Spacecraft attitude control has a variety of requirements, which are mainly for attitude stabilization control and attitude maneuver control. Attitude stabilization control keeps the attitude of a spacecraft along a reference frame by overcoming the influence of the internal and external disturbance torque. Attitude maneuver control refers to the process of changing a spacecraft’s attitude from unknown to known or from one attitude to another; it may also refer to the tracking of the desired attitude. In addition to the attitude control of the spacecraft body, certain subsystems of the spacecraft must be controlled to complete a space mission, necessitating unified attitude control or the hierarchical control of the spacecraft.


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    Title :

    Spacecraft Attitude Control


    Additional title:

    Space Sci. Technol.


    Contributors:
    Xie, Yongchun (author) / Lei, Yongjun (author) / Guo, Jianxin (author) / Meng, Bin (author)


    Publication date :

    2021-07-14


    Size :

    108 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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