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Volumn 6, Issue 7, 1998, Pages 805-828

Introduction to quantitative feedback theory for lateral robust flight control systems design

Author keywords

Control design; Frequency domain; QFT; Robustness; Tracking

Indexed keywords

AIRCRAFT; FEEDBACK; FLIGHT DYNAMICS; FREQUENCY DOMAIN ANALYSIS; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY;

EID: 0032108198     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(98)00053-7     Document Type: Article
Times cited : (25)

References (21)
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    • Bossert, D.E.1
  • 6
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    • Robust flight control using quantitative feedback theory: Scalar system design
    • ICC/1/96, Industrial Control Centre, University of Strathclyde
    • Breslin, S.G., Grimble, M.J., 1996. Robust Flight Control using Quantitative Feedback Theory: Scalar System Design. Technical Report, ICC/1/96, Industrial Control Centre, University of Strathclyde.
    • (1996) Technical Report
    • Breslin, S.G.1    Grimble, M.J.2
  • 7
    • 85033894759 scopus 로고    scopus 로고
    • Robust flight control using quantitative feedback theory: Preliminary design studies
    • ICC/123/96, Industrial Control Centre, University of Strathclyde
    • Breslin, S.G., Grimble, M.J., 1996. Robust Flight Control using Quantitative Feedback Theory: Preliminary Design Studies. Technical Report, ICC/123/96, Industrial Control Centre, University of Strathclyde.
    • (1996) Technical Report
    • Breslin, S.G.1    Grimble, M.J.2
  • 10
    • 0030242490 scopus 로고    scopus 로고
    • Development and flight testing of quantitative feedback theory pitch rate stability augmentation system
    • Fontenrose, P.L., Hall, C.E., 1996. Development and Flight Testing of Quantitative Feedback Theory Pitch Rate Stability Augmentation System. J. Guidance, Control, and Dynamics, 19(5), pp. 1109-1115.
    • (1996) J. Guidance, Control, and Dynamics , vol.19 , Issue.5 , pp. 1109-1115
    • Fontenrose, P.L.1    Hall, C.E.2
  • 12
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    • Synthesis of feedback systems with nonlinear time uncertain plants to satisfy quantitative performance specifications
    • Horowitz, I.M., 1976. Synthesis of Feedback Systems with Nonlinear Time Uncertain Plants to Satisfy Quantitative Performance Specifications. IEEE Transactions on Automatic Control, 64, 123-130.
    • (1976) IEEE Transactions on Automatic Control , vol.64 , pp. 123-130
    • Horowitz, I.M.1
  • 14
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    • Synthesis of feedback systems with large plant ignorance for prescribed time domain tolerance
    • Horowitz, I.M., Sidi, M., 1972. Synthesis of Feedback Systems with Large Plant Ignorance for Prescribed Time Domain Tolerance. International Journal of Control 16(2), pp. 287-309.
    • (1972) International Journal of Control , vol.16 , Issue.2 , pp. 287-309
    • Horowitz, I.M.1    Sidi, M.2
  • 15
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    • Quantitative feedback theory (QFT): Technique for designing multivariabe control systems
    • AFWAL-TR-86-3107. Wright-Patterson Air Force Base, Ohio
    • Houpis, C.H., 1987. Quantitative Feedback Theory (QFT): Technique for Designing Multivariabe Control Systems. Air Force Wright Aeronautical Laboratories. AFWAL-TR-86-3107. Wright-Patterson Air Force Base, Ohio.
    • (1987) Air Force Wright Aeronautical Laboratories
    • Houpis, C.H.1
  • 18
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    • Full envelope flight control system design using quantitative feedback theory
    • Reynolds, O.R., Pachter, M., Houpis, C.H., 1996. Full Envelope Flight Control System Design Using Quantitative Feedback Theory. J Guidance, Control, and Dynamics 19(1), pp. 23-29.
    • (1996) J Guidance, Control, and Dynamics , vol.19 , Issue.1 , pp. 23-29
    • Reynolds, O.R.1    Pachter, M.2    Houpis, C.H.3
  • 19
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    • Quantitative feedback theory with a scheduled gain for full envelope longitudinal control
    • Snell, S.A., Stout, P.W., 1996. Quantitative Feedback Theory with a Scheduled Gain for Full Envelope Longitudinal Control, J. Guidance, Control, and Dynamics 19(5), pp. 1095-1101
    • (1996) J. Guidance, Control, and Dynamics , vol.19 , Issue.5 , pp. 1095-1101
    • Snell, S.A.1    Stout, P.W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.