Design of a flight control system for a highly maneuverable aircraft using robust dynamic

Guidance, Navigation, and Control Conference, 1994

Volumn , Issue , 1994, Pages 1270-1280

  Reiner, Jacob ^a   Balas, Gary J ^b   Garrard, William L ^b  

^a RAFAEL   (Israel)

^b UNIVERSITY OF MINNESOTA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; AIRCRAFT CONTROL; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; DESIGN; FLIGHT CONTROL SYSTEMS; LINEAR CONTROL SYSTEMS; LONGITUDINAL CONTROL; ROBUST CONTROL; ROBUSTNESS (CONTROL SYSTEMS);

AIRCRAFT RESPONSE; DYNAMIC INVERSION; FLIGHT CONTROLLERS; HIGH PERFORMANCE AIRCRAFTS; LINEAR CONTROLLERS; OUTER-LOOP CONTROLLER; RANGE OF ANGLES OF ATTACK; STRUCTURED SINGULAR VALUES;

CONTROLLERS;

EID: 84999274232     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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