Mathematical model of bang-bang reaction jet attitude control system, capable of generating high moments in space vehicle, is derived on basis of conditional switching techniques; computer study of system was accomplished and its actual vs theoretical performance compared; study showed that model yields desired attitude change in minimum amount of time; parameter study was made to derive magnitude of moments, duty cycle, angular impulse, and dynamic response information.


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    Title :

    Bang-bang attitude control system for space vehicles


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Publication date :

    1962


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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