This paper exploits the control algorithm design of fuel-optimal satellite formation keeping strategy using linear programming approach. In the study, a fuel-optimal control problem is converted into a linear programming problem by means of an approximate discretization method. Furthermore, model predictive control approach is adopted to realize the fuel-optimal maneuver. At last, the designed control algorithm is applied to a satellite which maneuvers from an initial orbit to a passive and periodic relative orbit with minimal fuel consumption. Simulation results demonstrate the efficiency and rapidity of the proposed algorithm.


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    Title :

    Model predictive control of passive and periodic satellite formation based on linear programming approach


    Contributors:
    Xu, Guangyan (author) / Yu, Tingting (author) / Wang, Jianchao (author) / Chen, Xia (author)


    Publication date :

    2014-08-01


    Size :

    128713 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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