The present work investigates the short take-off flight performance and controller design of the STOVL unmanned aerial vehicle (UAV) with thrust vector control. Because of the STOVL UAV’s special dynamic characteristics during the short take-off process and its strict requirements regarding take-off attitude angle, the short take-off control scheme is determined by the calculation and analysis of short take-off and level flight performance. An improved eigenstructure assignment method is used in the STOVL UAV controller design. A nonlinear flight dynamic model with six degrees-of-freedom is established by wind tunnel experimental data and the controller is applied to the short take-off flight simulation of the STOVL UAV in order to verify the feasibility and effect of the control scheme.


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    Titel :

    A Research on the Short-Takeoff Performance and Flight Control of STOVL Aircraft


    Beteiligte:
    Chen, Kun (Autor:in) / Fu, Junquan (Autor:in) / Zhu, Jiachen (Autor:in)


    Erscheinungsdatum :

    2018-08-01


    Format / Umfang :

    163172 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch