Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion


    Beteiligte:
    Tang, Peng (Autor:in) / Liu, Shuna (Autor:in) / Zheng, Chen (Autor:in)

    Kongress:

    International Conference on Guidance, Navigation and Control ; 2020 ; Tientsin



    Erscheinungsdatum :

    2022


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Design of Flight Control Law of Tilt-Rotor Aircraft Based on Incremental Nonlinear Dynamic Inversion

    Tang, Peng / Liu, Shuna / Zheng, Chen | British Library Conference Proceedings | 2022


    Adaptive Model Inversion Flight Control for Tilt-Rotor Aircraft

    Rolf T. Rysdyk / Anthony J. Calise | AIAA | 1999


    Adaptive Nonlinear Flight Control of STOL-Aircraft Based on Incremental Nonlinear Dynamic Inversion

    Beyer, Yannic / Kuzolap, Alexander / Steen, Meiko et al. | AIAA | 2018


    Incremental Nonlinear Dynamic Inversion and Control Allocation for a Tilt Rotor UAV (AIAA 2014-0963)

    Francesco, G. / D Amato, E. / Mattei, M. et al. | British Library Conference Proceedings | 2014