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Volumn 6, Issue 8, 2002, Pages 591-598

Flexible aircraft model identification for control law design

Author keywords

ERA algorithm; Flexible aircraft; Identification for control; Output error minimization

Indexed keywords

AIRCRAFT MODELS; ALGORITHMS; IDENTIFICATION (CONTROL SYSTEMS); LINEARIZATION;

EID: 0040673672     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(02)01197-5     Document Type: Article
Times cited : (18)

References (12)
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    • D.S. Bayard, An algorithm for state-space frequency domain identification without windowing distortions, IEEE Trans. Autom. Control 39 (9) (1994) 1880-1885.
    • (1994) IEEE Trans. Autom. Control , vol.39 , Issue.9 , pp. 1880-1885
    • Bayard, D.S.1
  • 2
    • 0022813358 scopus 로고
    • The fit of a sum of exponentials to noisy data
    • P. De Groen, B. De Moor, The fit of a sum of exponentials to noisy data, J. Comput. Appl. Math. 20 (1987) 175-187.
    • (1987) J. Comput. Appl. Math. , vol.20 , pp. 175-187
    • De Groen, P.1    De Moor, B.2
  • 4
    • 0029696291 scopus 로고    scopus 로고
    • Evolution of flight vehicle system identification
    • P.G. Hamel, R.V. Jategaonkar, Evolution of flight vehicle system identification, J. Aircraft 33 (1) (1996) 9-28.
    • (1996) J. Aircraft , vol.33 , Issue.1 , pp. 9-28
    • Hamel, P.G.1    Jategaonkar, R.V.2
  • 6
    • 0003409960 scopus 로고
    • Aircraft parameter estimation in the frequency domain
    • August
    • V. Klein, Aircraft parameter estimation in the frequency domain, August 1978, AIAA Paper 78-1344.
    • (1978) AIAA Paper 78-1344
    • Klein, V.1
  • 7
    • 0039916228 scopus 로고    scopus 로고
    • New flight control laws for large capacity aircraft. Experimentation on airbus A 340
    • Melbourne, Australia
    • F. Kubica, New flight control laws for large capacity aircraft. Experimentation on airbus A 340, in: 21th ICAS Congress Proceedings, Melbourne, Australia, 1998.
    • (1998) 21th ICAS Congress Proceedings
    • Kubica, F.1
  • 9
    • 0004293237 scopus 로고
    • Identification of dynamic systems - Applications to aircraft. Part 1: The output error approach
    • AGARD
    • R.E. Maine, K.W. Iliff, Identification of Dynamic Systems - Applications to Aircraft. Part 1: The Output Error Approach, in: AG300, Vol. 3, AGARD, 1986.
    • (1986) AG300 , vol.3
    • Maine, R.E.1    Iliff, K.W.2
  • 10
    • 0030388522 scopus 로고    scopus 로고
    • Vibration data analysis for a commercial aircraft
    • T. McKelvey, T. Abrahamsson, L. Ljung, Vibration data analysis for a commercial aircraft, Automatica 32 (12) (1996) 1689-1700.
    • (1996) Automatica , vol.32 , Issue.12 , pp. 1689-1700
    • McKelvey, T.1    Abrahamsson, T.2    Ljung, L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.