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    Fuel Minimizing Control for Constrained Relative Satellite Orbits

    155241_32669_Gao_Teo_Sun_Duan ICOCO.pdf (250.9Kb)
    Access Status
    Open access
    Authors
    Gao, X.
    Teo, Kok Lay
    Sun, Y.
    Duan, G.
    Date
    2010
    Type
    Conference Paper
    
    Metadata
    Show full item record
    Citation
    Gao, Xiangyu and Teo, Kok Lay and Sun, Yong and Duan, Guang-Ren. 2010. Fuel Minimizing Control for Constrained Relative Satellite Orbits, in Xu, H. and Yang, X. and Wei, W. (ed), the International Conference on Optimization and Control 2010, July 18 2010, pp. 149-157. Guiyang, China: Guiyang University.
    Source Title
    Proceedings of the International Conference on Optimization and Control 2010, Guiyang, China, July 18-23, 2010
    Source Conference
    the International Conference on Optimization and Control 2010, Guiyang, China, July 18-23, 2010
    School
    Department of Mathematics and Statistics
    URI
    http://hdl.handle.net/20.500.11937/28100
    Collection
    • Curtin Research Publications
    Abstract

    In this paper, we study the fuel minimization problem of hovering satellite subject to a practical constraint on the trajectory of the deputy satellite. It is first shown that the constraint condition can be expressed equivalently as maximum flight time inequalities. On this basis, a cost function relating to the fuel burn is formulated. A numerical procedure is developed to solve this fuel minimization problem.

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