Author:
YOHDA Kazuhisa,SAHARA Hironori
Publisher
Japan Society for Aeronautical and Space Sciences
Reference4 articles.
1. Design and Control of Approach Trajectory by Impulsive Velocity Change
2. 2) Prussing, J. E.: Optimal Multiple-Impulse Orbital Rendezvous, Sc. D. Thesis, Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology, 1967.
3. 3) Suzuki, N. and Sahara, H.: Generalized Mono/Bi-Propellant Propulsion System for Microsatellite Based on Non-Toxic Propellant Technology, 46th AIAA/ASME/ASEE Joint Propulsion Conference & 8th Exhibit, 95-LP-12, 2010.
4. 4) 軍縮.不拡散促進センター: 新たな宇宙環境と軍備管理を含めた宇宙利用の規制-新たなアプローチと枠組みの可能性-,平成21年度外務省委託研究,日本国際問題研究所,2010.