Art
J-GLOBAL ID：200902282174096306
Reference number：05A0463077
On Formation Deployment for Spinning Tethered Formation Flying
テザー連結型スピンフォーメーションフライングの隊列展開について
Author (2)：
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Material：
Volume：
53
Issue：
616
Page：
191-199
Publication year：
May. 05, 2005
JST Material Number：
L3565A
ISSN：
1344-6460
Document type：
Article
Article type：
原著論文
Country of issue：
Japan (JPN)
Language：
JAPANESE (JA)
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JST classification (1)：
JST classification
Category name(code) classified by JST.
Motion and orbit of space crafts
Reference (12)：
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1) Cobb, R., Das, A. and Denoyer, K.: TechSat 21: Developing Low-Cost, Highly Functional Micro-Satellite Clusters for 21st Century Air Force Missions, 50th Congress of the International Astronautical Federation, Amsterdam, The Netherlands, 1999.
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2) 森治,松永三郎:群型テザード衛星システムの回転運動制御,日本航空宇宙学会論文集,50 (2002), pp. 109–117.
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3) Mori, O., Nakaya, K., Maeda, N. and Matunaga, S.: Formation and Attitude Control of Tethered Satellite Cluster, 23rd International Symposium on Space Technology and Science, Matsue, Shimane, 2002-d-48, 2002.
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4) Tragesser, S. G.: Formation Flying with Tethered Spacecraft, AIAA/AAS Astrodynamics Specialist Conference, Denver, CO, AIAA Paper 2000-4133, 2000.
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5) DeCou, A. B.: Tether Static Shape for Rotating Multimass, Multitether, Spacecraft for ‘Triangle’ Michelson Interferometer, J. Guid. Control Dynam., 12 (1989), pp. 273–275.
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