Adaptive backstepping control for optimal descent with embedded autonomy

Li, Maodeng and Jing, Wuxing and Macdonald, Malcolm and McInnes, Colin (2011) Adaptive backstepping control for optimal descent with embedded autonomy. Aerospace Science and Technology, 15 (7). pp. 1396-1411. ISSN 1270-9638

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    Abstract

    Using Lyapunov stability theory, an adaptive backstepping controller is presented in this paper for optimal descent tracking. Unlike the traditional approach, the proposed control law can cope with input saturation and failure which enables the embedded autonomy of lander system. In addition, this control law can also restrain the unknown bounded terms (i.e., disturbance). To show the controller’s performance in the presence of input saturation, input failure and bounded external disturbance, simulation was carried out under a lunar landing scenario.

    Creators(s): Li, Maodeng, Jing, Wuxing, Macdonald, Malcolm ORCID logoORCID: https://orcid.org/0000-0003-4499-4281 and McInnes, Colin;
    Item type:Article
    ID code:28957
    Notes:Impact Factor 0.674, Half-Life 5.3
    Keywords:adaptive backstepping control , input failure , input saturation , optimal, Motor vehicles. Aeronautics. Astronautics, Mechanical engineering and machinery, Aerospace Engineering, Computational Mechanics, Control and Systems Engineering, Modelling and Simulation
    Subjects:Technology > Motor vehicles. Aeronautics. Astronautics
    Technology > Mechanical engineering and machinery
    Department:Faculty of Engineering > Mechanical and Aerospace Engineering
    Technology and Innovation Centre > Advanced Engineering and Manufacturing
    Depositing user: Pure Administrator
    Date deposited:14 Mar 2011 11:22
    Last modified:01 Jan 2021 09:39
    Related URLs:
    URI:https://strathprints.strath.ac.uk/id/eprint/28957
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