@inproceedings{oai:jaxa.repo.nii.ac.jp:00007312,
 author = {坂東, 麻衣 and 山川, 宏 and Bando, Mai and Yamakawa, Hiroshi},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, 摘要:本研究では.宇宙機の非線形運動を直接扱い,最適軌道を構築する方法について考察する.Guibout and Scheeres(2004)で提案された母関数による軌道最適化のアプローチを用いた2点境界値問題の解法と複数フライバイ問題への応用について議論する., In this paper, we consider a new low-thrust trajectory optimization method to find the optimal trajectory subject to the original nonlinear system in analytical form. We employ the generating functions approach proposed by Guibout and Scheeres(2004) and investigate its application to multiple flyby mission., 資料番号: AA0064734007},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {Application of Global Solution of Hamilton-Jacobi Equations to Nonlinear Trajectory Optimization of Spacecraft},
 volume = {2009},
 year = {2010}
}