The controller design for reusable launch vehicles is challenging due to enormous amounts of model parameter uncertainties and atmospheric disturbances. This paper first derives six-degree-of-freedom model of a reusable launch vehicle with atmospheric disturbances. Next, four kinds of atmospheric disturbances are introduced and wind models are established respectively. For attitude control of the reusable launch vehicle, a nonsingular terminal sliding mode controller is designed with stability guaranteed. Finally, simulation results show a satisfactory performance for the attitude tracking of the reusable launch vehicle with atmospheric disturbances.


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    Title :

    Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances


    Contributors:
    You, Ming (author) / Zong, Qun (author) / Tian, Bailing (author) / Zeng, Fanlin (author)


    Publication date :

    2018-09-01


    Size :

    15 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    Reusable launch vehicle control in sliding modes

    Shtessel, Yuri / Tournes, Christian / Krupp, Don | AIAA | 1997


    Nonsingular and Fast Terminal Sliding Mode Control Method

    Li, S.-b. / Li, K.-q. / Wang, J.-q. et al. | British Library Online Contents | 2009