Gain-scheduled control of PVTOL aircraft dynamics with parameter-dependent disturbance

Journal of the Franklin Institute

Volumn 345, Issue 8, 2008, Pages 906-925

  Wu, Sun Li ^a   Chen, Pang Chia ^a   Hsu, Chih Hua ^b   Chang, Koan Yuh ^c  

^a KAO YUAN UNIVERSITY   (Taiwan)

^b CHANG JUNG CHRISTIAN UNIVERSITY   (Taiwan)

^c CHIENKUO TECHNOLOGY UNIVERSITY   (Taiwan)

Author keywords

Disturbance attenuation; LMI; LPV system; PVTOL aircraft

Indexed keywords

AIRCRAFT; DYNAMICS; EXTRACTIVE METALLURGY; GRAVITATION; GRAVITATIONAL EFFECTS; LINEAR CONTROL SYSTEMS; TRACKING (POSITION); UNMANNED VEHICLES; VTOL/STOL AIRCRAFT;

AIRCRAFT DYNAMICS; CONSTANT PARAMETERS; CONTROLLER DESIGNS; DISTURBANCE ATTENUATION; DISTURBANCE ATTENUATIONS; EXTERNAL DISTURBANCES; EXTERNAL-; GAIN-SCHEDULED CONTROLS; GRAVITY FORCES; LINEAR MATRIXES; LINEAR PARAMETER-VARYING SYSTEMS; LMI; LPV SYSTEM; MIXED OPTIMIZATIONS; PVTOL AIRCRAFT; RELATIVE STABILITIES; ROLL ANGLES; TIME RESPONSES; VARYING PARAMETERS; VERTICAL TAKEOFFS; YAW PLANES;

LINEAR MATRIX INEQUALITIES;

EID: 55349101597     PISSN: 00160032     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfranklin.2008.05.006     Document Type: Article

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