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Volumn 6, Issue 3, 2009, Pages 171-186

Hybrid intelligent flight control with adaptive learning parameter estimation

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTATION STRATEGIES; ADAPTIVE LEARNING; FLIGHT CONDITIONS; HYBRID ADAPTIVE CONTROLS; HYBRID METHODS; INTELLIGENT FLIGHT CONTROLS; LEARNING LAWS; LYAPUNOV STABILITY THEORIES; NEURAL NETS; ONLINE PARAMETER ESTIMATIONS; RECURSIVE LEAST-SQUARES; TRACKING PERFORMANCE;

EID: 63049134159     PISSN: 15429423     EISSN: 15429423     Source Type: Journal    
DOI: 10.2514/1.35929     Document Type: Article
Times cited : (26)

References (17)
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    • Steinberg, M.L.1
  • 2
    • 0022118598 scopus 로고
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    • doi: 10.1109/TAC.1985.1104070
    • Rohrs, C. E., Valavani, L., Athans, M., and Stein, G., "Robustness of Continuous-Time Adaptive Control Algorithms in the Presence of Unmodeled Dynamics," IEEE Transactions on Automatic Control, Vol. 30, No. 9, 1985, pp. 881-889. doi: 10.1109/TAC.1985.1104070
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  • 4
    • 84959174847 scopus 로고    scopus 로고
    • FaultTolerant Flight Control viaAdaptive Neural NetworkAugmentation
    • AIAA, Reston, VA, AIAA Paper 1998-4483
    • Rysdyk, R.T., and Calise,A. J., "FaultTolerant Flight Control viaAdaptive Neural NetworkAugmentation," AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1998, AIAA Paper 1998-4483.
    • (1998) AIAA Guidance, Navigation, and Control Conference
    • Rysdyk, R.T.1    Calise, A.J.2
  • 5
  • 7
    • 0023288277 scopus 로고
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    • Narendra, K. S., and Annaswamy, A. M., "A New Adaptive Law for Robust Adaptation Without Persistent Excitation," IEEE Transactions on Automatic Control, Vol. 32, No. 2, 1987, pp. 134-145. doi: 10.1109/TAC.1987.1104543
    • (1987) IEEE Transactions on Automatic Control , vol.32 , Issue.2 , pp. 134-145
    • Narendra, K.S.1    Annaswamy, A.M.2
  • 10
    • 0025745889 scopus 로고
    • Accommodation of Failures in the F-16 Aircraft using Adaptive Control
    • doi: 10.1109/37.103360
    • Ahmed-Zaid, F., Ioannou, P., Gousman, K., and Rooney, R., "Accommodation of Failures in the F-16 Aircraft using Adaptive Control," IEEE Control Systems Magazine, Vol. 11, No. 1, 1991, pp. 73-78. doi: 10.1109/37.103360
    • (1991) IEEE Control Systems Magazine , vol.11 , Issue.1 , pp. 73-78
    • Ahmed-Zaid, F.1    Ioannou, P.2    Gousman, K.3    Rooney, R.4
  • 11
    • 0036640829 scopus 로고    scopus 로고
    • A Multiple Model Adaptive Flight Control Scheme for Accommodation of Actuator Failures
    • Boskovic, J. D., and Mehra, R. K., "A Multiple Model Adaptive Flight Control Scheme for Accommodation of Actuator Failures," Journal of Guidance, Control and Dynamics, Vol. 25, No. 4, 2002, pp. 712-724.
    • (2002) Journal of Guidance, Control and Dynamics , vol.25 , Issue.4 , pp. 712-724
    • Boskovic, J.D.1    Mehra, R.K.2
  • 12
    • 63049125674 scopus 로고    scopus 로고
    • Jacklin, S. A., Schumann, J. M., Gupta, P. P., Richard, R., Guenther, K., and Soares, F., Development of Advanced Verification and Validation Procedures and Tools for the Certification of Learning Systems in Aerospace Applications, AIAA Infotech@Aerospace Conference, AIAA, Reston, VA, 2005, AIAA Paper 2005-6912.
    • Jacklin, S. A., Schumann, J. M., Gupta, P. P., Richard, R., Guenther, K., and Soares, F., "Development of Advanced Verification and Validation Procedures and Tools for the Certification of Learning Systems in Aerospace Applications," AIAA Infotech@Aerospace Conference, AIAA, Reston, VA, 2005, AIAA Paper 2005-6912.
  • 14
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  • 17
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    • DynamicWaypoint Generation Given Reduced Flight Performance
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    • Atkins, E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.