- Article
Modeling and Analysis of Micro-Spacecraft Attitude Sensing with Gyrowheel
- Xiaokun Liu,
- Hui Zhao,
- Yu Yao and
- Fenghua He
This paper proposes two kinds of approaches of angular rate sensing for micro-spacecraft with a gyrowheel (GW), which can combine attitude sensing with attitude control into one single device to achieve a compact micro-spacecraft design. In this impl...