In this paper, the adaptive attitude tracking control of spacecraft with unknown time-varying disturbances is studied. Firstly, the attitude model is established using modified Rodriguez parameters, which is transformed into a high-order fully actuated (HOFA) system model with unknown time-varying parameters. Then, a novel adaptive attitude tracking control strategy based on the HOFA system approach is proposed. With the proposed control strategy, the unknown time-varying disturbances are estimated and compensated. The system stability of spacecraft attitude is guaranteed via Lyapunov theory. Finally, the effectiveness of the proposed control strategy is verified through numerical simulations.


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    Titel :

    Adaptive Attitude Tracking Control of Spacecraft Based on High-Order Fully Actuated System Approach


    Beteiligte:
    Jin, Dongyan (Autor:in) / Hou, Mingyu (Autor:in) / Wang, Tong (Autor:in) / Qiu, Jianbin (Autor:in)


    Erscheinungsdatum :

    10.05.2024


    Format / Umfang :

    1972608 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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