Flight vehicle attitude control system is mainly constituted by the controller, sensors, actuators, and space vehicles. Attitude sensors are responsible for attitude information and angular velocity which are calculated through the attitude determination algorithm for solving the real attitude, and then generates control signals, resulting in control of torque acting on the flight vehicle to achieve the desired state. The structure of flight vehicle block diagram is shown in Fig.4.1.
The Descriptions of Flight Vehicle
Lect.Notes Control
2013-01-01
10 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
The Descriptions of Flight Vehicle
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