A comparison of adaptive nonlinear control designs for an over-actuated fighter aircraft model

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  Van Oort, E R ^a,b   Sonneveldt, L ^a,b   Chu, Q P ^a,c   Mulder, J A ^a,c  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b ASTI   (Netherlands)

^c Faculty of Aerospace Engineering   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT MODELS; CONTROL SURFACES; CONTROL THEORY; DESIGN; FLIGHT CONTROL SYSTEMS; LEAST SQUARES APPROXIMATIONS; LYAPUNOV FUNCTIONS; PHILOSOPHICAL ASPECTS; QUADRATIC PROGRAMMING; SUPERSONIC AIRCRAFT;

ADAPTIVE CONTROL DESIGNS; ADAPTIVE FLIGHT CONTROLS; ADAPTIVE NONLINEAR CONTROL; CLOSED LOOP STABILITY; CONTROL LYAPUNOV FUNCTION; CONTROL SURFACE FAILURE; RECURSIVE LEAST SQUARES METHOD; SECOND-ORDER ACTUATOR DYNAMICS;

ADAPTIVE CONTROL SYSTEMS;

EID: 77957773767     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6786     Document Type: Conference Paper

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