微重力空间下微纳遥感卫星太阳翼构型仿真分析

针对微纳遥感卫星从技术试验阶段到业务化应用的转型发展，如何缓解其能量来源的受限条件，获取更高的太阳能充电效能，对微纳遥感卫星未来星座构建的发展需求有重要作为。通过设计不同构型的微纳卫星太阳翼，构造太阳电池阵列的仿真模型，根据太阳能电池阵列在微重力空间下的工作特性，仿真分析微重力空间下不同构型太阳翼的充电性能和充电效率，并对不同构型的使用性能进行了分析比较，结果表明，选择最优太阳翼构型能够为微纳遥感卫星提供更好的能源和动力支撑，为后续微纳遥感卫星开展更多商业应用提供有效参考。

Simulation Analysis on the Solar Panel of Remote Sensing CubeSat with different Structures in Microgravity Space

Remote sensing cubesat is in the transformation stage from technical test to business application, how to alleviate the energy limitation and obtain higher solar charging efficiency is important to the development of constellation construction. By designing the solar wings of cubsat with different configurations, and Constructing the simulation model of solar array, the charging performance, efficiency and service performance of different configurations of solar wings in microgravity space are simulated and analyzed. The results show that selecting the optimal configuration of solar array can provide better energy and power support for remote sensing cubesat, it provides an effective reference for the follow-up remote sensing cubesat to carry out more commercial applications.