期刊文献+

平流层飞艇机载风速测量方法 被引量:5

Stratospheric airship airborne velocity measurement
原文传递
导出
摘要 风场数据是平流层飞艇实现长时驻空和飞行控制的重要参数。针对平流层空气稀薄、传统机载压力式测风速方法测量精度低等问题,提出一种利用激光雷达直接探测技术的平流层飞艇机载风速测量方法。设计了基于直接探测原理的多普勒激光雷达测风速系统,构建了分别以FP(IFabry-Perot干涉仪)和MZ(IMach-Zehnder干涉仪)为鉴频器的条纹成像技术的风速反演数学模型,并进行了数值仿真分析。结果显示,在355 nm波长出射激光和20 m/s径向风速条件下,FPI-条纹成像技术与MZI-条纹成像技术的径向风速测量误差分别为11.0%和6.5%,测量分辨率分别为1.90 m/s和1.62 m/s,表明该方法能够满足平流层飞艇机载风速测量要求。 The wind field data are important input parameters for the stratospheric airship in the long-time loiter and the flight control. In view of the thin air in the stratosphere and the low precision of the pitot tube, a direct detection method based on LIDAR is proposed. A Doppler lidar velocity measurement system based on the direct detection principle is designed. The wind velocity inversion mathematical model of the two fringe imaging techniques is built and numerical simulations are carried out. It is shown that the measurement errors of the Fabry-Perot etalon(FPI) and the Mach-Zehnder interferometer(MZI) are 11.0% and 6.5%, respectively, at 355 nm output laser and20 m/s wind speed. And the velocity resolution of the two methods are 1.9 m/s and 1.6 m/s, respectively. The results indicate that the new method can effectively meet the requirements of the stratospheric airship wind speed measurement.
作者 张澜川 孟军辉 吕明云 ZHANG Lanchuan MENG Junhui LU Mingyun(School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China)
出处 《科技导报》 CAS CSCD 北大核心 2017年第2期80-86,共7页 Science & Technology Review
基金 中国博士后科学基金项目(2016M600891)
关键词 平流层飞艇 风速测量 激光雷达 条纹成像技术 stratospheric airship wind measurement lidar fringe imaging technique
  • 相关文献

参考文献17

二级参考文献164

共引文献195

同被引文献72

引证文献5

二级引证文献20

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部