ARGO500

Super Attitude and Heading Reference System

S-AHRS/IMU for Navigation and Stabilization

The Argo 500 is the most modern solid-state Fiber Optic Gyros based Inertial Platform with an optimized SWaP-C (Size, Weight, Power and Cost) solution for next generation aircraft Fly By Wire (FBW) flight control.
From stabilization grade to gyrocompass and navigation grade ARGO500 represent a scalable solution for Navigation to Stabilization dual-use application from Urban Air Mobility and Helicopters to Fast Jets Aircraft.

Characteristics

ARGO 510 (S-AHRS gyrocompass)

ARGO 520 (AHRS/IMU)

True Heading (95%)

1

N.A.

Roll/Pitch (95%)

0.1

0.8

Position (95%)

1 nm/15min

N.A

Alignment time (data availability)

5 mins

30 sec

Alignment time (full accuracy)

Mag Sensor; TAS; GNSS (optional)

Mag Sensor; TAS

Aiding source

Mag Sensor; TAS; GNSS (optional)

Mag Sensor; TAS

System Characteristics

Interface

RS422/RS232

ARINC429

Ethernet

PPS

Data output rate

up to 500 Hz

Power requirements

28VDC (18-36VDC) < 15 W
(configuration dependent)

Environmental and Reliability

Operating Temperature

-40°C to +71°C

Not-operationg Temperature

-55°C to +85°C

Altitude

up to 50.000 ft

EMC/EMI

DO-160G

Vibration

sinusoidal 5-150 Hz

random 10-2000 Hz (DO-150G)

MTBF

> 25000 hours

Supply Voltage

18-36VDC

IMU ACCELEROMETERS

W x H x D

156 x 126 x 178

Weight

2.8 Kg

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