Aircraft flight dynamics analysis and controller design using bifurcation tailoring

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Charles, Guy A ^a,b   Lowenberg, Mark H ^a,b   Stoten, David P ^a,b   Wang, Xiaofan ^a,b   di Bernardo, Mario ^a,b  

^a UNIVERSITY OF BRISTOL   (United Kingdom)

^b Dept of Mechanical Engineering ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BIFURCATION (MATHEMATICS); CONTROLLERS; FLIGHT DYNAMICS; SCHEDULING;

BIFURCATION DIAGRAM; CONTINUATION PARAMETERS; CONTROLLER DESIGNS; FEEDBACK STABILISATION; FLIGHT DYNAMICS MODEL; MINIMAL CONTROL SYNTHESIS; NUMERICAL CONTINUATION; UNIVERSITY OF BRISTOL;

MODEL REFERENCE ADAPTIVE CONTROL;

EID: 85087606080     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4751     Document Type: Conference Paper

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