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.
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