Coverage-Based Cooperative Guidance Strategy by Controlling Flight Path Angle

北京 中国 航天学 章节(排版) 运筹学 图书馆学 计算机科学 工程类 政治学 航空学 法学 操作系统
作者
Bolun Zhang,Di Zhou,Junlong Li,Yuhan Yao
出处
期刊:Journal of Guidance Control and Dynamics [American Institute of Aeronautics and Astronautics]
卷期号:45 (5): 972-981 被引量:19
标识
DOI:10.2514/1.g006504
摘要

No AccessEngineering NotesCoverage-Based Cooperative Guidance Strategy by Controlling Flight Path AngleBolun Zhang, Di Zhou, Junlong Li and Yuhan YaoBolun ZhangHarbin Institute of Technology, 150001 Harbin, People's Republic of China, Di ZhouHarbin Institute of Technology, 150001 Harbin, People's Republic of China, Junlong LiBeijing Institute of Electronic System Engineering, 100190 Beijing, People's Republic of China and Yuhan YaoBeijing Institute of Electronic System Engineering, 100190 Beijing, People's Republic of ChinaPublished Online:31 Jan 2022https://doi.org/10.2514/1.G006504SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Murtaugh S. A. and Criel H. E., "Fundamentals of Proportional Navigation," IEEE Spectrum, Vol. 3, No. 12, 1966, pp. 75–85. https://doi.org/10.1109/MSPEC.1966.5217080 CrossrefGoogle Scholar[2] Zha W. Z., Chen J., Peng Z. H. and Gu D. 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R. and Maity A., "Finite-Horizon Robust Suboptimal Control-Based Impact Angle Guidance," IEEE Transactions on Aerospace and Electronic Systems, Vol. 56, No. 3, 2020, pp. 1955–1965. https://doi.org/10.1109/TAES.2019.2938126 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byCooperative Guidance Law for High-Speed and High-Maneuverability Air Targets8 February 2023 | Aerospace, Vol. 10, No. 2 What's Popular Volume 45, Number 5May 2022 CrossmarkInformationCopyright © 2021 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerospace SciencesAir NavigationControl TheoryFlight DynamicsGuidance, Navigation, and Control SystemsNavigational GuidanceOptimal Control Theory KeywordsFlight Path AngleState Dependent Riccati EquationGuidance LawsProbability Distribution FunctionsTarget MissilesAlgebraic Riccati EquationPolar Coordinate SystemMonte Carlo SimulationProportional NavigationTerminal GuidanceAcknowledgmentThis work is in part supported by the National Natural Science Foundation of China (grant 61773142).PDF Received11 October 2021Accepted18 December 2021Published online31 January 2022
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