飞行器太阳能源计算方法  

The Method of Calculating Solar Energy on the Aerocraft

作　　者：梁君[1,2] 李海伟[1] 欧连军[1] 杨友超[1] 徐海运 

机构地区：[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　　处：《宇航计测技术》2015年第3期44-47,共4页Journal of Astronautic Metrology and Measurement

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。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.

关 键 词：太阳能源 计算方法 飞行器电源系统 

分 类 号：V57[航空宇航科学与技术—航空宇航推进理论与工程]