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- W4220785859 abstract "ALE Co., Ltd, and the Space Robotics Laboratory (SRL) in Tohoku University are actively developing the 3U CubeSat ALE-EDT. The mission of this nanosatellite is demonstrating the world-first device for Post Mission Disposal (PMD) using Electrodynamic Tether (EDT) and Carbon nanotube (CNT) cathode, contributing to prevention of the spread of space debris for sustainable space utilization. To achieve the mission, the attitude of this satellite must be stable throughout the EDT deployment sequence, although the tension causes a disturbance to the satellite when EDT is fully extended. Therefore, it is necessary the tether release angle should be properly controlled and should be robust against disturbances. In this paper, we present the design of Attitude Control System (ACS) for this spacecraft and attitude control strategy to conduct the mission successfully. The evaluation of the ACS was conducted by the Satellite and Space Environment Simulator (SSES) established by the SRL. By simulations with SSES, the validity of the ACS was confirmed." @default.
- W4220785859 created "2022-04-03" @default.
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- W4220785859 date "2022-01-09" @default.
- W4220785859 modified "2023-09-26" @default.
- W4220785859 title "Attitude Control System Design of 3U CubeSat with Electrodynamic Tether for Post Mission Disposal Demonstration" @default.
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- W4220785859 doi "https://doi.org/10.1109/sii52469.2022.9708853" @default.
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