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Volumn 14, Issue 5, 2012, Pages 1180-1193

Uncertainty modeling and robust minimax LQR control of multivariable nonlinear systems with application to hypersonic flight

Author keywords

feedback linearization; Nonlinear systems; robust control system design; uncertainty modeling

Indexed keywords

AIR; ALTITUDE CONTROL; CLOSED LOOP SYSTEMS; FEEDBACK LINEARIZATION; FLIGHT CONTROL SYSTEMS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; LINEAR CONTROL SYSTEMS; LONGITUDINAL CONTROL; MONTE CARLO METHODS; NONLINEAR SYSTEMS; ROBUST CONTROL; UNCERTAINTY ANALYSIS;

EID: 84866725717     PISSN: 15618625     EISSN: 19346093     Source Type: Journal    
DOI: 10.1002/asjc.399     Document Type: Article
Times cited : (49)

References (13)
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    • Adaptive feedback linearization control of a flexible spacecraft
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    • Adaptive sliding mode control design for a hypersonic flight vehicle
    • Xu, H., M. Mirmirani, and, P. A. Ioannou, " Adaptive sliding mode control design for a hypersonic flight vehicle," J. Guid. Control Dyn., Vol. 27, No. 5, pp. 829-838 (2004).
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    • Xu, H.1    Mirmirani, M.2    Ioannou, P.A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.