Engineering Test Satellite, ETS-8, large deployable reflector, solar array paddle, large space structure, satellite attitude control, satellite configuration, solar array
その他のタイトル（英）
On-orbit system identification experiments of ETS-8
Japan Aerospace Exploration Agency Structure Technology Center, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Structure Technology Center, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Structure Technology Center, Institute of Aerospace Technology
Japan Aerospace Exploration Agency Institute of Aerospace Technology
Japan Aerospace Exploration Agency Institute of Aerospace Technology
Japan Aerospace Exploration Agency Institute of Aerospace Technology
Japan Aerospace Exploration Agency
Japan Aerospace Exploration Agency
Japan Aerospace Exploration Agency
JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
巻
JAXA-SP-06-006
ページ
241 - 246
発行年
2006-11-01
抄録（英）
This report describes the studies on the on-orbit system identification experiments using ETS-8 (Engineering Test Satellite 8). ETS-8 will be launched by H-2A launch vehicle in fiscal year 2006. ETS-8 has large-scale, flexible Large Deployable Reflectors and Solar Array Paddles. The results of the on-orbit system identification experiments evaluate the on-orbit flexible characteristics and contribute to the design of the control system for the next large satellite. The establishment of the robust attitude control technology for large-scale flexible satellite is aimed at through the attitude control experiment.
ETS-8軌道上同定実験
49500053.pdf
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