HG2011AC03

Aircraft attitude computer

HG2011AC03 Description

Aircraft, embraer, model ERJ135 end item identification, external power source, attitude heading reference system m , uses digital ring-laser gyros and quartz accelerometers to keep track of changes in aircraft heading .

Features

Uses digital ring-laser gyros andquartz accelerometers to keep track ofchanges in aircraft heading and attitude

Properties of HG2011AC03

End Application:
Aircraft, embraer, model erj135 and erj145
Power Source:
External
Intelligence Input Method:
Electrical
Part Name Assigned By Controlling Agency:
Attitude heading reference syste m
NSN:
6605-01-500-0499
Description:
Computer,aircraft Attitude
Cage Code:
55939

Definition Aircraft Attitude Computer

A computer that contains the follow-up servo for pitch and roll information from the platform, and the circuitry for computing vertical attack angles, climb angle, vertical velocity, and ground speed to altitude ratio.

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Last modified 04/29/2024