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    Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints

    Access Status
    Fulltext not available
    Authors
    Gao, X.
    Teo, Kok Lay
    Duan, G.
    Date
    2012
    Type
    Journal Article
    
    Metadata
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    Citation
    Gao, X. and Teo, K.L. and Duan, G. 2012. Non-fragile robust H[infinity] control for uncertain spacecraft rendezvous system with pole and input constraints. International Journal of Control. 85: pp. 933-941.
    Source Title
    International Journal of Control
    ISSN
    0020-7179
    School
    Department of Mathematics and Statistics
    URI
    http://hdl.handle.net/20.500.11937/49246
    Collection
    • Curtin Research Publications
    Abstract

    This article investigates the robust H1 control problem for a class of spacecraft rendezvous systems with parameter uncertainties and subject to input constraint, pole constraint and external and controllerperturbations. Based on the Lyapunov theory, a sufficient condition for the existence of the non-fragile robust state-feedback controller is given in terms of linear matrix inequalities (LMIs). Then, proper non-fragile controller design can be cast as a convex optimisation problem subject to LMI constraints. With the obtained controller, the spacecraft rendezvous mission can be accomplished. An illustrative example is provided to show the effectiveness of the proposed control design method.

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