Investigated are the dynamics and control of high-order dynamical systems as used in flexible spacecraft. The procedure adopted is referred to as modal-space control and consists of a scheme for independent control of spacecraft modes. The basic idea behind this method is that the control laws are first designed in the modal-space for each independent set in a way that the response of one pair of modes does not effect those of any other pair. The approach makes a design of nonlinear on-off control laws as well as proportional control of high-order system possible. (de Posamentier)


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    Title :

    Dynamics and control in modal-space of flexible spacecraft


    Additional title:

    Dynamik und Steuerung komplexer Systeme in flexiblen Raumfahrzeugen


    Contributors:
    Oz, H. (author)

    Publication date :

    1979


    Size :

    191 Seiten


    Type of media :

    Theses


    Type of material :

    Print


    Language :

    English




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