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Volumn 7, Issue , 2005, Pages 5219-5229

Adaptive flight control of a sensor guided munition

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CHANGES; FLIGHT CONTROL SYSTEMS; LINEAR QUADRATIC REGULATORS; TUNNEL MEASUREMENT;

EID: 29744467988     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (39)

References (20)
  • 1
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    • to appear in the
    • Steinberg, M., A Historical Overview of Research in Reconfigurable Flight Control, to appear in the Journal of Aerospace Engineering, 2005.
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    • Steinberg, M.1
  • 2
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  • 3
    • 29744454562 scopus 로고    scopus 로고
    • Self designing controller
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  • 4
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    • Intelligent flight control
    • Final Report, May
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    • (1999) Boeing Report No. STL 99P0040 , vol.STL 99P0040
  • 5
    • 19944398696 scopus 로고    scopus 로고
    • Reconfigurable systems for tailless fighter aircraft - RESTORE
    • AFRL-VA-WP-TR-99-3067
    • Reconfigurable Systems for Tailless Fighter Aircraft - RESTORE, Final Report, AFRL-VA-WP-TR-99-3067.
    • Final Report
  • 7
    • 84959147326 scopus 로고    scopus 로고
    • Reconfigurable flight control for a tailless advanced fighter aircraft
    • Boston, MA, August
    • Wise, K., and J. Brinker, "Reconfigurable Flight Control for a Tailless Advanced Fighter Aircraft," Proc. of the AIAA GNC Conference, Boston, MA, August, 1998, pp. 75-87.
    • (1998) Proc. of the AIAA GNC Conference , pp. 75-87
    • Wise, K.1    Brinker, J.2
  • 9
    • 85087192694 scopus 로고    scopus 로고
    • Flight testing of a reconfigurable flight control law on the X-36 tailless fighter aircraft
    • Denver, CO, August
    • Brinker, J., and K. A. Wise, "Flight Testing of a Reconfigurable Flight Control Law on the X-36 Tailless Fighter Aircraft," Proc. of the AIAA GNC Conf., Denver, CO, August, 2000.
    • (2000) Proc. of the AIAA GNC Conf.
    • Brinker, J.1    Wise, K.A.2
  • 10
    • 84959178592 scopus 로고    scopus 로고
    • Neural-adaptive nonlinear autopilot design for an agile anti-air missile
    • San Diego, CA, August, Paper AIAA 96-3914
    • McFarland, M., and A. Calise, "Neural-adaptive nonlinear autopilot design for an agile anti-air missile," Proc. of the AIAA GNC Conf., San Diego, CA, August, 1996, Paper AIAA 96-3914.
    • (1996) Proc. of the AIAA GNC Conf.
    • McFarland, M.1    Calise, A.2
  • 11
    • 84959088865 scopus 로고    scopus 로고
    • Multi-layer Neural networks and adaptive nonlinear control of for agile anti-air missiles
    • New Orleans, LA., August. Paper AIAA 97-3540
    • McFarland, M., and A. Calise, "Multi-layer Neural networks and adaptive nonlinear control of for agile anti-air missiles," Proc. of the AIAA GNC Conf., New Orleans, LA., August, 1997. Paper AIAA 97-3540.
    • (1997) Proc. of the AIAA GNC Conf.
    • McFarland, M.1    Calise, A.2
  • 13
    • 85087605832 scopus 로고    scopus 로고
    • Application of an adaptive autopilot design to a family of guided munitions
    • Denver, CO, August, AIAA Paper No, 2000-3969
    • Sharma, M., A. J. Calise, and J. E. Corban, "Application of an Adaptive Autopilot Design to a Family of Guided Munitions, Proc. of the AIAA GNC Conf, Denver, CO, August, 2000, AIAA Paper No, 2000-3969.
    • (2000) Proc. of the AIAA GNC Conf
    • Sharma, M.1    Calise, A.J.2    Corban, J.E.3
  • 14
    • 78651072099 scopus 로고    scopus 로고
    • Neural network augmentation of existing linear controllers
    • Montreal, Canada, August, AIAA Paper No, 2001-4163
    • Sharma, M., and A. Calise, "Neural Network augmentation of Existing Linear Controllers," Proc. of the AIAA GNC Conf., Montreal, Canada, August, 2001, AIAA Paper No, 2001-4163.
    • (2001) Proc. of the AIAA GNC Conf.
    • Sharma, M.1    Calise, A.2
  • 16
    • 23944483772 scopus 로고    scopus 로고
    • Positive μ - Modification for stable adaptation in a class of nonlinear systems with actuator constraints
    • June
    • E. Lavretsky, N. Hovakimyan, "Positive μ - modification for stable adaptation in a class of nonlinear systems with actuator constraints," Proceedings of American Control Conference, June 2004.
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    • Lavretsky, E.1    Hovakimyan, N.2
  • 17
    • 0025254702 scopus 로고
    • Bank-to-turn missile autopilot design using loop transfer recovery
    • Wise, K.A., "Bank-To-Turn Missile Autopilot Design Using Loop Transfer Recovery," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1, 1990, pp. 145-152.
    • (1990) Journal of Guidance, Control, and Dynamics , vol.13 , Issue.1 , pp. 145-152
    • Wise, K.A.1
  • 18
    • 19644383485 scopus 로고
    • Approximating a linear quadratic missile autopilot design using an output feedback projective control
    • New Orleans, LA, August, Paper AIAA 91-2613
    • Wise, K. and F. Deylami, "Approximating a Linear Quadratic Missile Autopilot Design Using an Output Feedback Projective Control," Proc. of the AIAA GNC Conf., New Orleans, LA, August, 1991, Paper AIAA 91-2613, pp. 114-122.
    • (1991) Proc. of the AIAA GNC Conf. , pp. 114-122
    • Wise, K.1    Deylami, F.2
  • 20
    • 0026882722 scopus 로고
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    • Pomet, J.B., Praly, L., "Adaptive Nonlinear Regulation: Estimation from Lyapunov Equation. IEEE Transactions on Automatic Control", 37(6): 729-740, 1992.
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    • Pomet, J.B.1    Praly, L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.