Back-stepping Active Disturbance Rejection Control for Attitude Control of Aircraft Systems Based on Extended State Observer

被引：16

作者：

Zhuang, Huixuan ^{[1
,2
]}

Sun, Qinglin ^{[1
,2
]}

Chen, Zengqiang ^{[1
,2
]}

Zeng, Xianyi ^{[3
,4
]}

机构：

[1] Nankai Univ, Coll Artificial Intelligence, Tianjin 300350, Peoples R China

[2] Nankai Univ, Intelligent Robots Key Lab, Tianjin 300350, Peoples R China

[3] Univ Lille 1, F-59000 Lille, France

[4] ENSAIT, GEMTEX Lab, F-59100 Roubaix, France

来源：

INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS | 2021年 / 19卷 / 06期

基金：

中国国家自然科学基金;

关键词：

Active disturbance rejection control; aircraft attitude control; back-stepping technique; extended state observer;

D O I：

10.1007/s12555-019-1029-x

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Robust flight control laws based on back-stepping technology and ADRC method are designed for attitude control of a non-linear aircraft system. First, non-linear aircraft model is introduced and converted to standard equation of state. Then, the extended state observer is applied to estimate the unknown variables, the homologous ADRC is designed to ensure the state variables of the CLS to astringe to the reference state. Next, the stability of ESO and ADRC are analyzed and proven theoretically. At last, the effectiveness of this method is illustrated by extensive comparative simulations. The results acquired from simulation attest that ADRC can achieve better control performance than PID and SMC method.

引用

页码：2134 / 2149

页数：16

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