Aircraft parameter estimation using a stacked long short-term memory network and Levenberg-Marquardt method

Author:

HUI Zhe,KONG Yinan,YAO WeigangORCID,CHEN Gang

Funder

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Natural Science Foundation of Shaanxi Province

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference35 articles.

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3. Nonlinear model identification methodology for small, fixed-wing, unmanned aircraft;Simmons;J Aircr,2019

4. Peyada NK, Arpita S, Ghosh AK. Aerodynamic characterization of HANSA-3 aircraft using equation error, maximum likelihood and filter error methods. Proceedings of the international multiconference of engineers and computer scientists; 2008 Mar 19-21; Hong Kong, China. 2008.

5. Gresham JL, Simmons BM, Hopwood JW, et al. Spin aerodynamic modeling for a fixed-wing aircraft using flight data. AIAA scithch 2022 forum; 2022 Jan 3-7; San Diego, CA. Reston: AIAA; 2022.

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