An attitude system is a system that determines the heading (heading) and attitude (pitch and pitch) of a vehicle (aircraft or spacecraft) and provides reference signals of heading and attitude to the automatic control system and navigation computer.
The general heading attitude reference system determines the true north direction and carrier attitude by measuring the earth's rotation vector and the local gravity vector based on the inertia principle, which is usually combined with the inertial navigation system. Recently, it has been developed into a space-based course attitude reference system for determining the course and attitude of the vehicle through Global navigation satellite System.
Post time: May-15-2023