摘要
CubeSat以体积小、成本低、研制周期短等优点受到越来越广泛的关注,但CubeSat的高度集成化、模块化设计对结构热控提出了更高的要求,而且宇宙中的辐射也会对立方体卫星造成影响。本文在参考国外高校对CubeSat的结构热控和辐射防护方案基础上,对结构热控与辐射防护方案进行分析与讨论,给出更理想的方案。
CubeSat is more and more popular because of its peculiarity such as smaller size,low costing and short build-time.However,because it is Highly Integrated and modular,we are requested to do better when we are designing automation for satellite thermal control.At the same time,the radiation in the space will also has impact on our CubeSat.This paper aim to analyze,discuss and present a more ideal scheme using genetic algorithm after reading scheme other school offered.
引文
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