Controller design and stability analysis for spinning missiles via tensor product

Zhiming Zhou; Zhen Liu; Yi PanJianqiang Yi

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Controller design and stability analysis for spinning missiles via tensor product

机译：Controller design and stability analysis for spinning missiles via tensor product

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摘要

In this paper, the controller design and stability analysis for the parameters time-varying model of spinning missiles are investigated. A mathematical model for the spinning missile considering the flight parameters varying with time is proposed. Based on tensor product (TP) model transformation for the spinning missile, the parallel distributed compensation (PDC) state feedback controller is designed, and the stability of the controlled system is analyzed with the tool of linear matrix inequalities (LMIs). Numerical simulations with time-varying parameters are conducted to demonstrate the effectiveness of the proposed controller. The given controller can not only guarantee the steady performance but also the decoupling performance between pitch and yaw channels when used in the flight parameters time-varying spinning missiles.

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来源
《Aerospace science and technology》 |2022年第11期|107877.1-107877.9|共9页
作者
Zhiming Zhou; Zhen Liu; Yi PanJianqiang Yi;
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作者单位

Institute of Automation, Chinese Academy of Sciences, Beijing, 100190, China;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种英语
中图分类
关键词
Spinning missile; Tensor product model transformation; Parallel distributed compensation; Model filtering; Stability analysis;

Controller design and stability analysis for spinning missiles via tensor product

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