solar sail, attitude control, rotation, control simulation, mathematical model, stability, spinning solar sail, control input, control response, tension, spin stabilization, multi-particle model, sympathetic vibration, electric propulsion, chemical propulsion
University of Tokyo
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
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/ISAS)
雑誌名
第16回アストロダイナミクスシンポジウム講演後刷り集 2006
雑誌名(英)
Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics
Solar sails are the spacecraft that are propelled by sunlight. At The Institute of Space and Astronomical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA), spinning solar sail is proposed. This type uses centrifugal force to maintain and deploy the membrane. Because it doesn't have the tube or mast to keep the membrane stable, there is a possibility of deformation and oscillation in changing the attitude. In this paper, control input to enable the stable attitude change is obtained by using numerical simulation.
A study on attitude control of spinning solar sail-craft
