磁盘卫星质量矩姿态控制方法
By combining a differential tracker and a PD controller with a linear or nonlinear state observer, the aerodynamic torque of the centroid of the disk satellite is adjusted, solving the problem of complex disturbances in the attitude control of the disk satellite and achieving high-precision and low-cost attitude control.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- HARBIN INST OF TECH
- Filing Date
- 2024-07-08
- Publication Date
- 2026-07-17
AI Technical Summary
Attitude control of disk satellites faces complex disturbances. Traditional methods fail to effectively consider the additional torque caused by the slider motion and the model perturbation caused by the irregular aerodynamic shape, making it difficult to achieve high-precision attitude control.
By employing a differential tracker and a PD controller combined with a linear or nonlinear state observer, the satellite's center of mass is adjusted through the displacement of the mass block, and active control is achieved using aerodynamic torque to suppress disturbances and improve robustness.
It effectively suppressed complex disturbances, improved the accuracy and robustness of satellite attitude control, and reduced fuel consumption and the complexity of the control system.
Smart Images
Figure CN118618635B_ABST