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Volumn 4, Issue 1, 2001, Pages 19-50

On-line parameter estimation for restructurable flight control systems

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Indexed keywords


EID: 0001817603     PISSN: 13698869     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1369-8869(00)00023-9     Document Type: Article
Times cited : (36)

References (27)
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    • Nonlinear simulation analysis of a tailless advanced fighter aircraft reconfigurable flight control law
    • AIAA Paper 99-4040, Portland, OR, August
    • Brinker JS, Wise KA. Nonlinear simulation analysis of a tailless advanced fighter aircraft reconfigurable flight control law. Proceedings of the 1999 AIAA Guidance Navigation and Control Conference, AIAA Paper 99-4040, Portland, OR, August 1999.
    • (1999) Proceedings of the 1999 AIAA Guidance Navigation and Control Conference
    • Brinker, J.S.1    Wise, K.A.2
  • 6
    • 0347201434 scopus 로고    scopus 로고
    • Direct adaptive aircraft control using dynamic cell structure neural networks
    • May
    • Jorgensen CC. Direct adaptive aircraft control using dynamic cell structure neural networks. NASA TM 112198, May 1997.
    • (1997) NASA TM 112198
    • Jorgensen, C.C.1
  • 10
    • 0142226215 scopus 로고    scopus 로고
    • A fault tolerant flight control systems for sensor and actuator failures using neural networks
    • Napolitano MR, Younghwan A, Seanor B. A fault tolerant flight control systems for sensor and actuator failures using neural networks, Aircraft Design 2000;3(2):103-28.
    • (2000) Aircraft Design , vol.3 , Issue.2 , pp. 103-128
    • Napolitano, M.R.1    Younghwan, A.2    Seanor, B.3
  • 11
    • 0346571273 scopus 로고
    • Determination of stability derivatives from flight data using a Newton-Raphson minimization technique
    • Iliff KW, Taylor LW. Determination of stability derivatives from flight data using a Newton-Raphson minimization technique. NASA TN D-6579, 1972.
    • (1972) NASA TN D-6579
    • Iliff, K.W.1    Taylor, L.W.2
  • 12
    • 0347201430 scopus 로고
    • Practical aspects of using a maximum likelihood estimation method to extract stability and control derivatives from flight data
    • Iliff KW, Maine RE. Practical aspects of using a maximum likelihood estimation method to extract stability and control derivatives from flight data. NASA TN D-8209, 1976.
    • (1976) NASA TN D-8209
    • Iliff, K.W.1    Maine, R.E.2
  • 13
    • 0345940088 scopus 로고
    • Identification of dynamic systems: Theory and formulation
    • June
    • Maine RE, Iliff KW. Identification of dynamic systems: theory and formulation. NASA RF 1168, June 1986.
    • (1986) NASA RF 1168
    • Maine, R.E.1    Iliff, K.W.2
  • 22
    • 0345940083 scopus 로고    scopus 로고
    • High accuracy evaluation of the finite Fourier transform using sampled data
    • June
    • Morelli EA. High accuracy evaluation of the finite Fourier transform using sampled data. NASA TM 110340, June 1997.
    • (1997) NASA TM 110340
    • Morelli, E.A.1
  • 25
    • 0003963588 scopus 로고
    • USAF stability and control DATCOM
    • October 1960, Revised
    • Hoak DE, Finck RD. USAF stability and control DATCOM. AFWAL-TR-83-3048, October 1960, Revised 1978.
    • (1978) AFWAL-TR-83-3048
    • Hoak, D.E.1    Finck, R.D.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.