Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/111633
DC FieldValue
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
Appears in Collections:Staff Publications

Show simple item record
Files in This Item:
There are no files associated with this item.

Page view(s)

39
checked on May 2, 2021

Google ScholarTM

Check


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.