Impact Time and Angle Control Optimal Guidance with Field-of-View Constraint

No AccessEngineering NotesImpact Time and Angle Control Optimal Guidance with Field-of-View ConstraintYe Chen, Shufan Wu and Xiaoliang WangYe Chen https://orcid.org/0000-0003-1221-7111Shanghai Jiao Tong University, 200240 Shanghai, People's Republic of China, Shufan WuShanghai Jiao Tong University, 200240 Shanghai, People's Republic of China and Xiaoliang Wang https://orcid.org/0000-0003-4345-1613Shanghai Jiao Tong University, 200240 Shanghai, People's Republic of ChinaPublished Online:26 Sep 2022https://doi.org/10.2514/1.G007030SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Jeon I.-S., Lee J.-I. and Tahk M.-J., "Impact-Time-Control Guidance Law for Anti-Ship Missiles," IEEE Transactions on Control Systems Technology, Vol. 14, No. 2, 2006, pp. 260–266. https://doi.org/10.1109/TCST.2005.863655 CrossrefGoogle Scholar[2] Cho N. and Kim Y., "Modified Pure Proportional Navigation Guidance Law for Impact Time Control," Journal of Guidance, Control, and Dynamics, Vol. 39, No. 4, 2016, pp. 852–872. https://doi.org/10.2514/1.G001618 LinkGoogle Scholar[3] Hu Q., Han T. and Xin M., "Sliding-Mode Impact Time Guidance Law Design for Various Target Motions," Journal of Guidance, Control, and Dynamics, Vol. 42, No. 1, 2019, pp. 136–148. https://doi.org/10.2514/1.G003620 LinkGoogle Scholar[4] Kim H.-G., Cho D. and Kim H. 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E., Ho Y. C. and Siouris G. M., "Applied Optimal Control: Optimization, Estimation, and Control," IEEE Transactions on Systems Man and Cybernetics, Vol. 9, No. 6, 1979, pp. 366–367. https://doi.org/10.1109/TSMC.1979.4310229 Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 45, Number 12December 2022 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 supported by the Shanghai Academy of Spaceflight Technology and Shanghai Jiao Tong University (SAST-SJTU) Advanced Space Technology Joint Research Fund under Grant Nos. USCAST2020-8 and USCAST2020-20, and the National Natural Science Foundation of China under Grant No. U20B2054.PDF Received9 June 2022Accepted13 August 2022Published online26 September 2022