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ARGO 500
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.
Argo 500 represents a scalable solution for Navigation to Stabilization dual-use applications from Urban Air Mobility and Helicopters to Fast Jets Aircraft.
Argo 500 represents a scalable solution for Navigation to Stabilization dual-use applications 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
SW/HW Compliance
DO-178C, DO-254
DO-178C, DO-254
System Characteristics
Interfaces
RS422/RS232
ARINC429
Ethernet
PPS
Data output rate
up to 500 Hz
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-160G)
MTBF
> 25000 hours
Dimensions
W x H x D
106 x 126 x 178
Weight
2.5 Kg
Power requirements
28VDC (18-36VDC) < 15 W(configuration dependent)
