Safe Attitude and Orbit Control for ISS-Deployed CubeSat HOKUSHIN-1 with Cold-Gas Propulsion System.

Saki Komachi,Shinya Fujita, Kohei Takeda, Hayate Nakaoka,Toshinori Kuwahara,Kazuya Yoshida,Junichiro Kawaguchi

2024 IEEE/SICE International Symposium on System Integration (SII)(2024)

引用 0|浏览1
暂无评分
摘要
A compact propulsion system that can operate in a low-power and low-temperature environment is necessary to expand the field of activity of CubeSats from Earth orbit to deep space. Tohoku University, Hokkaido University, and Muroran Institute of Technology are developing the 3U CubeSat “HOKUSHIN-1” for future lunar exploration by CubeSats. For orbit maintenance and 3-axis attitude control, this satellite is equipped with a new 1U size cold gas propulsion system developed by Patchedconics, LLC, and is planned for technical demonstration on the ISS orbit. This paper proposes a system design and operation method to prevent hazards caused by malfunction of the propulsion system and to ensure safety during orbit operations. Furthermore, the attitude and orbit control capability of the new propulsion system is evaluated by numerical simulation.
更多
查看译文
关键词
Positive Control,Propulsion System,Orbit Control,Safe Attitudes,Numerical Simulations,Spaceborne,Open Method,Earth Orbit,Stage 2,Optimal Control,Angular Velocity,Major Axis,Satellite Orbit,Phase Period,Air Resistance,Ground Station,Satellite Position,Propellant,International Space Station,Waiting Period,Along-track Direction,Orbital Period,Propulsion Efficiency,Solenoid Valve,Altitude Difference,Solar Activity,Hazard Control,Worst-case Conditions
AI 理解论文
溯源树
样例
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要