TY - GEN
T1 - Orbital Maneuver Evaluation of Micro-satellite ALE-1 with a Separable Drag Sail
AU - Pala, Alperen
AU - Kuwahara, Toshinori
AU - Takeda, Kohei
AU - Shibuya, Yoshihiko
AU - Sato, Yuji
AU - Fujita, Shinya
AU - Suzuki, Daisuke
AU - Kaneko, Tetsuya
N1 - Funding Information:
This project is supported by Innovative Satellite Technology Demonstration Program of JAXA.
Publisher Copyright:
© 2022 IEEE.
PY - 2022
Y1 - 2022
N2 - 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.
AB - 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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U2 - 10.1109/SII52469.2022.9708783
DO - 10.1109/SII52469.2022.9708783
M3 - Conference contribution
AN - SCOPUS:85126267742
T3 - 2022 IEEE/SICE International Symposium on System Integration, SII 2022
SP - 877
EP - 881
BT - 2022 IEEE/SICE International Symposium on System Integration, SII 2022
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2022 IEEE/SICE International Symposium on System Integration, SII 2022
Y2 - 9 January 2022 through 12 January 2022
ER -