The recently developed nonlinear servomechanism theory is applied to the attitude control of large maneuvering spacecraft subject to sinusoidal disturbances and parametric uncertainties.


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    Title :

    Spacecraft Attitude Control Using Nonlinear Servomechanism Theory


    Contributors:
    Huang, J. (author) / Lin, C. (author) / Hadaegh, F. Y. (author) / Chiang, R. Y. (author)

    Publication date :

    1994-04-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English