Direct adaptive reconfigurable control of a Tailless fighter aircraft

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 88-97

  Calise, A J ^a   Lee, S ^a   Sharma, M ^a  

^a AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AIRCRAFT CONTROL; PRODUCT DESIGN; SUPERSONIC AIRCRAFT;

AIRCRAFT CONFIGURATIONS; CONTROL ALLOCATION; DIRECT ADAPTIVE CONTROL; FLIGHT CONTROL DESIGN; LARGE-SCALE FAILURES; RECONFIGURABLE CONTROL; RECONFIGURABLE FLIGHT CONTROL; REDUNDANT CONTROLS;

QUALITY CONTROL;

EID: 84959136266     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4108     Document Type: Conference Paper

References (9)

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3. Monaco, J., Ward, D., Barron, R. and Bird, R., "Implementation and Flight Test Assessment of an Adaptive Reconfigurable Flight Control System", AIAA-97-3738, Guidance, Navigation and Control Conference, August 1997.
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6. Brinker, J. S., Wise, K. A., "Reconfigurable/Damage Adaptive Flight Control for Tailless Fighter Aircraft", Guidance, Navigation, and Control Conference, AIAA-98-4107, 1998.
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9. McFarland, M., Calise, A., "Multilayer Neural Networks and Adaptive Nonlinear Control of Agile Anti-Air Missiles", Guidance, Navigation, and Control Conference, AIAA-97-3540.