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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。
Due to the harsh environmental conditions in the stratosphere, the overall top-level design of the airship system is totally different from the design concept of low-altitude airships. According to the stratospheric environmental conditions, three balancing design concepts of energy balance, thermal balance and weight balance in the overall design of the airship system are put forward from the top of system design. It is pointed out that the three balances are the general outline of the optimization design of the airship. Based on the three balanced design concepts, eight main research contents of the overall design optimization of the airship system are proposed.