Full-envelope modular adaptive control of a fighter aircraft using orthogonal least squares

Journal of Guidance, Control, and Dynamics

Volumn 33, Issue 5, 2010, Pages 1461-1472

  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 Aerospace Software and Technologies Institute   (Netherlands)

^c Faculty ot Aerospace Engineering   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AIRCRAFT CONTROL; CONTINUOUS TIME SYSTEMS; CONTROL THEORY; DEGREES OF FREEDOM (MECHANICS); EQUATIONS OF MOTION; FLIGHT ENVELOPES; FREE FLIGHT;

CONTINUOUS TIME FORMULATIONS; ENTIRE FLIGHT ENVELOPE; LINEARIZED EQUATIONS; NON-LINEAR ADAPTIVE CONTROLS; NONLINEAR FLIGHT CONTROLLERS; ORTHOGONAL LEAST SQUARES; PARAMETER ESTIMATION ERRORS; SIX DEGREE-OF-FREEDOM;

SUPERSONIC AIRCRAFT;

EID: 78149315018     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.48175     Document Type: Article

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