Moon Tracking Attitude Control Experiment of a Bias Momentum Micro Satellite “μ-LabSat”
スポンサーリンク
概要
- 論文の詳細を見る
A micro-piggyback satellite, “μ-LabSat”, was launched by an H-IIA rocket on 14 December 2002. μ-LabSat is a bias momentum micro-satellite with two wheels, a configuration that is not normally capable of three-axis attitude maneuvers. This paper describes an algorithm that has been developed to enable such maneuvers and presents the results of its evaluation by numerical simulation and in-orbit experiment.
- 社団法人 日本航空宇宙学会の論文
著者
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YAMAMOTO Toru
Japan Nuclear Energy Safety Organization
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TERUI Fuyuto
Japan Aerospace Exploration Agency
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NAKASUKA Shinichi
Department of Aeronautics and Astronautics, the University of Tokyo
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Nakasuka S
Department Of Aeronautics And Astronautics The University Of Tokyo
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KIMURA Shinichi
National Institute of Information and Communications Technology
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NAGAI Yasufumi
National Institute of Information and Communications Technology
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YAMAMOTO Hiroshi
National Institute of Information and Communications Technology
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YOSHIHARA Keisuke
Japan Aerospace Exploration Agency
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