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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    Titel :

    Bang-bang attitude control system for space vehicles


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1962


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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