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    Robust H[infinity] control of spacecraft rendezvous on elliptical orbit

    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. Robust H[infinity] control of spacecraft rendezvous on elliptical orbit. Journal of the Franklin Institute. 349 (8): pp. 2515-2529.
    Source Title
    Journal of the Franklin Institute
    DOI
    10.1016/j.jfranklin.2012.08.005
    ISSN
    00160032
    School
    Department of Mathematics and Statistics
    URI
    http://hdl.handle.net/20.500.11937/37346
    Collection
    • Curtin Research Publications
    Abstract

    This paper investigates the robust H∞H∞ control problem of spacecraft rendezvous on elliptical orbit. Based on Lyapunov theory, a sufficient condition for the existence of the robust H∞H∞ controller is given in terms of the periodic Riccati differential equation (RDE). Then, a stabilizable controller design method based on a fast multi-shot algorithm is proposed. With the controller obtained, 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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