Technical

Features

  • Communications

    • 2 x isolated CAN buses

    • 1 x RS 232 bus

    • 1 x I2C bus

    • 1 x USB port

    • 1 x RS 485 full duplex bus

    • 1 x UART bus

    • Over USB, RS 485 or RS 232 firmware update

    • 1 x 3G module

  • Input / Output

    • 16 x configurable input / output signals

    • 5 x analog input signals 0 - 3.3 V

    • 1 x EQEP bus

  • Power

    • 6.5 - 36 V DC required for input power supply

    • 1 x output power with 3.3 V, up to 100 mA

    • 1 x output power with 5 V, up to 100 mA

  • Protection

    • EMI shield

    • Against inrush current for connecting power supply

Note

The number of communication ports and signals can be increased with Veronte CEX or Veronte MEX.

Variants

The Veronte Autopilot 1x has 3 variants:

  • W/O DAA

  • With Remote ID

  • With ADS-B

Sensor Specifications

Accelerometers (3 axis each one)

Specification

IMU 1

IMU 2

IMU 3

Range

16 g

24 g

8 g

Maximum shock

20,000 g for 0.2 ms

10,000 g/ms

14,700 \(m/sec^2\)

Sensitivity

16,393 LSB/(\(m/sec^2\))

10,920 LSB/(\(m/sec^2\))

26,756,268 LSB/(\(m/sec^2\))

Update Time

1 ms

Error

3 mg (RMS noise)

190 Z axis 160 X & Y axis \(\mu g/ \sqrt{Hz}\) (noise density)

0.000167 X & Y axis 0.000243 Z axis \(m/sec^2 / \sqrt{Hz}\) (noise density)

Offset

0 mg

± 20 mg

0.0196 \(m/sec^2\)

Gyroscopes (3 axis each one)

Specification

IMU 1

IMU 2

IMU 3

Range

125 to 2,000 °/sec

125 to 2,000 °/sec

2,000 °/sec

Sensitivity

228 to 14.2 LSB/°/sec

262 to 16 LSB/°/sec

655,360 to 10 LSB/°/sec

Update Time

1 ms

RMS noise

0.075 °/sec

0.1 °/sec

0.152 °/sec

Offset

0 °/sec

±1 °/sec

0.14 X & Z axis 1.4 Y axis °/sec

Magnetometers

Specification

Magnetometer 0

Magnetometer 1

Magnetometer 2

Range

4 G

8 G

11 G

Sensitivity

6,842 to 1,711 LSB/G

4,096 LSB/G

0.13 mG

Update Time

8.3 ms

12.5 ms

RMS noise

3.2 X & Y axis 4.1 Z axis mG

0.4 mG

0.3 mG

Offset

0 G

0 G

0 G

Static pressure

Specification

Sensor 1 (INT port)

Sensor 2 (STATIC port)

Range

1,000 - 120,000 Pa

30,000 - 120,000 Pa

Band Error

500 Pa

200 Pa

Resolution

1.2 to 6.5 Pa

0.5 Pa

Update Time

20 ms

31.3 ms

RMS noise

6.5 Pa

0.35 Pa

Dynamic pressure sensor

Specification

Pitot

Range

3 Pa (5 kt 8 km/h sea level) to 6,900 Pa (206 kt 382 km/h sea level)

Band Error

140 Pa

Resolution

25,500 Pa

Update Time

20 ms

Bias

±7 Pa

GNSS receivers

Specification

GNSS 1 & GNSS 2

Constellations

BeiDou, Galileo, GLONASS, GPS / QZSS

Concurrent GNSS

4

Bands

L2OF, L2C, E1B/C, B2I, E5b, L1C/A, L1OF, B1I

Position accuracy RTK

0.01 m + 1 ppm CEP

Update rate RTK

Up to 20 Hz

Anti-jamming

Active CW detection and removal Onboard band pass filter

Anti-spoofing

Advanced anti-spoofing algorithms

Advanced Functions

  • Moving base capable

  • GNSS based attitude estimation

Update time

250 ms

Location Accuracy

Vertical

0.01 m

Horizontal

SBAS

1 m

RTK

0.01 m

Velocity Accuracy

0.05 m/s

Temperature

Device

Resolution

Bias

IMU 1

256 LSB/°C (16 bit)

15°C

IMU 2

8 LSB/°C

1°C

IMU 3

10 LSB/°C

5°C

MPU

-

15°C

Magnetometer 0

8 LSB/°C

-

Magnetometer 1

1.25 LSB/°C

-

Static pressure 1

0.01 °C

-

Static pressure 2

0.01 °C

-

Note

An external pressure sensor is required to measure below -20 °C

Internal Radio

RF baudrate

250 kbps

LOS range

Up to 3200 m

Transmission power

19 dBm

Receiver sensitivity

-103 dBm

Frequency band

ISM 2.4 GHz

Mechanical and Electrical Specifications

Variable

Value

Weight

W/O DAA variant: 198 g.

With Remote ID or ADS-B: 210 g.

Temperature range

-40 to 65 ºC.

Protection rating

IP67.

Maximum acceleration

32 g.

Voltage input

6.5 V to 36 V.

Power consumption

2.2 W in maintenance mode.

2.2 W in normal mode with CPU at 98 %, internal radio off and 3G module off.

2.6 W in normal mode with CPU at 98 %, internal radio on and 3G module on.

Dimensions

Aircraf Mounting - Veronte dimensions

Veronte Autopilot 1x dimensions

M3 screws are recommended for mounting. In saline environments such as coastal and oceanic, the screw material must be stainless steel.

Interfaces

Connector Layout

Aircraf Mounting - Connectors

Connectors

Index

Connector

1

LOS SSMA connector

2

GNSS1 SSMA connector

3

Static pressure port (Int. D. 2.5 mm x Out. D. 4 mm) for static pressure sensor 1

4

Static pressure port (Int. D. 2.5 mm x Out. D. 4 mm) for static pressure sensor 2

5

Dynamic pressure port (Int. D. 2.5 mm x Out. D. 4 mm)

6

ADS-B or remote ID SSMA connector

Warning

When using ADS-B or remote ID, there must be an adequate antenna or load connection to the DAA SMA

7

GNSS2 SSMA connector

8

M2M SSMA connector

Warning

If the SARA (3G) module is enabled, a suitable antenna must be connected to this SSMA port. The 4G Antenna with the Embention reference P000112 is recommended

9

68-pin connector

Both static pressure ports must be used for sensor redundancy (Y tubing connection is strongly recommended).

Warning

The static pressure port 4 is always used by Autopilot 1x to calculate speed (using the difference of pressure between ports 4 and 5), no matter which sensor is selected in configuration.

Mating Connectors

Index

Autopilot 1x Connector

Mating Connector

1

RF antenna (SSMA Jack Female)

SSMA male Plug, low-loss cable is recommended.

2, 7

GNSS antenna (SSMA Jack Female)

SSMA male Plug, low-loss cable is recommended.

Active Antenna GNSS:

  • Gain min 15dB (to compensate signal loss in RF Cable)

  • Gain max 50 dB

  • Maximum noise figure 1.5dB

  • Power supply 3.3V

  • Max current 20 mA

8

M2M antenna (SSMA Jack Female)

SSMA male Plug, low-loss cable is recommended.

6

ADS-B or remote ID (SSMA Jack Female)

SSMA male Plug, low-loss cable is recommended.

9

Connector HEW.LM.368.XLNP

Mating connector: FGW.LM.368.XLCT (Embention reference P005688). Mating harnesses with 1.8 m length cable is available on demand with the Embention reference P001114 and P007043