Orbital Maneuver Evaluation of Micro-satellite ALE-1 with a Separable Drag Sail

Alperen Pala,Toshinori Kuwahara,Kohei Takeda,Yoshihiko Shibuya,Yuji Sato,Shinya Fujita,Daisuke Suzuki,Tetsuya Kaneko

2022 IEEE/SICE INTERNATIONAL SYMPOSIUM ON SYSTEM INTEGRATION (SII 2022)（2022）

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摘要

ALE-1 is a microsatellite that needs to change its initial launch orbital altitude before its main mission can start. A passive de-orbiter system is used for this maneuver. This paper summarizes the history of this orbital maneuver sub-mission and the results of ALE-1's de-orbiting over the months since its launch. Furthermore, these results are compared to a simulation and the end date of this orbital maneuver is estimated.

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关键词

orbital maneuver evaluation,microsatellite ALE-1,separable drag sail,initial launch orbital altitude,passive de-orbiter system,orbital maneuver sub-mission

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