Design of Lateral Three-Loop Autopilot with Pseudo-Angle of Sideslip Feedback Based on Active Disturbance Rejection Control

Heting Wang, Hui Wang, Keqing Guo, Daoguang Tang*, Yuanyue Lei

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The lateral linear control model of missile is established and the symbol definition of lateral aerodynamic transfer function is given in this paper. And the frequency domain characteristics of the lateral airframe are analyzed in the low, middle and high frequency band, respectively. Combined with the active disturbance rejection control method, a lateral three-loop autopilot based on linear active disturbance rejection control is proposed. Through the dynamic estimation and compensation of the extended state observer, the robustness to the system uncertainty is enhanced. Simulation results of different cases demonstrate the effectiveness and robustness of proposed autopilots and lateral active disturbance rejection three-loop autopilot is more robust.

源语言英语
主期刊名2023 42nd Chinese Control Conference, CCC 2023
出版商IEEE Computer Society
3552-3558
页数7
ISBN(电子版)9789887581543
DOI
出版状态已出版 - 2023
活动42nd Chinese Control Conference, CCC 2023 - Tianjin, 中国
期限: 24 7月 202326 7月 2023

出版系列

姓名Chinese Control Conference, CCC
2023-July
ISSN(印刷版)1934-1768
ISSN(电子版)2161-2927

会议

会议42nd Chinese Control Conference, CCC 2023
国家/地区中国
Tianjin
时期24/07/2326/07/23

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