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    An optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique

    Access Status
    Fulltext not available
    Authors
    Gao, X.
    Teo, Kok Lay
    Duan, G.
    Date
    2013
    Type
    Journal Article
    
    Metadata
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    Citation
    Gao, Xiangyu and Teo, Kok Lay and Duan, Guang ren. 2013. An optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique. International Journal of Innovative Computing, Information and Control. 9 (5): pp. 2099-2110.
    Source Title
    International Journal of Innovative Computing, Information and Control
    ISSN
    1349-4198
    URI
    http://hdl.handle.net/20.500.11937/12266
    Collection
    • Curtin Research Publications
    Abstract

    In this paper, a new optimal robust control design approach is proposed for the task of spacecraft rendezvous such that both the stabilization and optimal performance are achieved. An approximate closed-form solution to the nonlinear optimal control problem is obtained by employing the θ-D technique, which is derived based on an approximate solution to the Hamilton-Jacobi-Bellman equation obtained via a perturbation technique. This approach provides a simple design procedure, and the feedback control law obtained is easy for on-board implementation. The effectiveness of the proposed approach is demonstrated through simulation studies.

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