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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Descriptions of Flight Vehicle


    Additional title:

    Lect.Notes Control


    Contributors:
    Xia, Yuanqing (author) / Fu, Mengyin (author)


    Publication date :

    2013-01-01


    Size :

    10 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    The Descriptions of Flight Vehicle

    Xia, Yuanqing / Fu, Mengyin | Tema Archive | 2013




    Redundant Flight-Critical Control System Evaluation. Analog and Digital Systems Descriptions

    K. E. Andreasen / M. L. Beattie / J. H. Husband et al. | NTIS | 1974