[1]吴 瑕,李晓栋,王思远,等. 基于RLESO 的高超声速巡航飞行器跟踪控制器设计[J].控制与信息技术,2018,(06):1.[doi:10.13889/j.issn.2096-5427.2018.06.200]
 WU Xia,LI Xiaodong,WANG Siyuan,et al. Design of Tracking Controller for Hypersonic Cruise Vehicle Based on RLESO[J].High Power Converter Technology,2018,(06):1.[doi:10.13889/j.issn.2096-5427.2018.06.200]
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 基于RLESO 的高超声速巡航飞行器跟踪控制器设计()
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《控制与信息技术》[ISSN:2095-3631/CN:43-1486/U]

卷:
期数:
2018年06期
页码:
1
栏目:
出版日期:
2018-12-05

文章信息/Info

Title:
 Design of Tracking Controller for Hypersonic Cruise Vehicle Based on RLESO
文章编号:
2096-5427(2018)06-0000-00
作者:
 吴 瑕1李晓栋2王思远2罗世彬2
 (1. 中南大学 信息科学与工程学院,湖南 长沙 410083;2. 中南大学 航空航天学院, 湖南 长沙 410083)
Author(s):
WU Xia1 LI Xiaodong2 WANG Siyuan2 LUO Shibin2
 ( 1.School of Information Science and Engineering, Central South University, Changsha, Hunan 410083, China;
2. School of Aeronautics and Astronautics, Central South University, Changsha, Hunan 410083, China )
关键词:
 高超声速巡航飞行器降阶线性扩张状态观测器自抗扰跟踪控制器
Keywords:
 hypersonic cruise vehicle reduced-order linear extended state observer active disturbance rejection tracking controller
分类号:
V249.1
DOI:
10.13889/j.issn.2096-5427.2018.06.200
文献标志码:
A
摘要:
 针对高超声速巡航飞行器的强非线性、强耦合、快时变以及不确定性等特性,设计了一种基于降阶线性扩张状态观测器的自抗扰跟踪控制器。其将高超声速巡航飞行器的纵向平面运动模型分为速度回路和高度回路,对各回路分别设计辅助状态变量以简化跟踪控制器的设计过程;在此基础上,对两个回路分别设计基于降阶线性扩张状态观测器的自抗扰跟踪控制器来获得满意的控制性能。仿真结果表明,相比于常规的线性自抗扰跟踪控制器,以降阶线性扩张状态观测器为基础的自抗扰跟踪控制器能够以更快的速度跟踪上系统的期望输入,且超调量更小。
Abstract:
 An active disturbance rejection tracking controller based on reduced-order linear extended state observer was designed for the hypersonic cruise vehicle with strong nonlinearity, coupling, uncertainties and fast time-varying. The longitudinal plane motion model of the hypersonic cruise vehicle can be divided into the velocity loop and the altitude loop. New variables were set for the two loops to simplify the design process of the tracking controllers. Then, the active disturbance rejection tracking controller based on reduced-order linear extended state observer was designed separately for each loop to acquire desired performance. Simulations were performed to verify the performance of the designed controllers. Results show that the active disturbance rejection tracking controller based on reduced-order linear extended state observer has faster response and smaller overshoot compared with the conventional linear active disturbance rejection controller.

参考文献/References:

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备注/Memo

备注/Memo:
收稿日期:2018—09—30
作者简介:吴瑕(1992—),女,博士研究生,主要研究方向为高超声速飞行器姿态控制。
基金项目:国家自然科学基金(11272349)
更新日期/Last Update: 2018-11-30