Application

Attitude and heading control system

The attitude and heading control system consists of two sets of heading and attitude systems. The full-pose combination gyro is used as the central gyroscope on the aircraft. It is a flight instrument that measures, displays and provides the aircraft’s heading and attitude angle signals. This system consists mainly of a full-view gyroscope, a magnetic induction sensor or an astronomical compass, and a full attitude indicator. It can indicate to the flight crew the heading angle required for navigation and the tilting angle and pitch angle required for driving. It can also provide a uniform heading angle for other airborne equipment such as autopilot, fire control system, radar antenna, aerial camera and so on. Attitude angle signal.

DTG

If you want to get more details about AHRS,pls visit https://www.ericcointernational.com/attitude-heading-reference-system/

 

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