Passive fault-Tolerant control design for near-space hypersonic vehicle dynamical system

Circuits, Systems, and Signal Processing

Volumn 31, Issue 2, 2012, Pages 565-581

  Gao, Zhifeng ^a   Jiang, Bin ^a   Shi, Peng ^b,c   Liu, Jianye ^a   Xu, Yufei ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

^b UNIVERSITY OF GLAMORGAN   (United Kingdom)

^c VICTORIA UNIVERSITY   (Australia)

Author keywords

Actuator faults; Near space hypersonic vehicle (NSHV); Parameter uncertainty; Passive fault Tolerant control (FTC)

Indexed keywords

ACTUATOR FAULT; ADMISSIBLE PARAMETERS; ASYMPTOTICALLY STABLE; DISTURBANCE ATTENUATION LEVELS; FAULT TOLERANT CONTROL; GAIN MATRICES; LINEAR MATRIX INEQUALITY (LMIS); NEAR-SPACE HYPERSONIC VEHICLE (NSHV); PARAMETER UNCERTAINTY; STANDARD SOFTWARE; VEHICLE DYNAMICAL SYSTEM;

CONTROL SYSTEM ANALYSIS; DYNAMICAL SYSTEMS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; LINEAR MATRIX INEQUALITIES;

FAULT TOLERANCE;

EID: 84860613619     PISSN: 0278081X     EISSN: 15315878     Source Type: Journal    
DOI: 10.1007/s00034-011-9385-7     Document Type: Article

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