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Volumn 8, Issue 6, 2000, Pages 1010-1016

QFT-based robust/fault-tolerant flight control design for a remote pilotless vehicle

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; FAULT TOLERANT COMPUTER SYSTEMS; FEEDBACK CONTROL; FLIGHT DYNAMICS; FREQUENCY DOMAIN ANALYSIS; REMOTE CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TRACKING (POSITION); UNCERTAIN SYSTEMS;

EID: 0034317595     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.880607     Document Type: Article
Times cited : (25)

References (10)
  • 1
    • 0015386585 scopus 로고
    • Synthesis of feedback systems with large plant ignorance for prescribed time domain tolerance
    • I. M. Horowitz and M. Sidi, "Synthesis of feedback systems with large plant ignorance for prescribed time domain tolerance," Int. J. Contr., vol. 16, no. 2, pp. 287-309, 1972.
    • (1972) Int. J. Contr. , vol.16 , Issue.2 , pp. 287-309
    • Horowitz, I.M.1    Sidi, M.2
  • 2
    • 0029191478 scopus 로고    scopus 로고
    • QFT applied to fault tolerant flight control system design
    • June 1998
    • M. S. Keating, M. Pachter, and C. H. Houpis, "QFT applied to fault tolerant flight control system design," in ACC Proc., June 1998, pp. 184-188.
    • ACC Proc. , pp. 184-188
    • Keating, M.S.1    Pachter, M.2    Houpis, C.H.3
  • 3
    • 0029772257 scopus 로고    scopus 로고
    • Full envelope flight control system design using quantitative feedback theory
    • O. R. Reynolds, M. Pachter, and C. H. Houpis, "Full envelope flight control system design using quantitative feedback theory," J. Guidance, Contr., Dyn., vol. 19, no. 1, pp. 23-29, 1996.
    • (1996) J. Guidance, Contr., Dyn. , vol.19 , Issue.1 , pp. 23-29
    • Reynolds, O.R.1    Pachter, M.2    Houpis, C.H.3
  • 4
    • 0030241111 scopus 로고    scopus 로고
    • Quantitative feedback theory with a scheduled gain for full envelope longitudinal control
    • S. A. Snell and P. W. Stout, "Quantitative feedback theory with a scheduled gain for full envelope longitudinal control," J. Guidance, Contr. Dyn., vol. 19, no. 5, pp. 1095-1101, 1996.
    • (1996) J. Guidance, Contr. Dyn. , vol.19 , Issue.5 , pp. 1095-1101
    • Snell, S.A.1    Stout, P.W.2
  • 5
    • 0030242490 scopus 로고    scopus 로고
    • Development and flight testing of quantitative feedback theory pitch rate stability augmentation system
    • P. L. Fontenrose and C. E. Hall, "Development and flight testing of quantitative feedback theory pitch rate stability augmentation system," J. Guidance, Contr., Dyn., vol. 19, no. 5, pp. 1109-1115, 1996.
    • (1996) J. Guidance, Contr., Dyn. , vol.19 , Issue.5 , pp. 1109-1115
    • Fontenrose, P.L.1    Hall, C.E.2
  • 6
    • 0032108198 scopus 로고    scopus 로고
    • Introduction to quantitative feedback theory for lateral robust flight control system design
    • S.-F. Wu, M. J. Grimble, and S. G. Breslin, "Introduction to quantitative feedback theory for lateral robust flight control system design," IFAC J. Contr. Eng. Practice, vol. 6, no. 7, pp. 805-827, 1998.
    • (1998) IFAC J. Contr. Eng. Practice , vol.6 , Issue.7 , pp. 805-827
    • Wu, S.-F.1    Grimble, M.J.2    Breslin, S.G.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.