• development and application of an integrated framework for small uav flight control development

    نویسندگان :
    جزئیات بیشتر مقاله
    • تاریخ ارائه: 1392/07/24
    • تاریخ انتشار در تی پی بین: 1392/07/24
    • تعداد بازدید: 911
    • تعداد پرسش و پاسخ ها: 0
    • شماره تماس دبیرخانه رویداد: -
      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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