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|Title:||Design and implementation of robust flight control system for a small-scale UAV helicopter||Authors:||Cai, G.
Flight control systems
Unmanned aerial vehicle (UAV)
|Issue Date:||2009||Citation:||Cai, G.,Chen, B.M.,Lee, T.H. (2009). Design and implementation of robust flight control system for a small-scale UAV helicopter. Proceedings of 2009 7th Asian Control Conference, ASCC 2009 : 691-697. ScholarBank@NUS Repository.||Abstract:||The primary focus of this work is to design and implement a robust automatic flight control system for a small-scale unmanned helicopter. A comprehensive nonlinear model for the unmanned system, which is constructed by our research team at the National University of Singapore, is first derived and presented. Based on its linearized model, a robust automatic flight control system is then designed by employing H∞ control and dynamic inversion techniques. Design specifications for military rotorcraft set for the US army aviation are adopted throughout the whole process to guarantee a top level performance. The result of actual flight tests shows our design is very successful. The unmanned helicopter system is capable of achieving a top level performance in accordance with the military standard in most of the categories under examination. ©2009 ACA.||Source Title:||Proceedings of 2009 7th Asian Control Conference, ASCC 2009||URI:||http://scholarbank.nus.edu.sg/handle/10635/83606||ISBN:||9788995605691|
|Appears in Collections:||Staff Publications|
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