宇航计测技术 ›› 2015, Vol. 35 ›› Issue (3): 44-47.doi: 10.12060/j.issn.1000-7202.2015.03.10

• 论文 • 上一篇    下一篇

飞行器太阳能源计算方法

梁君1,2；李海伟1；欧连军1；杨友超1；徐海运1   

  1. 1、中国运载火箭技术研究院研究发展中心，北京 100076；
     2、上海交通大学，上海 200240
  • 出版日期:2015-06-15 发布日期:2015-06-15
  • 作者简介:梁君（1980-）， 男，高级工程师，主要研究方向：电气综合技术。

The Method of Calculating Solar Energy on the Aerocraft

LIANG Jun1,2；LI Hai-wei1；OU Lian-jun1；YANG You-chao1；XU Hai-yun1   

  1. 1、China Academe of Launch Vehicle Technology R&D Center, Beijing 100076;
    2、Shanghai Jiao Tong University, Shanghai 200240
  • Online:2015-06-15 Published:2015-06-15

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摘要： 介绍了空间飞行器典型电源系统组成，通过对影响太阳能源输出的各项参数因素分析，提出了空间飞行器太阳能源计算方法，该方法包括由功率计算所需太阳阵面积的公式和由太阳阵面积计算输出功率的公式，达到了准确计算太阳能源的效果，解决了以往空间飞行器太阳能源估算误差大，在总体回路设计中电源参数难以闭环的问题。

关键词: 太阳能源, 计算方法, 飞行器电源系统

Abstract: The representative power system of aerocraft was introduced.All kinds of parameters，which impacted production of soalr energy, were analyzed.The method of calculating solar energy on the aerocraft was provided,which included from the power to the area of the solar array and from area of the solar array to the producing power.The effect of accurately calculating solar energy was achieved.The problem,which the power parameters for the aerocraft were difficult to realize due to error of estimate in macro loop design,was solved.

Key words: Solar energy, Calculation method, Power system of aerocraft

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