摘要
基于临近空间飞行器宽速域、大机动飞行对大气传感系统的需求,结合国内外在相关领域的研究情况,对比分析了探出式和球形头部两种大气传感系统的工作原理及其在复杂外形飞行器上应用存在的问题,详细梳理了临近空间飞行器大气传感的关键技术及后续亟需解决的难题。
Aiming at the demands of the airdata sensing technologies for near space high-speed aerocraft , such as the high speed flight, the both working theory about extrusive airdata sensing systems and orbic- ular airdata sensing systems have been contrastively analyzed. To avoid the drawback of the both airdata sensing systems, some airdata sensing pivotal technologies fitting for intricate aerocraft are proposed . Fi- nally, the pivotal technologies and some issues to be ravelled out of future development about airdata sensing systems have been summarized.
出处
《战术导弹技术》
2014年第1期22-26,62,共6页
Tactical Missile Technology
关键词
临近空间飞行器
大气传感系统
关键技术分析
near space high-speed airvehicle
airdata sensing systems
pivotal technologies analysis
