Spatial–temporal cooperative guidance with no-fly zones avoidance

IF 5.4 2区 计算机科学 Q1 AUTOMATION & CONTROL SYSTEMS Control Engineering Practice Pub Date : 2024-11-15 DOI:10.1016/j.conengprac.2024.106162
Kai Zhao , Jia Song , Yang Liu
{"title":"Spatial–temporal cooperative guidance with no-fly zones avoidance","authors":"Kai Zhao ,&nbsp;Jia Song ,&nbsp;Yang Liu","doi":"10.1016/j.conengprac.2024.106162","DOIUrl":null,"url":null,"abstract":"<div><div>This paper proposes a three-dimensional spatial–temporal cooperative guidance law for striking maneuvering targets, with consideration of no-fly zones avoidance. A fixed-time convergent integral sliding mode guidance law based on a second-order system consensus protocol is proposed to ensure the consistency of the remaining distance and radial relative velocity, instead of using estimates of time-to-go based on small angle assumptions. In the elevation and azimuth directions, to mitigate excessive guidance commands during the initial phase, a nonlinear sliding surface and a finite-time reaching law are designed to meet impact angle constraints. In addition, considering the stagnation points escape in the process of no-fly zones avoidance an integrated cooperation and obstacle avoidance guidance law is proposed, which effectively avoids no-fly zones, accelerates the convergence speed of cooperative consistency, and reduces terminal errors. Using Lyapunov’s theory, this paper theoretically proves the fixed-time and finite-time convergence characteristics of the proposed algorithm. Simulation results indicate that the miss distance and terminal elevation and azimuth angle errors of the proposed algorithm are 55.04%, 27.5%, and 81.75% of those of the comparison algorithm, respectively.</div></div>","PeriodicalId":50615,"journal":{"name":"Control Engineering Practice","volume":"154 ","pages":"Article 106162"},"PeriodicalIF":5.4000,"publicationDate":"2024-11-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Control Engineering Practice","FirstCategoryId":"94","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0967066124003216","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"AUTOMATION & CONTROL SYSTEMS","Score":null,"Total":0}
引用次数: 0

Abstract

This paper proposes a three-dimensional spatial–temporal cooperative guidance law for striking maneuvering targets, with consideration of no-fly zones avoidance. A fixed-time convergent integral sliding mode guidance law based on a second-order system consensus protocol is proposed to ensure the consistency of the remaining distance and radial relative velocity, instead of using estimates of time-to-go based on small angle assumptions. In the elevation and azimuth directions, to mitigate excessive guidance commands during the initial phase, a nonlinear sliding surface and a finite-time reaching law are designed to meet impact angle constraints. In addition, considering the stagnation points escape in the process of no-fly zones avoidance an integrated cooperation and obstacle avoidance guidance law is proposed, which effectively avoids no-fly zones, accelerates the convergence speed of cooperative consistency, and reduces terminal errors. Using Lyapunov’s theory, this paper theoretically proves the fixed-time and finite-time convergence characteristics of the proposed algorithm. Simulation results indicate that the miss distance and terminal elevation and azimuth angle errors of the proposed algorithm are 55.04%, 27.5%, and 81.75% of those of the comparison algorithm, respectively.
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
时空协同制导,避开禁飞区
本文提出了一种用于打击机动目标的三维时空协同制导法则,并考虑了禁飞区规避问题。本文提出了一种基于二阶系统共识协议的固定时间收敛积分滑模制导法则,以确保剩余距离和径向相对速度的一致性,而不是使用基于小角度假设的到达时间估计值。在仰角和方位角方向,为减少初始阶段过多的制导指令,设计了非线性滑动面和有限时间到达法,以满足撞击角约束。此外,考虑到避开禁飞区过程中的停滞点逃逸,提出了合作与避障一体化制导法则,有效地避开了禁飞区,加快了合作一致性的收敛速度,减少了终端误差。本文利用李亚普诺夫理论,从理论上证明了所提算法的定时收敛特性和有限时间收敛特性。仿真结果表明,所提算法的失误距离、终端仰角和方位角误差分别是对比算法的 55.04%、27.5% 和 81.75%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
Control Engineering Practice
Control Engineering Practice 工程技术-工程:电子与电气
CiteScore
9.20
自引率
12.20%
发文量
183
审稿时长
44 days
期刊介绍: Control Engineering Practice strives to meet the needs of industrial practitioners and industrially related academics and researchers. It publishes papers which illustrate the direct application of control theory and its supporting tools in all possible areas of automation. As a result, the journal only contains papers which can be considered to have made significant contributions to the application of advanced control techniques. It is normally expected that practical results should be included, but where simulation only studies are available, it is necessary to demonstrate that the simulation model is representative of a genuine application. Strictly theoretical papers will find a more appropriate home in Control Engineering Practice''s sister publication, Automatica. It is also expected that papers are innovative with respect to the state of the art and are sufficiently detailed for a reader to be able to duplicate the main results of the paper (supplementary material, including datasets, tables, code and any relevant interactive material can be made available and downloaded from the website). The benefits of the presented methods must be made very clear and the new techniques must be compared and contrasted with results obtained using existing methods. Moreover, a thorough analysis of failures that may happen in the design process and implementation can also be part of the paper. The scope of Control Engineering Practice matches the activities of IFAC. Papers demonstrating the contribution of automation and control in improving the performance, quality, productivity, sustainability, resource and energy efficiency, and the manageability of systems and processes for the benefit of mankind and are relevant to industrial practitioners are most welcome.
期刊最新文献
Physical-anchored graph learning for process key indicator prediction Predictive sliding mode control for flexible spacecraft attitude tracking with multiple disturbances Spatial–temporal cooperative guidance with no-fly zones avoidance Sliding-mode energy management strategy for dual-source electric vehicles handling battery rate of change of current Optimization of the energy-comfort trade-off of HVAC systems in electric city buses based on a steady-state model
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1