Backstepping sliding mode control for integrated guidance and control design based on active disturbance rejection

被引：6

作者：

Dong, Chao-Yang ^{[1
]}

Cheng, Hao-Yu ^{[1
]}

Wang, Qing ^{[2
]}

机构：

[1] School of Aeronautic Science and Engineering, Beihang University, Beijing

[2] School of Automation Science and Electrical Engineering, Beihang University, Beijing

来源：

Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2015年 / 37卷 / 07期

关键词：

Active disturbance rejection control; Backstepping terminal sliding mode; Extended state observer; Integrated guidance and control;

D O I：

10.3969/j.issn.1001-506X.2015.07.21

中图分类号：

学科分类号：

摘要：

Based on active disturbance rejection control and the backstepping-sliding mode design method, an integrated guidance and control design is proposed for missiles during the terminal course. The integrated model is formulated as a block-strict-feedback nonlinear system, in which modeling errors and target maneuvers are viewed as unknown uncertainties. An extended state observer is developed to estimate and compensate the impact from uncertainties and disturbances. A backstepping-sliding mode controller is proposed to realize the attitude control. Simulation results show that, with the application of the proposed method, small miss distances are achieved, and the system is robust against system uncertainties and disturbances. ©, 2015, Chinese Institute of Electronics. All right reserved.

引用

页码：1604 / 1610

页数：6

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