Layout Optimization of Solar Array for Stratospheric Airship with Thermal Effect

被引:0
作者
Wu, Yifei [1 ]
Lv, Mingyun [1 ]
Cui, Erqiang [1 ]
Zhu, Ming [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China
来源
PROCEEDINGS OF 2018 9TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE 2018) | 2018年
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
layout optimization; solar array; stratospheric airship; thermal effect; genetic algorithm; OUTPUT PERFORMANCE;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The layout of solar array is one of the main factors affecting the output power of solar array for long-endurance flight of stratospheric airship. The temperature of solar array plays a major rule in conversion efficiency of solar array. But the research about layout optimization of solar array considering the effect of temperature on conversion efficiency of solar array is rare. This paper develops a numerical model consisting of solar radiation model, stratospheric airship thermal model, power output model, and optimization model to optimize the layout of solar array considering thermal effect. The feasibility of the model is verified by comparing the calculation results with the results of other researchers. Then, the layout of solar array is optimized with thermal effect by genetic algorithm (GA). The results show that the output energy of the whole year rises by 7.6% after layout optimization of solar array. The results of the paper would provide a useful guide to obtain suitable layout of solar array for long-endurance stratospheric airship.
引用
收藏
页码:85 / 89
页数:5
相关论文
共 15 条
[1]   Performance simulation of high altitude scientific balloons [J].
Dai, Qiumin ;
Fang, Xiande ;
Li, Xiaojian ;
Tian, Lili .
ADVANCES IN SPACE RESEARCH, 2012, 49 (06) :1045-1052
[2]   Effect of angular losses on the output performance of solar array on long-endurance stratospheric airship [J].
Du, Huafei ;
Zhu, Weiyu ;
Wu, Yifei ;
Zhang, Lanchuan ;
Li, Jun ;
Lv, Mingyun .
ENERGY CONVERSION AND MANAGEMENT, 2017, 147 :135-144
[3]  
Garg A., 2011, 11 AIAA AV TECHN INT, P6974
[4]   Thermal insulation performance of lightweight substrate for solar array on stratospheric airships [J].
Li, Jun ;
Lv, Mingyun ;
Sun, Kangwen ;
Zhu, Weiyu .
APPLIED THERMAL ENGINEERING, 2016, 107 :1158-1165
[5]   Output performance analyses of solar array on stratospheric airship with thermal effect [J].
Li, Jun ;
Lv, Mingyun ;
Tan, Dongjie ;
Zhu, Weiyu ;
Sun, Kangwen ;
Zhang, Yuanyuan .
APPLIED THERMAL ENGINEERING, 2016, 104 :743-750
[6]   Modeling and analysis of floating performances of stratospheric semi-rigid airships [J].
Li, Xiaojian ;
Fang, Xiande ;
Dai, Qiuming ;
Zhou, Zhanru .
ADVANCES IN SPACE RESEARCH, 2012, 50 (07) :881-890
[7]   Research on Thermal Characteristics of Photovoltaic Array of Stratospheric Airship [J].
Li, Xiaojian ;
Fang, Xiande ;
Dai, Qiuming .
JOURNAL OF AIRCRAFT, 2011, 48 (04) :1380-1386
[8]  
Liu Q., 2017, ADV SPACE RES
[9]   Solar array layout optimization for stratospheric airships using numerical method [J].
Lv, Mingyun ;
Li, Jun ;
Du, Huafei ;
Zhu, Weiyu ;
Meng, Junhui .
ENERGY CONVERSION AND MANAGEMENT, 2017, 135 :160-169
[10]  
Naito H., 1999, 13 AIAA LIGHT AIR TE