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Published on: October 3, 2018
Characteristic Study of a Typical Satellite Solar Panel under Mechanical Vibrations
Xin Shen1, Yipeng Wu1, Quan Yuan1
1State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.
Mechanical vibration significantly degrades solar photovoltaic (PV) wing performance on spacecraft. This study shows vibration reduces maximum output power by 5.53% and lowers the fill factor, impacting energy conversion efficiency.
Area of Science:
- Spacecraft engineering
- Materials science
- Electrical engineering
Background:
- Photovoltaic (PV) power generation is crucial for spacecraft energy.
- Mechanical vibrations from uncertain factors and unbalanced forces degrade PV wing performance during on-orbit operations.
Purpose of the Study:
- To investigate the impact of mechanical vibration on the output characteristics of solar PV array systems.
- To analyze the dynamic response and electrical output of a three-segment solar panel under vibration.
Main Methods:
- Numerical simulation software was employed to model a three-segment solar panel.
- Dynamic response and electrical output characteristics under mechanical vibration were analyzed.
- Simulation model correctness was validated through partial experimental confirmation.
Main Results:
- A maximum output power reduction of 5.53% was observed.
- The fill factor declined from 0.8031 to 0.7587 under specific vibration conditions (10 N/m², 0.3754 Hz, 74.9871° deflection).
Conclusions:
- Mechanical vibration significantly decreases the maximum output power and fill factor of solar panels.
- Overall energy conversion efficiency of solar panels is notably reduced when operating under vibration conditions.
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