对一种利用高空风的风速差控制飞行轨迹的新型低能耗临近空间飞行器，进行了力学分析与配平计算。
The mechanical analysis and the trimming were performed for a novel near space aircraft which uses the variation in wind speed at high altitude to control its flight path.
进行临近空间飞行器防空反导预警系统体系结构设计时，面临的主要问题之一是设计模拟对象的模型体系。
This paper is of great reference value to the design of air defense and anti-missile warning system.
大气中子是这一区域诱发元器件发生单粒子效应最主要的原因，严重威胁着临近空间飞行器安全、可靠地工作。
Atmospheric neutron is the main radioactive particle in the near space that induced single event effects (SEE) and seriously imperils the safety of the aircraft at this altitude.
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