Flight control reconfiguration based on online physical model identification and nonlinear dynamic inversion

AIAA Guidance, Navigation and Control Conference and Exhibit

Volumn , Issue , 2008, Pages

  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 of Aerospace Engineering   (Netherlands)

^c DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; AIRCRAFT MODELS; DYNAMICS; FAULT TOLERANCE; FLIGHT SIMULATORS; FRACTURE MECHANICS; NONDESTRUCTIVE EXAMINATION; SAFETY ENGINEERING; STRUCTURAL INTEGRITY;

ADAPTIVE CONTROLLERS; FAILURE HANDLING; FAULT TOLERANT CONTROL; NONLINEAR DYNAMIC INVERSION; PHYSICAL MODEL IDENTIFICATION; RECONFIGURING CONTROLS; SIMULATION MODEL; STRUCTURAL FAILURE;

FAILURE (MECHANICAL);

EID: 77953753553     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-7435     Document Type: Conference Paper

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