Solving Pursuit/Evasion Game Along Elliptical Orbit by Providing Precise Gradient

No AccessEngineering NotesSolving Pursuit/Evasion Game Along Elliptical Orbit by Providing Precise GradientBo Pang, Changxuan Wen, Hongwei Han and Dong QiaoBo Pang https://orcid.org/0000-0003-3351-7041Beijing Institute of Technology, 100081 Beijing, People's Republic of China, Changxuan Wen https://orcid.org/0000-0002-2293-4395Beijing Institute of Technology, 100081 Beijing, People's Republic of China, Hongwei HanBeijing Institute of Technology, 100081 Beijing, People's Republic of China and Dong QiaoBeijing Institute of Technology, 100081 Beijing, People's Republic of ChinaPublished Online:4 Mar 2024https://doi.org/10.2514/1.G007025SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Isaacs R., Differential Games, Wiley, New York, 1965, pp. 278–280. Google Scholar[2] Chen R. H., Speyer J. 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All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerospace SciencesApplied MathematicsAstrodynamicsAstronauticsComputational Fluid DynamicsControl TheoryFluid DynamicsGeneral PhysicsGuidance, Navigation, and Control SystemsMathematical AnalysisNumerical AnalysisOptimal Control TheoryOrbital ManeuversSpace OrbitStructures, Design and Test KeywordsOrbital ManeuversNumerical IntegrationApplied MathematicsPontryagin's Maximum PrincipleLinear Quadratic RegulatorParticle Swarm OptimizationSatellitesDifferential EquationsOrbital Pursuit Evasion GameGradient MethodAcknowledgmentThis work was supported by the National Natural Science Foundation of China (grant numbers 11702293 and 12102037).Digital Received8 June 2022Accepted12 January 2024Published online4 March 2024