- Article
Output Feedback Control for Spacecraft Attitude System with Practical Predefined-Time Stability Based on Anti-Windup Compensator
- Nguyen Xuan-Mung,
- Mehdi Golestani,
- Huu Tiep Nguyen,
- Ngoc Anh Nguyen and
- Afef Fekih
This paper investigates the problem of output feedback attitude control for rigid spacecraft subject to inertia matrix uncertainty, space disturbance, and input saturation. Firstly, a model transformation is adopted to convert an attitude system with...