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Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/111633
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dc.titleReliable aircraft tracking control via quadratic parameter-dependent Lyapunov functions: State feedback case
dc.contributor.authorLiao, F.
dc.contributor.authorWang, J.L.
dc.contributor.authorYang, G.H.
dc.date.accessioned2014-11-28T01:54:25Z
dc.date.available2014-11-28T01:54:25Z
dc.date.issued2002
dc.identifier.citationLiao, F.,Wang, J.L.,Yang, G.H. (2002). Reliable aircraft tracking control via quadratic parameter-dependent Lyapunov functions: State feedback case. Proceedings of the IEEE Conference on Decision and Control 4 : 4474-4479. ScholarBank@NUS Repository.
dc.identifier.issn01912216
dc.identifier.urihttp://scholarbank.nus.edu.sg/handle/10635/111633
dc.description.abstractThis paper investigates the reliable tracking problem against aircraft control surface impairment. New analysis and synthesis methods of reliable tracking control using quadratic parameter-dependent Lyapunov functions are provided in the term of solvability of Iterative Linear Matrix Inequalities (ILMIs). The proposed method has less conservativeness than that via the common (parameter-independent) Lyapunov function, which is demonstrated by an aircraft example.
dc.sourceScopus
dc.subjectH2
dc.subjectQuadratic parameter-dependent Lyapunov function
dc.subjectReliable control
dc.subjectTracking
dc.typeConference Paper
dc.contributor.departmentTEMASEK LABORATORIES
dc.description.sourcetitleProceedings of the IEEE Conference on Decision and Control
dc.description.volume4
dc.description.page4474-4479
dc.description.codenPCDCD
dc.identifier.isiutNOT_IN_WOS
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