox
err_ubx_nack618A Ublox configuration message was rejected by a Ublox device (GNSS)
err_guid_pid619Invalid type of guidance controller
err_cmd_leg620Guidance uses an invalid runway or site
err_mixarray622Error in mixarray construction (possibly there is not enough RAM memory to store all the blocks)
err_xrtable623Invalid number of entries for XrTable
err_blk_varset624Block trying to write in an invalid variable, possibly the selected variable is not user writable
err_tuntrait625Error trying to resize an array out of its maximum size
err_asuite626Selected dynamic pressure sensor is not valid in this hardware version
err_xpcmap627Invalid producer/consumer in I/O connections
err_blk_arraysplit628Invalid block: array of less than 2 elements cannot be split
err_blk_array629Bundle block error, it must have more than one input and the input sizes must be one
err_vblk_varget630Invalid ID for block Read Real
err_vblk_vec_ops631Error in either; Vector: Add, Subtract, Cross product or Matrix rotation
err_autotune633Invalid maximum duration of autotuning process or invalid number of stages for FFT
err_vblk_azeld1634Error in the connections for block azeld -> xyz
err_vblk_azeld635Error in the connections for block xyz -> azeld
err_vblk_dot636Error in the connections for block Dot Product
err_vblk_enctrl637Error in the connections for block Energy Control or invalid conversion factor from speed difference to desired acceleration
err_vblk_bnxb1638Error in the connections for block(s) AND/OR
err_vblk_r1xr1639Error in the connections for block
err_vblk_r2xr1640Error in the connections for block x+y or invalid subfunction for the block
err_vblk_rnxr1641Error in the connections for block(s) Multiply/Add Elements/Norm or invalid subfunction for the block(s)
err_vblk_iir642Error in the connections for block IIR Filter or invalid parameters for the transfer function
err_vblk_kmultvec643Error in the connections for block Scale
err_vblk_manual644Error in the connections for block Manual or invalid stick control channel
err_vblk_minmax645Error in the connections for block(s) Min/Max
err_vblk_mix646Error in the connections for block MIX or invalid mix control channel
err_vblk_movern647Error in the connections for block MIX Move
err_vblk_not648Error in the connections for block NOT
err_vblk_phase649Default case does not exist for block Phase Switch
err_vblk_tsched651Error in the connections for block T-Sched PID
err_vblk_pid652Invalid configuration or connection of a PID block
err_vblk_poly653Error in the connections for block Polynomial
err_vblk_posset654Error in the connections for block Write Feature or Fid is not user writable
err_vblk_predictive655Error in the connections for block Predictive Control or number of elements for numerator/denominator unmatched to the expected input size
err_vblk_ramp656Error in the connections for block Ramp or rise time/settling time less than (or equal to) 0
err_vblk_matvec657Error in the connections for block Linear Transformation or matrix size unmatched to the expected input size
err_vblk_rtable3d658Error in the connections for block 3D Table Interpolation
err_vblk_rtob659Error in the connections for block Real to Bool
err_vblk_rtou660Error in the connections for block Real to Integer
err_vblk_runwrap661Error in the connections for block [-pi,pi] Unwrap
err_vblk_utor662Error in the connections for block Integer to Real
err_vblk_relthis663Error in the connections for block Relative Vector
err_cancfg1664Number of mailboxes dedicated to rx exceeds maximum [32] or the filter applied to mailbox subset exceeds maximum filter id
err_stickvar_cfg665Decimate time is higher than the minimum period or number of stick virtual inputs exceeds maximum configured for block Virtual stick
err_vblk_gimbal666Error in the connections for block Gimbal
err_vblk_hysteresis667Error in the connections for block Hysteresis
err_vblk_arctrim668Error in the connections for block Arc Trim or control vector unmatched to expected size
err_blockprog669Incomplete set of LSB bits or with bit holes for execution mask or slot is not within the mask
err_vblk_n2b670Error in the connections for block NED to Body/Body to NED
err_vblk_pwm671Error in the connections for block PWM or PWM id exceeds maximum
