Development and application of an integrated framework for small UAV flight control development
Development and application of an integrated framework for small UAV flight control development
- New search for: Paw, Yew Chai
- New search for: Balas, Gary J.
- New search for: Paw, Yew Chai
- New search for: Balas, Gary J.
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.
Document information
Development and application of an integrated framework for small UAV flight control development
Mechatronics ; 21 , 5 ; 789-802
2011
14 Seiten
Article (Journal)
English
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