The paper presents a nonlinear H∞ state feedback for large angle attitude control of satellite. The dynamic equations of satellite with full-coupled body fixed canted attitude thruster control are derived. A nonlinear H∞ controller is designed to achieve stability and disturbance rejection for large angle maneuvers. The simulation results based on spacecraft system are presented to demonstrate the effectiveness of the proposed design method.
All Science Journal Classification (ASJC) codes
- Electrical and Electronic Engineering