Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/83606
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dc.titleDesign and implementation of robust flight control system for a small-scale UAV helicopter
dc.contributor.authorCai, G.
dc.contributor.authorChen, B.M.
dc.contributor.authorLee, T.H.
dc.date.accessioned2014-10-07T04:43:07Z
dc.date.available2014-10-07T04:43:07Z
dc.date.issued2009
dc.identifier.citationCai, 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.
dc.identifier.isbn9788995605691
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/83606
dc.description.abstractThe 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.
dc.sourceScopus
dc.subjectControl applications
dc.subjectFlight control systems
dc.subjectRobust control
dc.subjectUnmanned aerial vehicle (UAV)
dc.typeConference Paper
dc.contributor.departmentELECTRICAL & COMPUTER ENGINEERING
dc.description.sourcetitleProceedings of 2009 7th Asian Control Conference, ASCC 2009
dc.description.page691-697
dc.identifier.isiutNOT_IN_WOS
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