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高空飞艇系统总体设计优化初探
引用本文:江京.高空飞艇系统总体设计优化初探[J].中国电子科学研究院学报,2012,7(4):356-361.
作者姓名:江京
作者单位:中国电子科学研究院,北京,100041
摘    要:由于平流层苛刻的环境条件制约,高空飞艇系统总体顶层设计完全不同于中低空飞艇的设计理念。根据平流层环境条件从系统顶层设计角度提出了高空飞艇系统总体设计中的能量平衡、热平衡和重量平衡三个平衡设计概念。指出三个平衡是高空飞艇优化设计的总纲,并根据三个平衡设计概念提出了高空飞艇系统总体设计优化的8个主要研究内容。

关 键 词:平流层  飞艇  系统总体设计  优化

Exploration of High-altitude Airship System General Design Optimization
JIANG Jing.Exploration of High-altitude Airship System General Design Optimization[J].Journal of China Academy of Electronics and Information Technology,2012,7(4):356-361.
Authors:JIANG Jing
Institution:JIANG Jing(China Academy of Electronics and Information Technology, Beijing 100041,China)
Abstract:Due to the restriction of rigorous natural conditions in the stratospheric environment,the top design of the high-altitude airship system is completely different from the design concept of airships at low altitude or middle altitude.The design concept of three balances in the top design of the high-altitude airship system is put forward from the view point of the environmental conditions in the stratospheric.It is pointed out that "Three Balances" is a key line of optimization design of high-altitude airship system.Based on the design concept of "Three Balances",eight principal research aspects on the top design optimization of the high-altitude airship system are brought forward.
Keywords:stratospheric  airship  general design of the airship  optimization
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