Nonlinear reconfiguring flight control based on online physical model identification

Journal of Guidance, Control, and Dynamics

Volumn 32, Issue 3, 2009, Pages 727-748

  Lombaerts, T J J ^a,b   Huisman, H O ^a,b   Chu, Q P ^a,b   Mulder, J A ^a,b   Joosten, D A ^a,c  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b Faculty ot Aerospace Engineering   (Netherlands)

^c DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; AIRCRAFT MODELS; DYNAMICS; FAILURE (MECHANICAL); FAULT TOLERANCE; FLIGHT SIMULATORS; FRACTURE MECHANICS; SAFETY ENGINEERING; STRUCTURAL INTEGRITY;

ADAPTIVE CONTROLLERS; ADAPTIVE NONLINEAR DYNAMIC INVERSIONS; FAILURE CONDITIONS; FAULT TOLERANT CONTROL; NONLINEAR DYNAMIC INVERSION; PHYSICAL MODEL IDENTIFICATION; RECONFIGURING CONTROLS; STRUCTURAL FAILURE MODE;

AIRCRAFT CONTROL;

EID: 67149123514     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.40788     Document Type: Article

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