AbstractPart I of this paper considered the development of a two-surface solar controller to stabilize the spacecraft along any arbitrary inertial orientation. In Part II, the capability of the controller is extended to achieve large-angle attitude maneuvers of the spacecraft. A sequential application of the control policies enables the controller to accomplish any desired change in the spacecraft attitude followed by its stabilization along the target orientation.


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    Title :

    Optimal solar pressure attitude control of spacecraft—II


    Subtitle :

    Large-angle attitude maneuvers


    Contributors:

    Published in:

    Acta Astronautica ; 9 , 9 ; 541-545


    Publication date :

    1982-03-09


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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