Saddle Point of Orbital Pursuit-Evasion Game under J2-Perturbed Dynamics

No AccessEngineering NotesSaddle Point of Orbital Pursuit-Evasion Game Under J2-Perturbed DynamicsZhen-yu Li, Hai Zhu, Zhen Yang and Ya-zhong LuoZhen-yu LiNational University of Defense Technology, Changsha 410073, People's Republic of China, Hai ZhuNational University of Defense Technology, Changsha 410073, People's Republic of China, Zhen YangNational University of Defense Technology, Changsha 410073, People's Republic of China and Ya-zhong LuoNational University of Defense Technology, Changsha 410073, People's Republic of ChinaPublished Online:14 Jul 2020https://doi.org/10.2514/1.G004459SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Basar T. and Olsder G. J., Dynamic Noncooperative Game Theory, Soc. for Industrial and Applied Mathematics, Philadelphia, 1999, pp. 17–23. Google Scholar[2] Isaacs R., Differential Games, Wiley, New York, 1965, pp. 278–280. 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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 eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAlgorithms and Data StructuresAstronomyCelestial Coordinate SystemCelestial MechanicsComputer Programming and LanguageComputing and InformaticsComputing, Information, and CommunicationData ScienceEvolutionary AlgorithmOptimization AlgorithmPlanetary Science and ExplorationPlanetsRoboticsRobotsSpace Science and Technology KeywordsLagrange MultipliersEarthPontryagin's Maximum PrincipleExhaust VelocityParticle Swarm OptimizationArgument of LatitudeNonlinear DynamicsOrbital ElementsOptimization AlgorithmBoundary Value ProblemsAcknowledgmentsThe authors acknowledge financial support from the National Natural Science Foundation of China (grants numbers 11572345 and 11972044).PDF Received14 April 2019Accepted15 June 2020Published online14 July 2020