Design, Implementation and In-orbit Demonstration of Attitude and Orbit Control System for Micro-satellite ALE-2-Reference-Cited by-同舟云学术

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Design, Implementation and In-orbit Demonstration of Attitude and Orbit Control System for Micro-satellite ALE-2

Published:2021-01-11 Issue: Volume: Page:
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Container-title:2021 IEEE/SICE International Symposium on System Integration (SII)
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Author:

Sato Yuji,Fujita Shinya,Kuwahara Toshinori,Shibuya Yoshihiko,Kamachi Koh

Funder

Tohoku University

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9382420/9382486/09382731.pdf?arnumber=9382731

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Safe Attitude and Orbit Control for ISS-Deployed CubeSat HOKUSHIN-1 with Cold-Gas Propulsion System;2024 IEEE/SICE International Symposium on System Integration (SII);2024-01-08

2. High Accuracy Pointing Control Using a MEMS Mirror for a Micro Space Telescope;2024 IEEE/SICE International Symposium on System Integration (SII);2024-01-08

3. Attitude and Orbit Control Strategy with 10N Thruster for ALE-3;2023 IEEE/SICE International Symposium on System Integration (SII);2023-01-17

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