CLC number: V27
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2012-12-10
Cited: 3
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Jian Liu, Quan-bao Wang, Hai-tao Zhao, Ji-an Chen, Ye Qiu, Deng-ping Duan. Optimization design of the stratospheric airship’s power system based on the methodology of orthogonal experiment[J]. Journal of Zhejiang University Science A, 2013, 14(1): 38-46.
@article{title="Optimization design of the stratospheric airship’s power system based on the methodology of orthogonal experiment",
author="Jian Liu, Quan-bao Wang, Hai-tao Zhao, Ji-an Chen, Ye Qiu, Deng-ping Duan",
journal="Journal of Zhejiang University Science A",
volume="14",
number="1",
pages="38-46",
year="2013",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A1200138"
}
%0 Journal Article
%T Optimization design of the stratospheric airship’s power system based on the methodology of orthogonal experiment
%A Jian Liu
%A Quan-bao Wang
%A Hai-tao Zhao
%A Ji-an Chen
%A Ye Qiu
%A Deng-ping Duan
%J Journal of Zhejiang University SCIENCE A
%V 14
%N 1
%P 38-46
%@ 1673-565X
%D 2013
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A1200138
TY - JOUR
T1 - Optimization design of the stratospheric airship’s power system based on the methodology of orthogonal experiment
A1 - Jian Liu
A1 - Quan-bao Wang
A1 - Hai-tao Zhao
A1 - Ji-an Chen
A1 - Ye Qiu
A1 - Deng-ping Duan
J0 - Journal of Zhejiang University Science A
VL - 14
IS - 1
SP - 38
EP - 46
%@ 1673-565X
Y1 - 2013
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A1200138
Abstract: The optimization design of the power system is essential for stratospheric airships with paradoxical requirements of high reliability and low weight. The methodology of orthogonal experiment is presented to deal with the problem of the optimization design of the airship’s power system. Mathematical models of the solar array, regenerative fuel cell, and power management subsystem (PMS) are presented. The basic theory of the method of orthogonal experiment is discussed, and the selection of factors and levels of the experiment and the choice of the evaluation function are also revealed. The proposed methodology is validated in the optimization design of the power system of the ZhiYuan-2 stratospheric airship. Results show that the optimal configuration is easily obtained through this methodology. Furthermore, the optimal configuration and three sub-optimal configurations are in the Pareto frontier of the design space. Sensitivity analyses for the weight and reliability of the airship’s power system are presented.
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