Identification of Aerodynamic Parameters Based on Maximum Likelihood Estimation

Author:

Dai Guicheng1,Cheng Lei2,Li Donghui2,Ma Hongtu3,Zhang Lei3

Affiliation:

1. Shenyang Aircraft Design and Research Institute,Shenyang,China

2. Shenyang Aerospace University,Shenyang,China

3. Liaoning General Aviation Academy,Shenyang,China

Publisher

IEEE

Reference19 articles.

1. Research on aerodynamic parameter identification technology in wind tunnel free-flight test based on Maximum Likelihood Estimation[J];tianjiao;Journal of Experiments in Fluid Mechanics,2015

2. Parameter Identification and Adaptive Control of Aircraft Based on BP Neural Network[J];guanghui;Aerospace Control,2021

3. Modeling and simulation of longitudinal autopilot for general aviation aircraft

4. Survey on design technology of distributed electric propulsion aircraft[J];huang;Acta Aeronautica et Astronautica Sinica,2021

5. Parameter Identification Method of Quadrotor Unmanned Aerial Vehicle[J];yijie;Journal of Fudan University (Natural Science),2021

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