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Volumn 19, Issue 5, 1996, Pages 1095-1101

Quantitative feedback theory with a scheduled gain for full envelope longitudinal control

Author keywords

[No Author keywords available]

Indexed keywords

DYNAMICS; FEEDBACK; FIGHTER AIRCRAFT; INVARIANCE; MATHEMATICAL MODELS; OSCILLATIONS; ROBUSTNESS (CONTROL SYSTEMS);

EID: 0030241111     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21750     Document Type: Article
Times cited : (12)

References (17)
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  • 3
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  • 4
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    • 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. 3, 1992, pp. 976-984.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.3 , pp. 976-984
    • Snell, S.A.1    Enns, D.F.2    Garrard, W.L.3
  • 5
    • 0026856998 scopus 로고
    • Nonlinear Control Law with Application to High Angle-of-Attack Flight
    • Bugajski, D. J., and Enns, D. F., "Nonlinear Control Law with Application to High Angle-of-Attack Flight," Journal of Guidance, Control, and Dynamics, Vol. 15, No. 3, 1992, pp. 761-767.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.3 , pp. 761-767
    • Bugajski, D.J.1    Enns, D.F.2
  • 6
    • 0003093484 scopus 로고
    • Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws
    • (Hilton Head, SC), AIAA, Washington, DC, (AIAA Paper 92-4330)
    • Snell, S. A., "Preliminary Assessment of the Robustness of Dynamic Inversion Based Flight Control Laws," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Hilton Head, SC), AIAA, Washington, DC, 1992 (AIAA Paper 92-4330).
    • (1992) Proceedings of the AIAA Guidance, Navigation, and Control Conference
    • Snell, S.A.1
  • 7
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    • Robust, Nonlinear, High Angle-of-Attack Control Design for a Supermaneuverable Vehicle
    • (Monterey, CA), AIAA, Washington, DC, (AIAA Paper 93-3774)
    • Buffington, J. M., Adams, R. J., and Banda, S. S., "Robust, Nonlinear, High Angle-of-Attack Control Design for a Supermaneuverable Vehicle," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Monterey, CA), AIAA, Washington, DC, 1993 (AIAA Paper 93-3774).
    • (1993) Proceedings of the AIAA Guidance, Navigation, and Control Conference
    • Buffington, J.M.1    Adams, R.J.2    Banda, S.S.3
  • 8
    • 0029210924 scopus 로고
    • Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft
    • Reiner, J., Balas, G. J., and Garrard, W. L., "Robust Dynamic Inversion for Control of Highly Maneuverable Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 18, No. 1, 1995, pp. 18-24.
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    • Reiner, J.1    Balas, G.J.2    Garrard, W.L.3
  • 12
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    • Quantitative Feedback Theory Applied to the Design of a Rotorcraft Flight Control System
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    • (1993) Journal of Guidance, Control, and Dynamics , vol.18 , Issue.4 , pp. 748-753
    • Hess, R.A.1    Gorder, P.J.2
  • 13
    • 84999260855 scopus 로고
    • Rotorcraft Flight Control System Design Including Rotor Degrees of Freedom
    • (Scottsdale, AZ), AIAA, Washington, DC, (AIAA Paper 94-3692)
    • Gorder, P. J., and Hess, R. A., "Rotorcraft Flight Control System Design Including Rotor Degrees of Freedom," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Scottsdale, AZ), AIAA, Washington, DC, 1994 (AIAA Paper 94-3692).
    • (1994) Proceedings of the AIAA Guidance, Navigation, and Control Conference
    • Gorder, P.J.1    Hess, R.A.2
  • 14
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    • Full Envelope Flight Control System Design Using Qualitative Feedback Theory
    • Reynolds, O. R., Pachter, M., and Houpis, C. H., "Full Envelope Flight Control System Design Using Qualitative Feedback Theory," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 1, 1996, pp. 23-29.
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    • Reynolds, O.R.1    Pachter, M.2    Houpis, C.H.3
  • 15
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    • Improvement in Quantitative Nonlinear Feedback Design by Cancellation
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  • 17
    • 0020191066 scopus 로고
    • Plant Rational Transfer Function Approximation from Input-Output Data
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    • Golubev, B.1    Horowitz, I.M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.