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Volumn , Issue , 2007, Pages 1215-1220

Application of fault tolerant control using sliding modes with on-line control allocation on a large civil aircraft

Author keywords

[No Author keywords available]

Indexed keywords

CIVIL AIRCRAFTS; CONTROL ALLOCATION; FAULT TOLERANT CONTROL; ONLINE CONTROL;

EID: 43049164338     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/CCA.2007.4389401     Document Type: Conference Paper
Times cited : (9)

References (17)
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  • 4
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    • Simulator evaluation of simplified propulsion-only emergency flight control system on transport aircraft
    • Technical Report NASA/TM-1999-206578, NASA, 1999
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  • 8
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    • Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis
    • S. Ganguli, A. Marcos, and G.J. Balas. Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis. In American Control Conference, pages 3612-3617, 2002.
    • (2002) American Control Conference , pp. 3612-3617
    • Ganguli, S.1    Marcos, A.2    Balas, G.J.3
  • 9
    • 0005544728 scopus 로고
    • The simulation of a jumbo jet transport aircraft. Volume II: Modelling data
    • Technical Report CR-114494/D6-30643-VOL2, NASA and The Boeing Company
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    • (1970)
    • Hanke, C.1    Nordwall, D.2
  • 10
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    • Resolving actuator redundancy -optimal control vs. control allocation
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    • Harkegard, O.1    Glad, S.T.2
  • 11
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    • Fault tolerant flight control: An overview. GARTEUR action group 16: Fault tolerant control. draft for deliverable D1.1 (task T1.2)
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    • (2005)
    • Jones, C.N.1    Maciejowski, J.M.2
  • 12
    • 1842420807 scopus 로고    scopus 로고
    • A Boeing 747-100/200 aircraft fault tolerant and diagnostic benchmark
    • Technical Report AEM-UoM-2003-1, Department of Aerospace and Engineering Mechanics, University of Minnesota
    • A. Marcos and G.J. Balas, A Boeing 747-100/200 aircraft fault tolerant and diagnostic benchmark. Technical Report AEM-UoM-2003-1, Department of Aerospace and Engineering Mechanics, University of Minnesota, 2003.
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    • Marcos, A.1    Balas, G.J.2
  • 14
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    • Tailless aircraft flight control using multiple time scale re-configurable sliding modes
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    • Shtessel, Y.1    Buffington, J.2    Banda, S.3
  • 15
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    • Wells, S.R.1    Hess, R.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.