In this paper, An adaptive dynamic inversion control scheme integrated with control allocation module is presented for an uncertain aircraft system. Through the online estimation for system uncertainties, the adaptive controller implements the basic system output tracking. Considering the deficiencies of the controller in rudders oversaturation and malfunction, a control allocation module based on quadratic programming algorithm is adopted to increase the use ratio of rudder loop and the reliability of the system. Simulation studies verify the effectiveness of the proposed approach.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Control allocation based adaptive dynamic inversion fault tolerant control scheme for an uncertain aircraft


    Beteiligte:
    Binwen Lu (Autor:in) / Jianjun Ma (Autor:in) / Zhiqiang Zheng (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    476120 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Fault-Tolerant Structured Adaptive Model Inversion Control

    Monish Tandale / John Valasek | AIAA | 2006


    Fault-Tolerant Fixed Allocation Control Scheme for Octorotor

    Ijaz, Salman / Chen, Fuyang / Li, Yuqing | British Library Conference Proceedings | 2022


    Fault tolerant control based on control allocation for morphing aircraft model

    Weilai, J. / Chaoyang, D. / Tong, W. et al. | British Library Online Contents | 2014


    Fault-Tolerant Fixed Allocation Control Scheme for Octorotor

    Ijaz, Salman / Chen, Fuyang / Li, Yuqing | Springer Verlag | 2021