In this paper the problem of maneuvering a flexible spacecraft through a large angle is considered, where the disturbance-accommodating feedback control tracks a desired output state. The desired output state is provided from an open-loop solution for the linear system model. The components of the disturbance vector are assumed to be represented in terms of Fourier series. Closed-form solutions are provided for the Ricati, prefilter, state trajectory, and residual state trajectory equations which define the optimal control. Example maneuvers are presented where control-rate penalties have been included in the performance index for frequency-shaping, in order to smooth both the open- and closed-loop control commands.


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    Titel :

    Disturbance-accommodating tracking maneuvers of flexible spacecraft


    Beteiligte:
    Turner, J. D. (Autor:in) / Juang, J.-N. (Autor:in) / Chun, H. M. (Autor:in)


    Erscheinungsdatum :

    1985-06-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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