结果表明，本文方法对浮空器副气囊的设计有一定参考价值。
The result shows that the method has a reference value in the aerostat ballonet design.
当时高度存在大误差时，采用副气囊和空气舵组合控制改变飞艇的姿态实现快速爬升或下降；
It is present a method to design altitude control system for a high altitude airship using auxiliary ballonet charge or deflation and elevator combination control.
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