Robust nonlinear H_inf decoupling control of flight vehicle in hovering

Proceedings of the IEEE Conference on Decision and Control

Volumn 4, Issue , 2002, Pages 4486-4491

  Yang, Ciann Dong ^a   Kung, Chien Chung ^b  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

^b NATIONAL DEFENSE UNIVERSITY   (Taiwan)

Author keywords

Helicopter control; Hovering mode; Nonlinear H flight control

Indexed keywords

AERODYNAMIC LOADS; CONTROL SYSTEM SYNTHESIS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; GRAVITATION; HELICOPTERS; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); VELOCITY;

FLIGHT CONTROL; HELICOPTER CONTROL; HOVERING MODE;

NONLINEAR CONTROL SYSTEMS;

EID: 0036994209     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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