Minimum-Time Rendezvous via Simplified Initial Costate Normalization and Auxiliary Orbital Transfer

规范化(社会学) 轨道机动 轨道力学 会合 计算机科学 传输(计算) 控制理论(社会学) 物理 应用数学 数学 航天器 并行计算 天文 人工智能 卫星 控制(管理) 社会学 人类学
作者
Guo Xiang,Di Wu,Fanghua Jiang
出处
期刊:Journal of Guidance Control and Dynamics [American Institute of Aeronautics and Astronautics]
卷期号:: 1-10 被引量:4
标识
DOI:10.2514/1.g007268
摘要

No AccessEngineering NotesMinimum-Time Rendezvous via Simplified Initial Costate Normalization and Auxiliary Orbital TransferXiang Guo, Di Wu and Fanghua JiangXiang Guo https://orcid.org/0000-0002-3288-8070Tsinghua University, 100084 Beijing, People's Republic of China, Di WuTsinghua University, 100084 Beijing, People's Republic of China and Fanghua JiangTsinghua University, 100084 Beijing, People's Republic of ChinaPublished Online:4 May 2023https://doi.org/10.2514/1.G007268SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Rayman M. D., Fraschetti T. C., Raymond C. A. and Russell C. 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L. and Taheri E., "Exploration of Alternative State Vector Choices for Low-Thrust Trajectory Optimization," Journal of Guidance, Control, and Dynamics, Vol. 42, No. 1, 2019, pp. 47–64. https://doi.org/10.2514/1.G003686 LinkGoogle Scholar[25] Gao Y. and Kluever C., "Low-Thrust Interplanetary Orbit Transfers Using Hybrid Trajectory Optimization Method with Multiple Shooting," AIAA/AAS Astrodynamics Specialist Conference and Exhibit, AIAA Paper 2004-5088, 2004. https://doi.org/10.2514/6.2004-5088 Google Scholar[26] Battin R. H., An Introduction to the Mathematics and Methods of Astrodynamics, AIAA, New York, 1999, pp. 191–236. Google Scholar[27] Lewis F. L., Vrabie D. and Syrmos V. L., Optimal Control, Wiley, Hoboken, NJ, 2012, pp. 213–259. Google Scholar[28] Taheri E., Arya V. and Junkins J. L., "Costate Mapping for Indirect Trajectory Optimization," Astrodynamics, Vol. 5, No. 4, 2021, pp. 359–371. https://doi.org/10.1007/s42064-021-0114-0 CrossrefGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Articles in Advance CrossmarkInformationCopyright © 2023 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. KeywordsLow ThrustMinimum-Time RendezvousSimplified Initial Costate NormalizationAuxiliary Orbital TransferAcknowledgmentsThis work was supported by the National Key R&D Program of China (Grant No. 2020YFC2201200) and the National Natural Science Foundation of China (Grant No. 12022214).PDF Received29 September 2022Accepted15 March 2023Published online4 May 2023

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