Picture of product AHR50

Part #: AHR50

OEM:

Archangel

Desc:

Attitude Heading Reference System+

Part Number :

ArchangelLogo2.jpg

FEATURES

  • The AHR50 is a highly flexible inertial sensor system for cost-sensitive attitude and control functions
  • Functions as a bank and pitch instrument
  • With both integrated sensor suites and additional input capabilities, the AHR50 can function as an AHRS (Attitude Heading Reference System) or and embedded INS (Inertial Navigation System)
  • Archangel's AHR150A-2 MSU provides heading data for the AHR50, and it is fully qualified to DO-160E, DO-178B Level A, and TSO C6e
  • The AHR50 can also accept air data information via RS-232 and blend it with inertial measurements to enhance attitude estimates
  • Qualified for Mission Critical applications including IFR, SAR, primary flight systems, and UAS in the NAS
  • Complete set of support documents for embedding into larger systems
  • Certified for Part 23, 25, 27, and 29 aircraft
  • Mates with AHR150A-2 MSU
  • RS-232 input and output
  • Filtered micro DB9 connectors 

 

 

SPECIFICATIONS

dimension:

1.25” x 2.5” x 2.0” (H x W x D)

WEIGHT:

0.17 lbs

power: 8–24 VDC, 0.4 A @ 12 V nominal
inputs/outputs: RS-232 Out All inertial data RS-232 In Air data Output Data Rate 100 Hz (new message every 10 ms) RS-232 Baud Rate 115200 RS-485 Bi-directional MSU Interface
altitude: 1,500 to 52,000 ft pressure altitude
temperature:

-40°C to +70°C operating, -55°C to +125°C non-operating

rates: ±150°/second
pitch roll: ±1.0°, 3 σ
heading: ±2.0°, 3 σ
body rates 0.2% of input rate
ACCELERATION: ±10 g

 

CERTIFICATIONS

faa:

TSO C4c and C6e

catagories: XXXXFXXXXXXXXXXXXX
software catagories: DO-178B Level A
ENVIRONMENTAL: DO-160E [D2]XBBB[U2(FF1)]
 

 

 

 

Part Number: Description:
AHR50  Attitude Heading Reference System+


 

AHR50
- Attitude Heading Reference System+
Price Condition Status
REQUEST NEW OUTRIGHT REQUEST LEAD TIME

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