This paper presents an integrated framework for small Unmanned Aerial Vehicle (UAV) flight control development. The approach provides a systematic procedure for flight control design process with a set of design tools that enables control engineers to rapidly synthesize, analyze and validate a candidate controller design. A model-based environment integrated with control synthesis, off-line and real-time simulation is developed for flight control synthesis, analysis and testings. The effectiveness of the proposed integrated framework is demonstrated by applying the framework approach to a small UAV testbed. Software-in-the-loop, processor-in-the-loop and flight testings are conducted with the synthesized controller implemented. Closed-loop performance and robustness results obtained are presented.


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    Titel :

    Development and application of an integrated framework for small UAV flight control development


    Beteiligte:
    Paw, Yew Chai (Autor:in) / Balas, Gary J. (Autor:in)

    Erschienen in:

    Mechatronics ; 21 , 5 ; 789-802


    Erscheinungsdatum :

    2011


    Format / Umfang :

    14 Seiten




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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