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Volumn 20, Issue 5, 1997, Pages 933-940

Robust longitudinal control design using dynamic inversion and quantitative feedback theory

Author keywords

[No Author keywords available]

Indexed keywords

BANDWIDTH; CONTROL NONLINEARITIES; CONTROL SYSTEM SYNTHESIS; FEEDBACK; FLIGHT DYNAMICS; MATHEMATICAL MODELS; ROBUSTNESS (CONTROL SYSTEMS);

EID: 0031237430     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4137     Document Type: Article
Times cited : (42)

References (19)
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    • Reynolds, O.R.1    Pachter, M.2    Houpis, C.H.3
  • 9
    • 0019610451 scopus 로고
    • Improvement in Quantitative Nonlinear Feedback Design by Cancellation
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    • Horowitz, I.1
  • 10
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    • Quantitative Feedback Theory with a Scheduled Gain for Full Envelope Longitudinal Control
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    • Snell, S.A.1    Stout, P.W.2
  • 11
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    • Gain-Scheduling: Potential Hazards and Possible Remedies
    • Shamma, J. S., and Athans, M., "Gain-Scheduling: Potential Hazards and Possible Remedies," IEEE Control Systems Magazine, Vol. 12, No. 3, 1992, pp. 101-107.
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    • Shamma, J.S.1    Athans, M.2
  • 12
    • 0026897471 scopus 로고
    • Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft
    • Snell, S. A., Enns, D. F., and Garrard, W. L., "Nonlinear Inversion Flight Control for a Supermaneuverable Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp. 976-984.
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    • Snell, S.A.1    Enns, D.F.2    Garrard, W.L.3
  • 13
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    • Nonlinear Control Law with Application to High Angle-of-Attack Flight
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    • Bugajski, D.J.1    Enns, D.F.2
  • 14
    • 0003096706 scopus 로고
    • Dynamic Inversion: An Evolving Methodology for Flight Control Design
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    • (1994) International Journal of Control , vol.59 , Issue.1 , pp. 71-91
    • Enns, D.1    Bugajski, D.2    Hendrick, R.3    Stein, G.4
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.