Robust control of angle of attack using dynamic inversion combined with quantitative feedback theory

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-12

  Antony Snell, S ^a   Stout, Perry W ^a  

^a Davis   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; DESIGN; DYNAMICS; FIGHTER AIRCRAFT; LINEAR CONTROL SYSTEMS; LINEARIZATION; ROBUST CONTROL; SUPERSONIC AIRCRAFT; TRACKING (POSITION); UNCERTAINTY ANALYSIS;

AIRCRAFT DYNAMICS; DYNAMIC INVERSION; FLIGHT CONTROL DESIGN; LINEAR CONTROL DESIGN; LINEAR DYNAMICS; MODEL UNCERTAINTIES; QUANTITATIVE FEEDBACK THEORY; ROBUST PERFORMANCE;

FEEDBACK;

EID: 84959170698     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

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