一种空间站太阳翼驱动控制保护方法
By designing a three-layer protection method for the space station's solar array, including software, hardware, and transmission chain protection, the safety issues of large solar array drive control were solved, achieving comprehensive protection for the space station's solar array and ensuring its safety and reliability in emergency or malfunction situations.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- SHANGHAI AEROSPACE CONTROL TECH INST
- Filing Date
- 2022-12-26
- Publication Date
- 2026-07-17
AI Technical Summary
Existing technologies are insufficient to effectively protect the propulsion and control of the large solar arrays on the space station, especially in emergency or malfunction situations where there is a lack of comprehensive protection measures, resulting in inadequate safety.
A drive control and protection method for a space station solar array is designed, which includes software protection, hardware protection and transmission chain protection. The three-layer protection is combined and designed for the unique structure and load characteristics of the space station solar array. Specific measures include automatic shutdown after communication failure, motor overcurrent protection, brake overcurrent protection, clutch overcurrent protection, and transmission chain motion constraints.
It achieves comprehensive protection for the space station's solar panels, ensuring timely protection of the solar panels in emergency or malfunction situations to prevent damage and improving the safety and reliability of the solar panels.
Smart Images
Figure CN115973459B_ABST