Optimal Midcourse Guidance for Dual-Pulse Rocket Using Pseudospectral Sequential Convex Programming

No AccessEngineering NotesOptimal Midcourse Guidance for Dual-Pulse Rocket Using Pseudospectral Sequential Convex ProgrammingBoseok Kim and Chang-Hun LeeBoseok Kim https://orcid.org/0000-0001-8897-2418Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea and Chang-Hun Lee https://orcid.org/0000-0002-0758-1974Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of KoreaPublished Online:26 May 2023https://doi.org/10.2514/1.G006882SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Cheng V. H. L. and Gupta N. K., "Advanced Midcourse Guidance for Air-to-Air Missiles," Journal of Guidance, Control, and Dynamics, Vol. 9, No. 2, 1986, pp. 135–142. https://doi.org/10.2514/3.20081 LinkGoogle Scholar[2] Sridhar B. and Gupta N. 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See also AIAA Rights and Permissions www.aiaa.org/randp. KeywordsOptimal Midcourse GuidanceDual-pulse RocketConvex ProgrammingComputational GuidanceLong Range Air-to-Air MissileAcknowledgmentsThis work was supported by Theater Defense Research Center funded by Defense Acquisition Program Administration under Grant UD200043CD.PDF Received7 April 2022Accepted16 April 2023Published online26 May 2023