Effect of angular losses on the output performance of solar array on long-endurance stratospheric airship

2017 ◽  
Vol 147 ◽  
pp. 135-144 ◽  
Author(s):  
Huafei Du ◽  
Weiyu Zhu ◽  
Yifei Wu ◽  
Lanchuan Zhang ◽  
Jun Li ◽  
...  
2016 ◽  
Vol 104 ◽  
pp. 743-750 ◽  
Author(s):  
Jun Li ◽  
Mingyun Lv ◽  
Dongjie Tan ◽  
Weiyu Zhu ◽  
Kangwen Sun ◽  
...  

2016 ◽  
Vol 17 (3) ◽  
pp. 432-441 ◽  
Author(s):  
Yuanyuan Zhang ◽  
Jun Li ◽  
Mingyun Lv ◽  
Dongjie Tan ◽  
Weiyu Zhu ◽  
...  

2017 ◽  
Vol 124 ◽  
pp. 22-33 ◽  
Author(s):  
Mingyun Lv ◽  
Zhongbing Yao ◽  
Lanchuan Zhang ◽  
Huafei Du ◽  
Junhui Meng ◽  
...  

2013 ◽  
Vol 772 ◽  
pp. 608-614
Author(s):  
Kang Wen Sun ◽  
Gao Ming Liang ◽  
Ke Li ◽  
Ming Zhu

As one of the key technic of achieving high-altitude and long-time flight, the stratospheric airship energy system in stratosphere is always the important point but also very difficult. In this paper, the stratospheric airship geometry analysis as a starting point, through a series analysis as follow: the stratospheric airship surface mesh model, the sun vector, the relationship between the sun vector and the body coordinate system, and the solar radiation model, we have accomplished the characteristics analysis of the radiation receiving on stratospheric airship. The analysis result show that: Although different flight direction corresponding to different distribution of light intensity, the light changes from sunrise to sunset is symmetrical when the stratospheric airship on the condition of level flight. Airship for east heading of region resides, the maximum energy can be obtained when the solar array laying in the installation of 0 β π / 4. With the changing of heading angle and pitch angle, the radiation receiving of the solar array can also transform, but the influence of pitch angle greater than heading angle.


2011 ◽  
Vol 88-89 ◽  
pp. 632-637
Author(s):  
M. Huang ◽  
Z.X. Xia ◽  
Q.H. Zeng

The stratospheric airship, with long-endurance and quasi-static capability, is suitable to carry out special mission such as communications relay, hot spots monitoring, etc. In order to improve the safety performance of the stratospheric airship and keep the robustness of mission, health management (HM) system is introduced, the foundation of which is the logic architecture. Based on the analysis of three options about the logic architecture used in spacecraft, hierarchical fusion architecture is selected, the functional modules in which are designed in detail. To solve urgent faults, moreover, the autonomous intelligent control system (AICS) is introduced. Meanwhile, monitoring mission is taken as an example to discuss the mission health management strategy based on laser communication.


Energies ◽  
2021 ◽  
Vol 14 (14) ◽  
pp. 4204
Author(s):  
Qiumin Dai ◽  
Daoming Xing ◽  
Xiande Fang ◽  
Yingjie Zhao

High altitude airships possess tremendous potential for long-endurance spot hovering platforms for both commercial and strategic applications. The energy system, which is mainly made up of solar array and regenerative fuel cell, is the key component of a high altitude airship. The thermal effect is a major factor that affects the performance of the energy system of long endurance stratospheric vehicles. In this paper, a conceptual design method focusing on the thermal and power characteristics of an energy system for stratospheric airships is proposed. The effect of thermal behavior of solar array on the energy system is analyzed. An optimized case is obtained on the consideration of power supply, thermal behaviors of helium and solar array. Results show that the maximum temperature difference of the solar array may be reduced by about 20 K and the mass of payload can be improved by up to 5%.


2014 ◽  
Vol 672-674 ◽  
pp. 1765-1769 ◽  
Author(s):  
Kang Wen Sun ◽  
Ming Zhu ◽  
Gao Ming Liang ◽  
Dong Dong Xu

In view of solar arrays applied in large-scale stratospheric airship, modular thinking was proposed by reasonable decomposition of solar array to design composite maximum power point tracking (MPPT) controller where the input and output are both in parallel, which ensures maximized solar energy output on a limited area. And each solar array sub-model was equipped with independent MPPT controller to control power tracking separately. Then, the solar array composed of three sub-models was used for simulation and its result indicates that MPPT controller of each sub-model can track the power quickly, and the output power can reach 93% of maximum input power when the efficiency loss of converter in reality is not considered . So, the model constructed in this paper can be used to optimize the design and analyze output characteristics quantitatively for the large-scale stratospheric airship's solar array.


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