Nonlinear adaptive trajectory control applied to an F-16 model

Journal of Guidance, Control, and Dynamics

Volumn 32, Issue 1, 2009, Pages 25-39

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

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b Aerospace Software and Technology Institute   (Netherlands)

^c Faculty ot Aerospace Engineering   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT MODELS; CONTROL SURFACES; CONTROL THEORY; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES; FLIGHT SIMULATORS; LYAPUNOV FUNCTIONS; NEURAL NETWORKS; TRAJECTORIES; UNCERTAINTY ANALYSIS;

ADAPTIVE TRAJECTORY; B-SPLINE NEURAL NETWORK; CLOSED LOOP STABILITY; CONTROL LYAPUNOV FUNCTION; NON-LINEAR AIRCRAFT MODELS; PARAMETER ESTIMATION PROCESS; STATE AND INPUT CONSTRAINTS; UNCERTAIN PARAMETERS;

SUPERSONIC AIRCRAFT;

EID: 60349092490     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.38785     Document Type: Conference Paper

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