Design of Magnetorquer-Based Attitude Control Subsystem for FORESAIL-1 Satellite

N. Jovanovic,B. Riwanto,P. Niemelä,M. Rizwan Mughal,J. Praks

IEEE Journal on Miniaturization for Air and Space Systems（2021）

引用 5|浏览9

暂无评分

摘要

The magnetorquer-based attitude control system capable of attaining high spin rates and precise pointing control is required for a 3U CubeSat satellite FORESAIL-1. The satellite, developed by the Finnish Centre of Excellence, needs to maintain a spin rate of 24°/s and precise pointing of the spin axis toward the Sun for the particle telescope instrument, as well as to reach 130°/s spin rate for th...

查看译文

关键词

Attitude control,Angular velocity,Plasmas,Magnetic moments,Magnetic circuits,Brakes,CubeSat

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