Model reference adaptive switching control of a linearized hypersonic flight vehicle model with actuator saturation

Proceedings of the Institution of Mechanical Engineers. Part I: Journal of Systems and Control Engineering

Volumn 224, Issue 3, 2010, Pages 289-303

  Dong, C ^a   Hou, Y ^a   Zhang, Y ^a   Wang, Q ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Actuator saturation; Adaptive control; Hypersonic flight vehicles; Switched systems; Switching control

Indexed keywords

ACTUATOR SATURATIONS; ADAPTIVE CONTROL; HYPERSONIC FLIGHT VEHICLES; SWITCHED SYSTEM; SWITCHING CONTROL;

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AEROSPACE VEHICLES; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FUZZY CONTROL; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; INTERACTIVE COMPUTER SYSTEMS; LINEARIZATION; STIMULATED RAMAN SCATTERING; SWITCHING; SWITCHING SYSTEMS; VEHICLES;

MODEL REFERENCE ADAPTIVE CONTROL;

EID: 77952059611     PISSN: 09596518     EISSN: None     Source Type: Journal    
DOI: 10.1243/09596518JSCE829     Document Type: Article

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