Closed-form analytical solutions are found which relate various parameters in off-on control systems; relationship is shown among lead time, rise time, delay time, dwell time, and limit-cycle amplitude determined as functions of inertia, aerodynamic damping, and available control moment; application to boost-glide vehicles.


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    Title :

    Closed-loop flip-flop control systems


    Additional title:

    J Aerospace Sciences


    Contributors:
    Rogers, M. (author) / Shapiro, G. (author)

    Published in:

    Publication date :

    1960


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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