AH-1000 Attitude and Heading Reference Systems (AHRS)
Overview
Our AH-1000 is a micro-electromechanical system (MEMS) attitude and heading reference system (AHRS) designed to serve as the attitude and heading reference system of choice for commercial aerospace primary or secondary attitude and heading systems.
The AH-1000 attitude and heading reference system was designed to provide unparalleled reliability and performance with significantly reduced size and weight compared to similar systems. This design allows the AH-1000 to provide the lowest total cost of ownership experience for an ARINC-705 AHRS.
The AH-1000 attitude and heading reference system was designed to provide unparalleled reliability and performance with significantly reduced size and weight compared to similar systems. This design allows the AH-1000 to provide the lowest total cost of ownership experience for an ARINC-705 AHRS.
Specifications
Key Differentiators
Certifications
- Environmental – DO-160F
- Hardware – DO-254 Level A
- Software – DO-178B Level A (maintenance Level D)
- Suitable for applications requiring Design Assurance Level (DAL) A
- TSO C3e, C4c, C5f, C6e (ETSO C3d, C4c, C5e, C6e)
Key Benefits
- ARINC-705 AHRS capability in a smaller and lighter form factor, significantly less than comparable systems, reduces operational costs
- Aircraft Personality Module (APM) stores aircraft-specific information, installation options, and calibration data
- Extraordinarily reliable with estimated >30,000 hour Mean Time Between Failure (MTBF)
- Full digital interface using proven Honeywell Aerospace MEMS technology
- Interfaces with Honeywell’s KMG7010 3-axis solid state magnetometer
- Most accurate attitude and heading MEMS AHRS available on the market, including TSO C5f for directional gyro mode
- Reduce operating costs with ARINC-705 AHRS capability in a significantly smaller and lighter form factor than comparable systems
Dimensions
Weight
- 3.2 lbs (1.45 kg)
Dimensions
- 2.5 x 5.0 x 7.8 in (97 cubic in)
- 63.5 x 127 x 198.12 mm (1598 cubic cm)
Performance Data
Alignments
- In-Air quick alignment of 5 seconds
- On-ground alignments of 15 seconds
Reliability
- >30,000 hour MTBF
Power
- 12W max @ 28 VDC (8W typical) Watt
Interface
- ARINC 429 and discrete I/O
- CAN bus (magnetometer)
- I2C (Aircraft Personality Module)
Heading Operational Modes
- Free drift directional gyro (DG) mode
- Heading slaved to magnetic sensor
Heading (Dynamic)
- 10.0 °/hr DG Mode (5°/hr typical DG mode)
- 2.0° magnetic mode
Cooling
- Passive
Connector
- Standard MIL-DTL-38999 Type III circular
Attitude Operational Modes
- Basic Mode without TAS aiding
- Normal Mode with TAS aiding
Attitude (Static)
- 0.5° normal mode
- 1.0° basic mode
Attitude (Dynamic)
- 1.0° normal mode
- 2.0° basic mode
