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Volumn 22, Issue 2, 2000, Pages 133-148

Estimation of aircraft aerodynamic derivatives using extended kaiman filter

Author keywords

Aerodynamic coefficient; Aerodynamic derivative; Kaiman filler; Parameter estimation; Simulation

Indexed keywords

COMPUTER SIMULATION; ESTIMATION; KALMAN FILTERING; LEAST SQUARES APPROXIMATIONS; MATHEMATICAL MODELS; PARAMETER ESTIMATION; STATISTICAL METHODS;

EID: 0034206314     PISSN: 01007386     EISSN: None     Source Type: Journal    
DOI: 10.1590/S0100-73862000000200001     Document Type: Article
Times cited : (14)

References (15)
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    • Emprego de Filtro Adaptative para Identificaçao dos Coeficientes do Movimento do Navio
    • Florianöpolis, Brasil
    • Brinati, Luiz H. and Rios Neto, Atair, 1977, Emprego de Filtro Adaptative para Identificaçao dos Coeficientes do Movimento do Navio, IV Congresso Brasileiro de Engenharia Mecânica- COBEM, Florianöpolis, Brasil.
    • (1977) IV Congresso Brasileiro de Engenharia Mecânica- COBEM
    • Brinati, L.H.1    Rios Neto, A.2
  • 4
    • 0141625585 scopus 로고    scopus 로고
    • the MIT press, Massachusetts Institute of Technology, Cambridge, Massachusetts
    • Gelb, Arthur at al, 1996, Applied Optimal Control, the MIT press, Massachusetts Institute of Technology, Cambridge, Massachusetts.
    • (1996) Applied Optimal Control
    • Gelb, A.1
  • 5
    • 0024732403 scopus 로고
    • Parameter Estimation for Flight Vehicles
    • Iliff, Kenneth W., 1989, Parameter Estimation for Flight Vehicles, AIAA Journal of Guidance and Control, vol. 12 (5) pp. 609-622.
    • (1989) AIAA Journal of Guidance and Control , vol.12 , Issue.5 , pp. 609-622
    • Iliff, K.W.1
  • 9
    • 33746697627 scopus 로고    scopus 로고
    • Closed-Loop System Identification Experience for Flight Control Law and Flying Qualities Evaluation of a High Performance Fighter Aircraft
    • Madrid, Spain
    • Murphy, Patrick C., 1998, Closed-Loop System Identification Experience for Flight Control Law and Flying Qualities Evaluation of a High Performance Fighter Aircraft, Paper n°. 16 - System Identification for Integrated Aircraft Development and Testing Symposium, Madrid, Spain.
    • (1998) Paper N°. 16 - System Identification for Integrated Aircraft Development and Testing Symposium
    • Murphy, P.C.1
  • 11
    • 0028550019 scopus 로고
    • Neural Network Based Parameter Estimation of Unstable Aerospace Dynamic Systems
    • Raoi, J. R., 1994, Neural Network Based Parameter Estimation of Unstable Aerospace Dynamic Systems, IEE Proceedings of Control Theory and Application, vol. 141 (6), pp. 385-388.
    • (1994) IEE Proceedings of Control Theory and Application , vol.141 , Issue.6 , pp. 385-388
    • Raoi, J.R.1
  • 13
    • 0023348475 scopus 로고
    • On-Line Aircraft and Stability Derivative Estimation Using the Modificd-Gain Extended Kaiman Filter
    • Speyer, Jason L. and Edwin, Z. Crues, 1987, On-Line Aircraft and Stability Derivative Estimation Using the Modificd-Gain Extended Kaiman Filter, AIAA Journal of Guidance and Control, vol. 10 (3), pp. 262-268.
    • (1987) AIAA Journal of Guidance and Control , vol.10 , Issue.3 , pp. 262-268
    • Speyer, J.L.1    Crues, E.Z.2
  • 15
    • 0031271514 scopus 로고    scopus 로고
    • Aerodynamic Parameter Estimation for High Performance Aircraft Using Extended Kaiman Filtering
    • Vélo, Juan Garcia and Walker, Bruce K., 1997, Aerodynamic Parameter Estimation for High Performance Aircraft Using Extended Kaiman Filtering, AIAA Journal of Guidance and Control, vol. 20 (6), pp. 1257-1259.
    • (1997) AIAA Journal of Guidance and Control , vol.20 , Issue.6 , pp. 1257-1259
    • Vélo, J.G.1    Walker, B.K.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.