A method for the design of attitude control systems for flexible spacecraft is presented. The design procedure employs input-output linearization and stabilization techniques; computation of the sampled-data control laws, and compensation techniques are applied to reduce the influence of the flexible part on the control system design. An idealized test vehicle subject to a variety of control laws was simulated. The improvements obtained by using a sampled-data scheme with an extended control are evident from the results of the simulations.


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    Title :

    Sampled Nonlinear Control for Large Angle Maneuvers of Flexible Spacecraft


    Contributors:
    S. Monaco (author) / D. N. Cyrot (author) / S. Stornelli (author)

    Publication date :

    1986


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Modeling and Control of a Flexible Spacecraft for Large-Angle Rapid Maneuvers

    Li, Y. / International Federation of Automatic Control | British Library Conference Proceedings | 1999