Title: Optimal Formation Reconfigurations Subject to Hill Three-Body Dynamics
Abstract: No AccessEngineering NoteOptimal Formation Reconfigurations Subject to Hill Three-Body DynamicsChandeok Park, Ji Hyun Yang and Daniel J. ScheeresChandeok ParkDepartment of Astronomy & Yonsei University Observatory, Yonsei University, Seoul 120-749, Republic of Korea, Ji Hyun YangDepartment of Automotive Engineering, Kookmin University, Seoul 136-702, Republic of Korea and Daniel J. ScheeresDepartment of Aerospace Engineering Sciences, University of Colorado, Boulder, Colorado 80309-0429Published Online:21 Feb 2014https://doi.org/10.2514/1.60944SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations About References [1] Guibout V. and Scheeres D. J., "Solving Relative Two Point Boundary Value Problems: Applications to Spacecraft Formation Flight Transfers," Journal of Guidance, Control, and Dynamics, Vol. 27, No. 4, 2004, pp. 693–704. doi:https://doi.org/10.2514/1.11164 JGCDDT 0162-3192 LinkGoogle Scholar[2] Park C., Guibout V. M. and Scheeres D. 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Publication Year: 2014
Publication Date: 2014-03-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 4
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