Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)
雑誌名
アストロダイナミクスシンポジウム講演後刷り集
雑誌名(英)
Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics
Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan
In this paper, we discuss attitude control of a satellite from the minimum fuel point of view. We derive equations of relative motion between a desired attitude motion and the present attitiude motion, and consider its stabilization. We design a linear feedback controller based on the linearizied equations of relative motion around the origin. The main perforamance index is the L(sub 1) norm of the feedback controller.
Attitude Control of an Axisymmetric Spinning Satellite
