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Volumn 19, Issue 6, 1996, Pages 1226-1230

Lyapunov stability analysis of daisy chain control allocation

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; FEEDBACK CONTROL; LYAPUNOV METHODS; MATHEMATICAL MODELS; REDUNDANCY; SYSTEM STABILITY;

EID: 0030287268     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21776     Document Type: Article
Times cited : (189)

References (20)
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  • 4
    • 0003096706 scopus 로고
    • Dynamic Inversion: An Evolving Methodology for Flight Control Design
    • Enns, D., Bugajski, D., Hendrick, R., and Stein, G., "Dynamic Inversion: An Evolving Methodology for Flight Control Design," International Journal of Control, Vol. 59, No. 1, 1994, pp. 71-91.
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    • Enns, D.1    Bugajski, D.2    Hendrick, R.3    Stein, G.4
  • 5
    • 0003580241 scopus 로고
    • Honeywell Technology Center, U.S. Air Force Contract F33615-92-C-3607, May
    • Anon., "Multivariable Control Design Guidelines, First Draft," Honeywell Technology Center, U.S. Air Force Contract F33615-92-C-3607, May 1995.
    • (1995) Multivariable Control Design Guidelines, First Draft
  • 8
    • 3943068494 scopus 로고
    • Aircraft Div., Northrop Corp., AFWAL-TR-88-2061, Hawthorne, CA, June
    • Anon., "Design Methods for Integrated Control Systems," Aircraft Div., Northrop Corp., AFWAL-TR-88-2061, Hawthorne, CA, June 1988.
    • (1988) Design Methods for Integrated Control Systems
  • 9
    • 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.
    • (1992) Journal of Guidance, Control, and Dynamics , vol.15 , Issue.4 , pp. 976-984
    • Snell, S.A.1    Enns, D.F.2    Garrard, W.L.3
  • 13
    • 0028388432 scopus 로고
    • Constrained Control Allocation: Three-Moment Problem
    • Durham, W. C., "Constrained Control Allocation: Three-Moment Problem," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 2, 1994, pp. 330-336.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.2 , pp. 330-336
    • Durham, W.C.1
  • 14
    • 84999084560 scopus 로고
    • On the Application of Neural Network Computing to the Constrained Flight Control Allocation Problem
    • (Scottsdale, AZ), AIAA, Washington, DC
    • Grogan, R. L., Durham, W. C., and Krishnan, R., "On the Application of Neural Network Computing to the Constrained Flight Control Allocation Problem," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Scottsdale, AZ), AIAA, Washington, DC, 1994, pp. 911-921.
    • (1994) Proceedings of the AIAA Guidance, Navigation, and Control Conference , pp. 911-921
    • Grogan, R.L.1    Durham, W.C.2    Krishnan, R.3
  • 15
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    • Optimizing the Use of Multiple Control Effectors Using Bifurcation Analysis
    • (Scottsdale, AZ), AIAA, Washington, DC
    • Lowenberg, M., "Optimizing the Use of Multiple Control Effectors Using Bifurcation Analysis," Proceedings of the AIAA Atmospheric Flight Mechanics Conference (Scottsdale, AZ), AIAA, Washington, DC, 1994, pp. 45-55.
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    • Lowenberg, M.1
  • 16
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    • Multivariable Control Allocation and Control Law Conditioning when Control Effectors Limit
    • (Scottsdale, AZ), AIAA, Washington, DC
    • Virnig, J. C., and Bodden, D. S., "Multivariable Control Allocation and Control Law Conditioning when Control Effectors Limit," Proceedings of the AIAA Guidance, Navigation, and Control Conference (Scottsdale, AZ), AIAA, Washington, DC, 1994, pp. 572-582.
    • (1994) Proceedings of the AIAA Guidance, Navigation, and Control Conference , pp. 572-582
    • Virnig, J.C.1    Bodden, D.S.2
  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.