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65424000.pdf4.93 MB
titleIn-orbit Control Experiment on ETS-VIII Spacecraft
Author(eng)ETS-VIII In-orbit Attitude Control Experiment Team
Author Affiliation(jpn)宇宙航空研究開発機構 (JAXA) : 電気通信大学
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA) : University of Electro-Communications (UEC)
Issue Date2012-09-30
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構研究開発報告
JAXA Research and Development Report
Start page1
End page104
Publication date2012-09-30
AbstractThis paper describes an in-orbit attitude control experiment carried out on ETS (Engineering Test Satellite)-VIII in June 2009 and March 2010. This experiment aims to develop a technical basis for the attitude control of a class of future large flexible spacecraft. Four novel robust control laws were developed and tested through the experiment; DVDFB (Direct Velocity and Displacement FeedBack) control law, DDFB (Dynamic Displacement FeedBack) control law, micro-synthesis based control law, and linearly interpolated gain scheduling law. Experimental results of each control law are presented to show its high control performance compared with a conventional control law.
DescriptionPhysical characteristics: Original contains color illustrations
形態: カラー図版あり
Document TypeTechnical Report
JAXA Category研究開発報告
Report NoJAXA-RR-12-002E

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