Reliable H2 static output-feedback tracking control against aircraft wing/control surface impairment

2003 International Conference Physics and Control, PhysCon 2003 - Proceedings

Volumn 1, Issue , 2003, Pages 112-117

  Liao, Fang ^a   Wang, Jian Liang ^a   Yang, Guang Hong ^b  

^a NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

^b NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

Aerospace control; Aircraft; Control systems; Ear; Iterative algorithms; Linear systems; Lyapunov method; Stability; System testing; Uncertain systems

Indexed keywords

AIRCRAFT; ALGORITHMS; CONTROL SURFACES; CONTROL SYSTEMS; CONVERGENCE OF NUMERICAL METHODS; FEEDBACK CONTROL; FLIGHT CONTROL SYSTEMS; ITERATIVE METHODS; LINEAR MATRIX INEQUALITIES; LINEAR SYSTEMS; LYAPUNOV FUNCTIONS; LYAPUNOV METHODS; MULTIOBJECTIVE OPTIMIZATION; NAVIGATION; SUPERSONIC AIRCRAFT; TRACKING (POSITION); UNCERTAIN SYSTEMS; WINGS;

AEROSPACE CONTROL; AFFINE PARAMETER-DEPENDENT LYAPUNOV FUNCTIONS; EAR; ITERATIVE ALGORITHM; ITERATIVE LINEAR MATRIX INEQUALITY; RELIABLE TRACKING CONTROL; STABILIZING CONTROLLERS; SYSTEM TESTING;

FIGHTER AIRCRAFT;

EID: 33645412412     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/PHYCON.2003.1236798     Document Type: Conference Paper

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