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.


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    Titel :

    The Descriptions of Flight Vehicle


    Weitere Titelangaben:

    Lect.Notes Control


    Beteiligte:
    Xia, Yuanqing (Autor:in) / Fu, Mengyin (Autor:in)


    Erscheinungsdatum :

    2013-01-01


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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