Aiming at improving the robustness of the Nonlinear Dynamic Inversion (NDI), a robust Adaptive Nonlinear Dynamic Inversion (ANDI) control strategy with a reference model structure is presented. In this method, the reference model and the adaptive law are introduced into NDI control structure to reduce the dependence on the knowledge of model and overcome the insufficient robustness of the NDI. Furthermore, the angular rates controller is verified under the change of center of gravity (CG). The simulation results showed the angular rates under this controller has excellent dynamic performance and overcome the change of CG.


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    Titel :

    Robust Flight Controller Design Based on Adaptive Nonlinear Dynamic Inverse with Reference Model


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Yu, Li (Autor:in) / Liu, Xiaoxiong (Autor:in) / Zhang, Weiguo (Autor:in) / Ruichen, Ming (Autor:in)


    Erscheinungsdatum :

    30.10.2021


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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