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Volumn 105, Issue 1051, 2001, Pages 525-533

Integrated sensor/actuator FDI and reconfigurable control for fault-tolerant flight control system design

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; ALGORITHMS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DECISION THEORY; FAULT TOLERANT COMPUTER SYSTEMS; FLIGHT DYNAMICS; KALMAN FILTERING; SYSTEMS ANALYSIS;

EID: 10844236595     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/s0001924000017966     Document Type: Article
Times cited : (27)

References (11)
  • 5
    • 0024143651 scopus 로고
    • Detection, identification and estimation of surface damage/actuator failure for high performance aircraft
    • Atlanta USA
    • CAGLAYAN, A.K., RAHNAMAI, K. and ALLEN, S.M. Detection, identification and estimation of surface damage/actuator failure for high performance aircraft. Proceedings of the American Control Conference (ACC), Atlanta USA, 1988, pp 2206-2212.
    • (1988) Proceedings of the American Control Conference (ACC) , pp. 2206-2212
    • Caglayan, A.K.1    Rahnamai, K.2    Allen, S.M.3
  • 6
    • 0040294933 scopus 로고
    • Surface failure detection and evaluation of control law for reconfiguration of flight control system
    • Boston MA
    • IOANNOU, P. and ROONEY, R. Surface failure detection and evaluation of control law for reconfiguration of flight control system, Proceedings AIAA Guidance and Navigation Control Congress, Boston MA, 1989, pp 733-740.
    • (1989) Proceedings AIAA Guidance and Navigation Control Congress , pp. 733-740
    • Ioannou, P.1    Rooney, R.2
  • 8
    • 85003272687 scopus 로고
    • New technique for aircraft flight control reconfiguration
    • NAPOLITANO, M.R. and SWAIM, R.L. New technique for aircraft flight control reconfiguration, J Guid Con and Dyn, 1991, 14, (1), pp 184-190.
    • (1991) J Guid Con and Dyn , vol.14 , Issue.1 , pp. 184-190
    • Napolitano, M.R.1    Swaim, R.L.2
  • 10
    • 0032273920 scopus 로고    scopus 로고
    • Failure detection and identification and fault tolerant control using the IMM-KF with applications to the Eagle-Eye UAV
    • Tampa, Florida, USA, December
    • RAGO, C., PRASANTH, R., MEHRA, R.K. and FORTENBAUGH, R. Failure detection and identification and fault tolerant control using the IMM-KF with applications to the Eagle-Eye UAV, Proceedings of 37th IEEE Conference on Decision and Control, Tampa, Florida, USA, December, 1998, pp 4208-4213.
    • (1998) Proceedings of 37th IEEE Conference on Decision and Control , pp. 4208-4213
    • Rago, C.1    Prasanth, R.2    Mehra, R.K.3    Fortenbaugh, R.4
  • 11
    • 0015126334 scopus 로고
    • An innovations approach to fault detection and diagnosis in dynamic systems
    • MEHRA, R.K. and PESCHON, J. An innovations approach to fault detection and diagnosis in dynamic systems, Automatica, 1971, 7, pp 637-640.
    • (1971) Automatica , vol.7 , pp. 637-640
    • Mehra, R.K.1    Peschon, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.