PID and fuzzy logic pitch attitude hold systems for a fighter jet

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Bossert, David E ^a   Cohen, Kelly ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER CIRCUITS; CONTROLLERS; FLIGHT ENVELOPES; PROPORTIONAL CONTROL SYSTEMS; ROOT LOCI; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; THREE TERM CONTROL SYSTEMS;

CONVENTIONAL CONTROLLERS; DEGRADATION CONDITION; ENTIRE FLIGHT ENVELOPE; FAULT-TOLERANT CAPABILITY; FUZZY LOGIC CONTROLLERS; LONGITUDINAL STABILITY; OFF-DESIGN PERFORMANCE; ROOT LOCUS TECHNIQUE;

FUZZY LOGIC;

EID: 85085779339     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4646     Document Type: Conference Paper

References (18)

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