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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
