Nonlinear Flight Mode Identification by Applying Modified Ensemble Empirical Mode Decomposition and Hilbert–Huang Transformation-Reference-Cited by-同舟云学术

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Nonlinear Flight Mode Identification by Applying Modified Ensemble Empirical Mode Decomposition and Hilbert–Huang Transformation

Published:2020-03-05 Issue:4 Volume:21 Page:1161-1173
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Mokhtari S. Abolfazl^ORCID,Sabzehparvar Mehdi,Imani Kazem

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s42405-020-00258-7.pdf

Reference29 articles.

1. Roskam J (1995) Airplane flight dynamics and automatic flight control. DAR corporation, Kansas, pp 33–113

2. Morelli EA (2000) Real-time parameter estimation in the frequency domain. J Guid Control Dyn 23(5):812–818

3. Jategaonkar R, Fischenberg D, Von Gruenhagen W (2004) Aerodynamic modeling and system identification from flight data-recent applications at DLR. J Aircr 41(4):681–691

4. Tischler MB, Remple RK (2006) Aircraft and rotorcraft system identification. American Institute of Aeronautics and Astronautics, New York, pp 22–53

5. Tayefi M, Roshanian J, Ghaffari A (2009) On estimation of vehicle linear model parameters. Aircr Eng Aerosp Technol 81(5):432–438

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