首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Stability region analysis of the parasitic loop of the semi-strapdown homing seeker
【24h】

Stability region analysis of the parasitic loop of the semi-strapdown homing seeker

机译:半捷联导引头寄生回路的稳定区域分析

获取原文
获取原文并翻译 | 示例
           

摘要

The stability of the parasitic loop induced by the disturbance rejection effect (DRE) of a semi-strapdown homing seeker (SSHS) is analysed in this paper. First, the seeker's tracking controller is designed so as to have a simple structure and then the explicit relationships between the control parameters and the desired performance index is presented. Mathematical models of the DRE of the SSHS and the parasitic loop are then proposed. The approximate maximum magnitude of the seeker's DRE as a function of the friction coefficient and the counter electromotive force coefficient is also given. Routh's criterion is used to obtain the approximate stability region of the parasitic loop. The necessary and sufficient conditions which ensure the stability of the parasitic loop are directly related to the seeker's control parameters. This approach provides direct theoretical support for the design of a seeker's control system. Simulations are performed to verify the validity of the stability analysis performed on the parasitic loop.
机译:本文分析了半捷联寻的导引头(SSHS)的干扰抑制效应(DRE)引起的寄生环路的稳定性。首先,将搜索器的跟踪控制器设计为具有简单的结构,然后给出控制参数与所需性能指标之间的明确关系。然后提出了SSHS的DRE和寄生回路的数学模型。还给出了作为摩擦系数和反电动势系数的函数的搜寻器DRE的近似最大大小。 Routh准则用于获得寄生环路的近似稳定区域。确保寄生环路稳定性的必要和充分条件直接与搜寻器的控制参数有关。这种方法为搜寻器控制系统的设计提供了直接的理论支持。进行仿真以验证对寄生环路执行的稳定性分析的有效性。

著录项

  • 来源
  • 作者单位

    Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

    Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

    Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;

    China Aerospace Science & Industry Corp, Beijing, China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    semi-strapdown homing seeker; parasitic loop; disturbance rejection effect; stability region;

    机译:半捷联导引头;寄生回路干扰抑制效果;稳定区;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号