This paper proposes a control framework using optimal prediction control allocation method (PM) and active disturbance rejection controller. First, the PM algorithm is adopted to extend the Attainable Moment Set compared with Pseudo-Inverse method (PI). By compensating the solution with null space vector, the saturation problem is solved while outputting the desired moments. Second, active disturbance rejection controller is adopted to observe and compensate the complex disturbance during the transition of tiltrotor aircraft. Numerical simulations demonstrate that PM can output optimal control allocation solution to generate larger moments under the same desired moments input compared with PI. The 6-DOF flight simulation shows that the overall control frame has better performance.


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    Titel :

    Optimal Prediction Control Allocation Algorithm for Tiltrotor Aircraft


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Wang, Yingxun (Autor:in) / Xuyang, TANG (Autor:in) / Zhihao, CAI (Autor:in) / Zhao, Jiang (Autor:in)


    Erscheinungsdatum :

    30.10.2021


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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    Optimal Prediction Control Allocation Algorithm for Tiltrotor Aircraft

    Wang, Yingxun / Xuyang, TANG / Zhihao, CAI et al. | TIBKAT | 2022


    CONTROL OF TILTROTOR AIRCRAFT

    Miller, M. / Narkiewicz, J. | British Library Online Contents | 2002


    TILTROTOR AIRCRAFT

    ROSS BRENT / GRONINGA KIRK / IVANS STEVEN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    CONTROL OF TILTROTOR AIRCRAFT

    Miller, M. / Narkiewicz, J. / Polskie Stowarzyszenie Wiroplatowe | British Library Conference Proceedings | 2002