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Research on Aircraft Attitude Control Method Based on Linear Active Disturbance Rejection

In this paper, a dual-loop active disturbance rejection attitude controller design method is proposed for the attitude control of aircraft. Firstly, based on the nonlinear dynamic model of aircraft, the control system model with inner loop as angular velocity and outer loop as attitude angle is esta...

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Detalhes bibliográficos
Principais autores: Zhiguo Song, Changjian Zhao, Huiqiang Zhang, Tian Dong, Aojia Ma, Dawei Yan
Formato: Artigo
Idioma:Inglês
Publicado em: Wiley 2022-01-01
coleção:International Journal of Aerospace Engineering
Acesso em linha:http://dx.doi.org/10.1155/2022/1908020
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