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

被引：1

作者：

Pala, Alperen ^{[1
]}

Kuwahara, Toshinori ^{[1
]}

Takeda, Kohei ^{[1
]}

Shibuya, Yoshihiko ^{[1
]}

Sato, Yuji ^{[1
]}

Fujita, Shinya ^{[1
]}

Suzuki, Daisuke ^{[2
]}

Kaneko, Tetsuya ^{[3
]}

机构：

[1] Tohoku Univ, Dept Aerosp Engn, Sendai, Miyagi, Japan

[2] ALE Co Ltd, Tokyo, Japan

[3] Nakashimada Engn Works Ltd, Hirokawa, Japan

来源：

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

关键词：

D O I：

10.1109/SII52469.2022.9708783

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

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.

引用

页码：877 / 881

页数：5

共 26 条

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