Controller Design and Stability Analysis for Spinning Missile Via Tensor Product

	Controller Design and Stability Analysis for Spinning Missile Via Tensor Product
	Zhiming Zhou; Zhen Liu; Yi Pan; Jianqiang Yi
发表期刊	Aerospace Science and Technology
	2022
页码	107877
文章类型	研究性论文
摘要	In this paper, the controller design and stability analysis for the parameters time-varying model of spinning missiles are investigated. Amathematical 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
语种	英语
七大方向——子方向分类	智能控制
国重实验室规划方向分类	智能计算与学习
是否有论文关联数据集需要存交	否
文献类型	期刊论文
条目标识符	http://ir.ia.ac.cn/handle/173211/57428
专题	复杂系统认知与决策实验室_听觉模型与认知计算
通讯作者	Zhiming Zhou
作者单位	中国科学院自动化研究所
第一作者单位	中国科学院自动化研究所
通讯作者单位	中国科学院自动化研究所
推荐引用方式 GB/T 7714	Zhiming Zhou,Zhen Liu,Yi Pan,et al. Controller Design and Stability Analysis for Spinning Missile Via Tensor Product[J]. Aerospace Science and Technology,2022:107877.
APA	Zhiming Zhou,Zhen Liu,Yi Pan,&Jianqiang Yi.(2022).Controller Design and Stability Analysis for Spinning Missile Via Tensor Product.Aerospace Science and Technology,107877.
MLA	Zhiming Zhou,et al."Controller Design and Stability Analysis for Spinning Missile Via Tensor Product".Aerospace Science and Technology (2022):107877.

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