err_vblk_stick672Error in stick block, connections, dimensions of matrices or stick sources could be wrong
err_vblk_u2s673Error in actuator block, connections or dimensions of matrices could be wrong
err_vblk_interp674Error in vector interpolation block, connections or sizes could be wrong, also the points in the table must be sorted in increasing order of x
err_vblk_ratelim678Error in the connections for block Rate limiter
err_vblk_clock679Unable to reset the clock timer in block Clock
err_vblk_mult_varget680Unable to initialize output vector or invalid variable id in block Read Multiple Reals
err_vblk_mult_varset681Error in the connections for block Write Multiple Bits/Write Multiple Reals or input vector different from input variables or variable not user writable
err_vblk_pid_static682Unable to subscribe autotune in block PID
err_vblk_quatctrl683Set of configurable variables cannot be 0 or outside their range in block Quaternion Control
err_vblk_senstp685Error 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
err_vblk_sengnss686Error for block GNSS sensor
err_vblk_ekfpos687Error for block EKF position
err_vblk_ekfvel688Error for block EKF Velocity
err_vblk_ekfmis689Error for block EKF Misalignment
err_vblk_drnmis690Error for block EKF GNSS compass
err_vblk_senrel691Error for block Relative position (Sensors)
err_vblk_ekfdem692Error for block EKF Terrain Height
err_vblk_senmag693Error in magnetometer sensor block, the selected might be invalid in your current hardware or the configured variance is negative or zero
err_mdg_gain694Error for block Madgwick Gain Computer
err_vblk_senalt696Error for block Altimeter
err_vblk_ekfalt697Error for block EKF Altitude
err_vblk_ekfvdn698Error for block EKF Velocity Down
err_vblk_nav699Error for block Navigation
err_e2acc700Error for variance increment due to high acceleration
err_vblk_ekfsplit701Error for block EKF Split
err_vblk_fft703Error ID for block FFT
err_vblk_ecu705Error ID for block ECU control
err_vblk_fuzzy706Error ID for block Fuzzy Logic Controller
err_vblk_guidance707Input of guidance block could not be connected
err_vblk_sysid709Error ID for block System Identification
err_cex_pwm710Error ID for CEX pwm arbitration, src ID greater than pulses array
err_cex_esc_tm711Error ID for CEX ESC period
err_cex_mcu_tm712Error ID for CEX MCU period
err_vblk_climb713Incorrect climb block operation
err_vblk_leg714Incorrect leg block operation
err_flyto715Incorrect fly to command (non-existing patch)
err_vblk_approach716Incorrect approach block operation
err_vblk_yawing717Incorrect yawing block configuration
err_vblk_siggen718Incorrect signal generation configuration
err_vblk_pnav719Incorrect PNAV guidance configuration
err_vblk_genex720Incorrect GENEX guidance configuration
err_vblk_modpnav721Incorrect ModPNAV guidance configuration
err_blk_lib722Incorrect library
err_vblk_ewma723Incorrect EWMA block configuration
err_uarray_resize724Incorrect uarray resize
err_oprvar725Incorrect operation/setup rvar configuration
err_block_const726Error in block const
err_block_posget727Error in block posguet
err_block_pnavbase728Error in block pnav base
err_block_arcade0729Error in block arcade0
err_unescape730Error in escape itport
err_initial_alignment731The 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
err_fft_block_disable732The FFT block is temporarily disabled in this version
err_vblk_acclim733Error in block acceleration limiter
err_ewma_avgvar734Error in EWMA average/variance time constants
err_sensor_fusion735Time constants for sensor fusion algorithm are incorrect
err_oprng736Error in operation range configuration
err_oprng_check737Error in operation range check
err_vgeoref738Error in vgeoref configuration
err_notch_filter739Incorrect notch filter parameters
err_notch_frequency740Incorrect notch filter frequency
err_geoid_version741Incorrect geoid version in SD
err_vblk_integrator742Error in the connections for block Integrator
err_vblk_derivative743Error in the connections for block Derivative
err_wrapper_ref744Incorrect envelope range (minimum must be less or equal than maximum)
err_sensor_fusion_sel745Selected gyroscopes or accelerometers are invalid in this hardware or the default sensor is not active
