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Volumn 5, Issue , 2002, Pages 3631-3636

Enhanced NDI strategies for reconfigurable flight control

Author keywords

[No Author keywords available]

Indexed keywords

AVIATION; COMPUTER SYSTEM RECOVERY; FAULT TOLERANT COMPUTER SYSTEMS; FIGHTER AIRCRAFT; NONLINEAR CONTROL SYSTEMS; ONLINE SYSTEMS;

EID: 0036055812     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2002.1024492     Document Type: Conference Paper
Times cited : (37)

References (10)
  • 1
    • 0005595073 scopus 로고
    • Lockheed Martin Skunk works and lockheed Martin tactical aircraft systems: Application of multivariable control theory to aircraft control laws
    • Honeywell Technology Center; WL-TR-96-3099, Final Report for Mar.; Mar. 1996, May
    • (1993)
  • 3
    • 25044469239 scopus 로고    scopus 로고
    • Reconfigurable flight control using nonlinear dynamic inversion with a special accelerometer implementation
    • AIAA 2000-4565, AIAA Guidance, Navigation, and Control Conference, August 14-17
    • (2000)
    • Bacon, B.J.1    Ostroff, A.J.2
  • 5
    • 0003843406 scopus 로고    scopus 로고
    • Constrained control allocation for systems with redundant control effectors
    • PhD. Dissertation, Virginia Polytechnic Institute, Dec.
    • (1996)
    • Bordigon, K.1
  • 7
    • 0003975877 scopus 로고
    • Military standard flying qualities of piloted aircraft
    • MIL-STD-1797A, Jan. 30
    • (1990)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.