Solar array and interrupt method, solar array drive circuit, device and system
By designing a vacuum dual-winding two-phase stepper motor and a main/backup drive circuit, combined with an MCU module and a Hall signal conditioning circuit, the stability and reliability issues of the solar panel drive device in the space environment were solved, enabling rapid solar orientation and multiple operating modes, meeting the design requirements of low cost, small size, and low weight.
Patent Information
- Application Number
- CN202310203239.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2023-03-06
- Publication Date
- 2026-07-24
- Estimated Expiration
- 2043-03-06
AI Technical Summary
Existing solar panel drive devices are difficult to achieve stable and reliable directional operation in the space environment, and the design of ground equipment is not suitable for the high and low temperature, vacuum and radiation conditions of the space environment, and cannot meet the requirements of low cost, small size, low weight and vibration and shock resistance.
It adopts a vacuum dual-winding two-phase stepper motor, with main and backup drive circuits designed. Combined with MCU module, PWM generation module and Hall signal conditioning circuit, it realizes real-time modulation drive and position information acquisition, has main and backup switching function, and supports multiple working modes and temperature data monitoring.
It achieves rapid sun orientation with high reliability and high positioning accuracy, improves the stability and reliability of SADA, meets the requirements of the space environment, collects zero-position information and temperature data in real time, and is suitable for low-cost, small-volume and low-weight designs.