err_volume_id746Incorrect volume identifier
err_fload_missing747Detected missing file at fload blocking
err_hi_3210_rx_cfg748Incorrect HI-3210 RX configuration
err_mixer749Incorrect mixer block configuration or it does not fit in memory
err_scheduler_data750Incorrect data size for scheduler block
err_asc751Incorrect configuration of ASC block
err_scheduler752Incorrect configuration of scheduler block
err_aacg753Incorrect data size for mixer block
err_mat2quat754Incorrect input to matrix to quaternion block
err_quat2mat755Incorrect input to quaternion to matrix
err_wrench_frame756Incorrect inputs to the wrench frame block
err_ffc_3d_block757Incorrect configuration of ffc3d block
err_srv_def_limits758A default position is not within X limits for servo actuator
err_pfield_file759Error in loading the saved fields
err_vblk_wind760Invalid configuration for wind estimation block
err_vblk_senqinf761Invalid configuration for dynamic pressure sensor block
err_vblk_code_size762External code block: Size greater than maximum allowed (64KW)
err_vblk_code_empty763External code block empty. No code has been loaded
err_vblk_code_ptr764External code block: Invalid pointer detected
err_vblk_code_inputs765External code block: Inputs read error
err_vblk_code_outputs766External code block: Outputs write error
err_vblk_ekfadapter767Incorrect configuration in custom EKF adapter
err_vblk_compiledsil768Tried to use the compiled code block on a SIL configuration
err_event_log770Invalid Event-Driven Log Fields configuration
err_onboard_log 771Invalid On-Board Low Rate Log Fields configuration
err_fast_log772Invalid Fast Log Fields configuration
err_updt_magfield773Magnetic field's partition not updated correctly
err_updt_geoid774Geoid's partition not updated correctly
err_op_var_def_val775Operation variable default value outside of range
err_arbitration10000Error ID for Arbitration cfg
err_arbitration_can10001Error ID for Arbitration_can cfg
err_arbitration_can110002Error ID for Arbitration_can cfg
err_arb_cfg010003Error ID for Arb cfg preferred ap oor
err_arb_cfg110004Error ID for Arb cfg method oor(out of range)
err_arb_cfg210005Error ID for Arb cfg tmin oor
err_arb_cfg310006Error ID for Arb cfg hysteresis oor
err_ap_nvars10007Error ID for Autopilot nvars oor
err_apcfg_nvars10008Error ID for Autopilot cfg nvars oor
err_jetibox10009Error ID for sci identifier of Jetibox cfg oor
err_jetibox_fmsgcmd10010Error ID for jetibox fmsg cmd oor
err_arb_init_time10011Error ID for Arbiter Power Init Time less than 0
err_arb_varcfg10013Incorrect arbiter variable configuration
err_hs_base_can_id15000High speed telemetry invalid Base CAN Id
err_hs_tm_nvars15001High speed telemetry number of variables too big
err_vmc_motor20000Motor cfg is not valid
err_vmc_control_mode20001Control mode is invalid
err_vmc_encoder_nbits20002Number of bits for encoder is invalid
err_mc_vmotor20003Virtual motor cfg invalid
err_mc_smo20004Slide Mode Observer cfg invalid
err_mc_control20005Control cfg invalid
err_mc_fault_detection20006Invalid fault detection limits
err_mangle_rate20007Invalid filter time constant
err_low_pll20008Invalid cut-off frequency
err_mc_main20009Invalid real time frequency
err_range_check20010Invalid range definition
err_ext_sens20011Invalid external sensor configuration
err_press_dev20012Invalid pressure sensor configuration
err_press_dps31020014Invalid pressure sensor DPS310 configuration
err_press_hsc20015Invalid pressure sensor HSC configuration
err_press_ms5620016Invalid pressure sensor MS561101 configuration
err_invalid_cal_table20017Invalid number of entries in calibration table
err_mag_lis3mdl20018Invalid magnetometer LIS3MDL configuration
err_mag_hscdtd20019Invalid magnetometer HSCDTD008A configuration
err_mag_mmc5883ma20020Invalid magnetometer MMC5883MA configuration
err_mag_rm310020021Invalid magnetometer RM3100 configuration
err_ex_ussa76_cmd20022Invalid period of external USSA76 command
err_cfgmr_length31999Unexpected size of PDI or command
err_check_test65535Error 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)
2Num 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)

© 2025 Embention. All rights reserved.