Large Angle Attitude Control of Satellite Using Model Predictive Control
摘要
This paper designs a spacecraft attitude control model based on the adaptive model predictive control method. By establishing a model predictive control (MPC) controller to solve the spacecraft attitude dynamics model, the controller’s state is continuously adjusted to adapt to the spacecraft’s environmental constraints. A simulation model is constructed in MATLAB, and it is compared with the results of traditional PID control. The results demonstrate that MPC has better response speed and robustness for spacecraft attitude control, thus verifying the effectiveness of the algorithm.