Output feedback variable structure adaptive control of an aeroelastic system

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 6, 1998, Pages 830-837

  Zeng, Yueming ^a,c   Singh, Sahjendra N ^a,b  

^a University of Nevada Las Vegas   (United States)

^b AIAA   (United States)

^c HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; MATHEMATICAL MODELS; TRAJECTORIES;

AAEROELASTIC SYSTEMS; TRAJECTORY CONTROL;

ADAPTIVE CONTROL SYSTEMS;

EID: 0032206717     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4342     Document Type: Article

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