論文

査読有り
2004年10月

Computation of low energy Earth-to-Moon transfers with moderate flight time

PHYSICA D-NONLINEAR PHENOMENA
  • K Yagasaki

197
3-4
開始ページ
313
終了ページ
331
記述言語
英語
掲載種別
研究論文(学術雑誌)
DOI
10.1016/j.physd.2004.07.005
出版者・発行元
ELSEVIER SCIENCE BV

We consider a problem of constructing a spacecraft transfer trajectory with low cost and moderate flight time from the Earth to the Moon. We adopt the planar circular restricted three-body problem (PCR3BP) as the spacecraft model, and reduce computation of optimal transfers to a nonlinear boundary value problem (BVP). Using a computer software called AUTO, we numerically solve the nonlinear BVP and continue its solutions to obtain optimal transfers. Especially, we find a transfer trajectory having the same cost but 22% shorter flight time or having 7.5% lower cost, compared to the traditional Hohmann type transfer. Moreover, we show that these transfers are unstable in an appropriate meaning and closely relate to chaotic dynamics of the PCR3BP. (C) 2004 Elsevier B.V. All rights reserved.

リンク情報
DOI
https://doi.org/10.1016/j.physd.2004.07.005
Web of Science
https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=JSTA_CEL&SrcApp=J_Gate_JST&DestLinkType=FullRecord&KeyUT=WOS:000224441300008&DestApp=WOS_CPL
ID情報
  • DOI : 10.1016/j.physd.2004.07.005
  • ISSN : 0167-2789
  • Web of Science ID : WOS:000224441300008

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