@inproceedings{be18820b534c4e98a06aaa50a74733df,
title = "Dynamic decoupling nonlinear control method for aircraft gust alleviation",
abstract = "A dynamic decoupling nonlinear control method for MIMO system is presented in this paper. The dynamic inversion method is used to decouple the multivariable system. The nonlinear control method is used to overcome the poor decoupling effect when the system model is inaccurate. The nonlinear control method has correcting function and is expressed in analytic form, it is easy to adjust the parameters of the controller and optimize the design of the control system. The method is used to design vertical transition mode of active control aircraft for gust alleviation. Simulation results show that the designed vertical transition mode improves the gust alleviation effect about 34% comparing with the normal aircraft.",
keywords = "Decoupling, Dynamic inversion, Gust alleviation, Nonlinear control",
author = "Yang Lv and Xiaopeng Wan and Aijun Li",
year = "2008",
doi = "10.1117/12.806859",
language = "英语",
isbn = "9780819473622",
series = "Proceedings of SPIE - The International Society for Optical Engineering",
booktitle = "Seventh International Symposium on Instrumentation and Control Technology",
note = "7th International Symposium on Instrumentation and Control Technology: Measurement Theory and Systems and Aeronautical Equipment ; Conference date: 10-10-2008 Through 13-10-2008",
}