Linear parameter varying switching attitude control for a near space hypersonic vehicle with parametric uncertainties

International Journal of Systems Science

Volumn 46, Issue 16, 2015, Pages 3019-3031

  Huang, Yiqing ^a,b   Sun, Changyin ^b   Qian, Chengshan ^b   Wang, Li ^b  

^a ANHUI POLYTECHNIC UNIVERSITY   (China)

^b SOUTHEAST UNIVERSITY   (China)

Author keywords

Attitude control; Linear parameter varying; Near space hypersonic vehicle; Switching control

Indexed keywords

ATTITUDE CONTROL; FLIGHT ENVELOPES; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; LINEAR MATRIX INEQUALITIES; MATHEMATICAL TRANSFORMATIONS; ROBUSTNESS (CONTROL SYSTEMS); SWITCHING; TENSORS; VEHICLES;

ASYMPTOTICALLY STABLE; LINEAR PARAMETER VARYING; NEAR SPACE; PARAMETRIC UNCERTAINTIES; ROBUST STABILITY ANALYSIS; SWITCHING CONTROL; TENSOR PRODUCT MODELS; TRACKING PERFORMANCE;

CONTROLLERS;

EID: 84946494998     PISSN: 00207721     EISSN: 14645319     Source Type: Journal    
DOI: 10.1080/00207721.2014.886743     Document Type: Article

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