@inproceedings{oai:jaxa.repo.nii.ac.jp:00007506,
 author = {山川, 宏 and 船木, 一幸 and Yamakawa, Hiroshi and Funaki, Ikko},
 book = {第16回アストロダイナミクスシンポジウム講演後刷り集　2006, Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {地球周回低軌道上にレーザー源を想定し、そのレーザーを受けることにより加速される宇宙機の軌道ダイナミクスについて考察する。Clohessy-Wiltshire方程式を用いて、積分量としての仮想的なエネルギー保存が成立することなどを示す。, This paper investigates the dynamics of an active space vehicle or a passive object around an orbiting station, assuming a laser-propelled system from the orbiting station. The linear rendezvous equations, Clohessy-Wiltshire equations, are used for the analysis. The objective is to gain insights into the requirements for thrust magnitude, thrust vector control, trajectory design, and feasible laser-propelled system design for application to space vehicle transfer., 資料番号: AA0063481005},
 pages = {28--31},
 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/ISAS)},
 title = {Orbital dynamics of laser-propelled space vehicle from orbiting laser station},
 year = {2007}
}