Robust Incremental Learning of Approximate Dynamic Programming for Nonlinear Optimal Guidance

IF 5.7 2区 计算机科学 Q1 ENGINEERING, AEROSPACE IEEE Transactions on Aerospace and Electronic Systems Pub Date : 2025-01-08 DOI:10.1109/TAES.2025.3525609
Han Wang;Lin Cheng;Shengping Gong;Xu Huang
{"title":"Robust Incremental Learning of Approximate Dynamic Programming for Nonlinear Optimal Guidance","authors":"Han Wang;Lin Cheng;Shengping Gong;Xu Huang","doi":"10.1109/TAES.2025.3525609","DOIUrl":null,"url":null,"abstract":"Existing nonlinear guidance methods are difficult to reconcile performance optimality with stability assurance. This study proposes a concept of robust incremental learning for approximate optimal control of nonlinear terminal guidance problems. It transitions incrementally and stably from a traditional analytically formulated guidance law to an approximate optimal guidance policy. Specifically, we propose an incremental policy iteration algorithm, where a base guidance law is utilized to mitigate the initial instability and warm-start the learning process. Then, a robustness enhancement technique is proposed to theoretically guarantee the stability of learning process, where the guidance command is refined leveraging a virtual Lyapunov-based energy function. As a result, a robust and efficient learning method for nonlinear optimal guidance problems is developed. Simulation results for a specific impact-angle-constrained guidance problem verify advantages of the proposed method on efficiency, stability, and optimality.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 3","pages":"6041-6052"},"PeriodicalIF":5.7000,"publicationDate":"2025-01-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace and Electronic Systems","FirstCategoryId":"94","ListUrlMain":"https://ieeexplore.ieee.org/document/10833863/","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

Existing nonlinear guidance methods are difficult to reconcile performance optimality with stability assurance. This study proposes a concept of robust incremental learning for approximate optimal control of nonlinear terminal guidance problems. It transitions incrementally and stably from a traditional analytically formulated guidance law to an approximate optimal guidance policy. Specifically, we propose an incremental policy iteration algorithm, where a base guidance law is utilized to mitigate the initial instability and warm-start the learning process. Then, a robustness enhancement technique is proposed to theoretically guarantee the stability of learning process, where the guidance command is refined leveraging a virtual Lyapunov-based energy function. As a result, a robust and efficient learning method for nonlinear optimal guidance problems is developed. Simulation results for a specific impact-angle-constrained guidance problem verify advantages of the proposed method on efficiency, stability, and optimality.
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
非线性最优制导的近似动态规划鲁棒增量学习
现有的非线性制导方法难以兼顾性能最优性和稳定性保证。本文提出了一种鲁棒增量学习的概念,用于非线性末端制导问题的近似最优控制。它从传统的解析式制导律逐步稳定地过渡到近似最优制导策略。具体而言,我们提出了一种增量策略迭代算法,该算法利用基本制导律来减轻初始不稳定性并热启动学习过程。然后,提出了一种鲁棒性增强技术,利用基于lyapunov的虚拟能量函数对制导命令进行细化,从理论上保证了学习过程的稳定性。为非线性最优制导问题提供了一种鲁棒、高效的学习方法。仿真结果验证了该方法在效率、稳定性和最优性方面的优势。
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
CiteScore
7.80
自引率
13.60%
发文量
433
审稿时长
8.7 months
期刊介绍: IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.
期刊最新文献
Fault-Tolerant Technology for Satellite-Borne Linux OS in Intelligent Computing: Dynamic Triple-Shielding Architecture (DTA) Magnetic-Inertial Orientation Estimation by Partial-state Updating Optimization A Dual PHD Filter for Multiple Slow Move-Stop-Move Targets Hidden in the Doppler Blind Zone Online Anti-Jamming Decision-Making for Frequency-Agile Radar in Non-Stationary Environments NUFFT-Extended Keystone Transform for Efficient Long-Time Coherent Integration in Hypersonic Target Detection
×
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:604180095
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