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• W4306869349 abstract "No AccessEngineering NotesDynamic Modeling and Distributed Control of Asymmetric Flexible SpacecraftKai Cao, Shuang Li, YinKang Li and Ming XinKai CaoNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China*Ph.D. Candidate, Department of Astronautics Engineering.Search for more papers by this author, Shuang Li https://orcid.org/0000-0001-9142-5036Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China†Professor, Department of Astronautics Engineering; . Member AIAA (Corresponding Author).Search for more papers by this author, YinKang LiNanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China*Ph.D. Candidate, Department of Astronautics Engineering.Search for more papers by this author and Ming Xin https://orcid.org/0000-0002-9947-6986University of Missouri, Columbia, Missouri 65211‡Professor, Department of Mechanical and Aerospace Engineering; . Associate Fellow AIAA.Search for more papers by this authorPublished Online:20 Oct 2022https://doi.org/10.2514/1.G006919SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Cao K., Li S., She Y. C., Biggs J. D., Liu Y. F. and Bian L. L., “Dynamics and On-Orbit Assembly Strategies for an Orb-Shaped Solar Array,” Acta Astronautica, Vol. 178, Jan. 2021, pp. 881–893. https://doi.org/10.1016/j.actaastro.2020.10.030 CrossrefGoogle Scholar[2] Meirovitch L., Fundamentals of Vibrations, McGraw–Hill, Boston, 2008, Chap. 8. Google Scholar[3] Gao H. J. and He W., “Modeling and Neural Network Control of a Flexible Beam with Unknown Spatiotemporally Varying Disturbance Using Assumed Mode Method,” Neurocomputing, Vol. 314, Nov. 2018, pp. 458–467. https://doi.org/10.1016/j.neucom.2018.06.039 Google Scholar[4] Liu H., Guo L. and Zhang Y. 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M., Salarieh H., Pishkenari H. N. and Jalili H., “Boundary Control Design for Vibration Suppression and Attitude Control of Flexible Satellites with Multi-Section Appendages,” Acta Astronautica, Vol. 173, Aug. 2020, pp. 22–30. https://doi.org/10.1016/j.actaastro.2020.04.001 CrossrefGoogle Scholar[28] Liu Y., Fu Y., He W. and Hui Q., “Modeling and Observer-Based Vibration Control of a Flexible Spacecraft With External Disturbances,” IEEE Transactions on Industrial Electronics, Vol. 66, No. 11, 2019, pp. 8648–8658. https://doi.org/10.1109/TIE.2018.2884172 Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 46, Number 1January 2023 CrossmarkInformationCopyright © 2022 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. AcknowledgmentsThis work was partially supported by the National Natural Science Foundation of China (Grant No. 11972182), and sponsored by Qing Lan Project, Postgraduate Research & Practice Innovation Program of Jiangsu Province (Grant No. KYCX21_0233). The authors fully appreciate their financial support. The authors would like to thank Xiaowei Zhang for his help during the revision process of the paper.PDF Received26 April 2022Accepted22 August 2022Published online20 October 2022" @default.
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