导弹与制导技术

基于LMI的雷达稳定伺服系统动态输出反馈 H控制

  • 杨大鹏 ,
  • 刘向东
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  • 北京理工大学自动化学院,北京 100081

杨大鹏(1988-),黑龙江人,博士研究生,研究方向:高精度伺服控制。

收稿日期: 2010-10-20

  网络出版日期: 2025-05-30

Dynamic Output Feedback H Control of Radar Stabilization Servo System Based on LMI

  • YANG Dapeng ,
  • LIU Xiangdong
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  • School of Automation, Beijing Institute of Technology, Beijing 100081, China

Received date: 2010-10-20

  Online published: 2025-05-30

摘要

为提高雷达稳定伺服系统的动态性能和抗干扰能力,基于线性矩阵不等式(LMI)设计了速度环动态输出反馈H控制器。对于不同幅值和频率的信号开展了阶跃响应和抗扰性能的Matlab仿真实验。结果表明,与传统PID控制器相比,采用这种输出反馈H控制器的伺服系统速度环阶跃响应动态性能优越;对不同频率的载体扰动信号情况下,隔离度均显著提高。提出的输出反馈H控制器阶次低,不存在输出饱和问题,便于物理实现。

本文引用格式

杨大鹏 , 刘向东 . 基于LMI的雷达稳定伺服系统动态输出反馈 H控制[J]. 弹箭与制导学报, 2011 , 31(4) : 53 -56,61 . DOI: 10.15892/j.cnki.djzdxb.2011.04.017

Abstract

To improve dynamic and disturbance rejecting ability of radar stable servo system, output feedback H controller of speed loop was presented based on LMI. For signals with different amplitude and frequency, simulations of the closed loop in Matlab were done, which contained both step response and disturbance tests. Simulation results indicate that the servo system with LMI controller performs better in dynamic response with shorter response time. The new designed system has better rejection rate than the system with traditional PID controller for variable frequency disturbance signals. Also, the LMI controller advanced here not only has no shortcoming like saturation of controlled output but also has some advantages such as low order and easy to realize.

参考文献

[1]
穆虹. 防空导弹雷达设计[M]. 北京: 宇航出版社, 1996.
[2]
陈康. 伺服稳定平台隔离能力研究[J]. 黑龙江科技信息, 2008(34): 15-17.
[3]
赵超. 导引头稳定系统隔离度研究[J]. 电光与控制, 2008, 15(7): 78-82.
[4]
严运彪, 何广军, 杨立耀. H控制理论在雷达伺服系统设计中的应用[J]. 现代防御技术, 2009, 37(1): 61-65.
[5]
邢卓异, 朱齐丹, 定宇. 基于幅相裕度参数整定的二自由度IMC-PID 雷达伺服系统设计[J]. 哈尔滨工程大学学报, 2006, 27(3): 404-408.
[6]
崔莹莹, 夏群力, 祁载康. 导引头稳定平台隔离度模型研究[J]. 弹箭与制导学报, 2006, 26(1): 22-25.
[7]
俞立. 鲁棒控制——线性矩阵不等式处理方法[M]. 北京: 清华大学出版社, 2002.
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