AH-2100 Super Attitude Heading Reference System (AHRS)
Overview
The AH-2100 Super Attitude Heading Reference System (AHRS) improves accuracy, provides greater safety and accommodates future growth as the communication, navigation, surveillance environment evolves. It is designed for growth and to be interchangeable with the LASEREF V Micro inertial reference system (IRS) and can be easily upgraded. You can reduce maintenance cost with 25,000 operating hours predicted reliability and eliminate the flux valve and compass calibration procedures.
Additional features include:
Additional features include:
- Automatic mode control eliminates the AHRS control panel, reducing pilot workload
- Immune to local magnetic disturbances, solar storms and lightning
- High accuracy heading and attitude information improves weather radar, enhanced ground proximity warning system (EGPWS), satellite communication, broadband datalink, displays and autopilot performance
- Dynamic performance - 20 times better than other AHRS equipment
- Eliminates low frequency wing rock
- Eliminates external aiding sources (traffic advisory system, magnetic sensor, global positioning system) allowing greater dispatch performance
- Built-in self-test with 99 percent coverage
- Passive cooling system eliminates weight and cost of cooling fans and ARINC mounting trays
Specifications
Key Differentiators
- Certifications
- DO-178B Level A, DO-254 Level A (HG2112)
- DO-178B Level A, DO-254 Level A (HG2113)
- TSO C201 and C196b (HG2113)
- TSO C3e, C4c, C5f, C6e (HG2112)
Dimensions
- Weight
- AHRU: 9.30 lbs (4.2Kg) (HG2113)
- AHRU: 9.30 lbs (4.2Kg) (HG2112)
- APM: 3.20 ounce (90.7g) (HG2113)
- APM: 3.20 ounce (90.7g) (HG2112)
- Tray: 0.550 lbs (249.48g) (HG2113)
- Tray: 0.550 lbs (249.48g) (HG2112)
Performance Data
- Altitude (hybrid)
- 150 feet (HG2113)
- True Heading (hybrid)
- 0.6 degrees (HG2113)
- True Heading
- 0.6 degrees (HG2112)
- 0.6 degrees (HG2113)
- Size
- 6.450 in x 6.540 in x 6.300 in (L,W,H) (Maximum) (HG2113) millimetre
- 6.450 in x6.540 in x 6.300 in (L,W,H) (Maximum) HG2112) millimetre
- Reliability
- Demonstrated >50000 Flight Hrs (HG2112)
- Demonstrated >50000 Flight Hrs (HG2113)
- Power
- 20 W Typical (HG2112) Watt
- 20 W Typical (HG2113) Watt
- Position (hybrid)
- 25 Meters (HG2113)
- Position
- 2 nm / 15 minutes R95 (HG2113)
- 40 nm R95 upto 18 Hrs (HG2113)
- Pitch / Roll Angle
- 0.14 degrees (HG2112)
- 0.14 degrees (HG2113)
- Interface
- 2 RS-422 GPS Receiver Time mark inputs (HG2112)
- 2 RS-422 GPS Receiver Time mark inputs (HG2113)
- 4 ARINC 429 Outputs (HG2112)
- 4 ARINC 429 Outputs (HG2113)
- 7 ARINC 429 Inputs (GPS, ADR,FMS) (HG2112)
- 7 ARINC 429 Inputs (GPS, ADR,FMS) (HG2113)
- Ground Speed
- 14 knots R95 (HG2113)
- 18 knots R95, Flight duration <12 hours (HG2112)
- Cooling
- Passive Cooling
- Coasting Performance (Integrity)
- 0.1 nm 100% availability (HG2113)
- DO-316 Appendix R; RNP AR (HG2113)
- Coasting Performance (95%)
- 10 Minutes 525 ft (160 meters) (HG2113)
- 20 Minutes 1607.7 ft (490 meters) (HG2113)
- 30 Minutes 3018.5 ft(920 meters) (HG2113)
- 60 Minutes 5905.8 ft (1800 meters) (HG2113)
- Time for loss Satellites (HG2113)
- Body Accelerations
- 0.005 Gs or 0.5% of output, whichever is greater (HG2112)
- 0.005 Gs or 0.5% of output, whichever is greater (HG2113)
- Attitude Rates
- 0.02 deg/sec or 0.5% of output, whichever is greater (HG2112)
- 0.02 deg/sec or 0.5% of output, whichever is greater (HG2113)
