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    Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation

    94529.pdf (1.485Mb)
    Access Status
    Open access
    Authors
    Gao, X.
    He, D.
    Teo, Kok Lay
    Wang, J.
    Yang, H.
    Date
    2023
    Type
    Journal Article
    
    Metadata
    Show full item record
    Citation
    Gao, X. and He, D. and Teo, K.L. and Wang, J. and Yang, H. 2023. Discrete gain scheduling control approach to elliptical orbit rendezvous system with actuator saturation. International Journal of Robust and Nonlinear Control. 33 (3): pp. 2357-2374.
    Source Title
    International Journal of Robust and Nonlinear Control
    DOI
    10.1002/rnc.6509
    ISSN
    1049-8923
    Faculty
    Faculty of Science and Engineering
    School
    School of Elec Eng, Comp and Math Sci (EECMS)
    Funding and Sponsorship
    http://purl.org/au-research/grants/arc/DP190103361
    URI
    http://hdl.handle.net/20.500.11937/94745
    Collection
    • Curtin Research Publications
    Abstract

    This paper studies the discrete gain scheduling control design problem of elliptical orbit spacecraft rendezvous system with actuator saturation. Due to the presence of actuator saturation, the dynamic performance of the spacecraft rendezvous system degrades significantly. In order to improve the dynamic performance of the system, a discrete gain scheduling control approach is adopted to construct a group of time-invariant ellipsoidal invariant sets, which can be used to determine the switching points of the discrete gain scheduling control. By choosing some discrete parameter values, the discrete gain scheduling control is obtained from a solution of a periodic Riccati matrix differential equation. Under the control obtained, the dynamic performance of the system is much improved while accomplishing successfully the rendezvous mission of the spacecraft. Finally, a practical example is provided to show the effectiveness of the proposed control design approach.

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