期刊文献+

基于法布里-珀罗干涉仪反演大气风速和温度的简化算法 被引量:7

A New Reduction Technique for Thermospheric Wind and Temperature Measurement with Fabry-Perot Interferometer
原文传递
导出
摘要 阐述了基于法布里-珀罗干涉仪(FPI)反演中高层大气风速和温度的基本原理,研究了FPI系统传递函数及其对入射谱线的响应表达式。借鉴传统FPI反演中高层大气风速和温度的经典理论,提出一种矩阵简化算法。利用分解和近似的数学基础方法来得到系统响应表达式的矩阵形式,然后采用最小二乘法反演出大气风速和温度。仿真结果表明:当预估风速和温度偏离实际风速和温度,小于150m/s和80K时,反演风速和温度的误差范围在±3m/s和±10K内。矩阵简化算法不但保留了完整傅里叶级数描述法的精确性,而且避免了激光校准和波长变换,具有简单和快速的优点。 The principle of measuring thermospheric wind and temperature by Fabry-Perot interferometer (FPI) is elaborated, the transfer function of FPI and the analytical response expression to the incident line is studied. Referring to the basic principle of traditional wind and temperature retrieval method with FPI, a new matrix reduction technique is proposed. This technique is based on the decompose and approximate mathematics to obtain the matrix form of analytical response expression, then a least-squares technique is employed to get the thermospheric wind and temperature. Simulation results show that when the guessed wind is less than 150 m/s and the guessed temperature is less than 80 K, the error range is ±3 m/s for wind and ±10 K for temperature. The matrix technique not only retains the accuracy of a full Fourier Series Representation method, but also avoids instrument calibration and wavelength translation, which makes it simple and fast.
出处 《光学学报》 EI CAS CSCD 北大核心 2013年第11期297-303,共7页 Acta Optica Sinica
基金 国家自然科学基金(41005109) 西部之光人才基金(Y129281213) 中科院光谱成像技术重点实验室创新基金(Y255C61ZZ0)
关键词 大气光学 风速温度反演 法布里-珀罗干涉仪 系统响应表达式 矩阵简化算法 atmospheric optics wind and temperature retrieval Fabry-Perot interferometer systematic response expression matrix reduction technique
  • 相关文献

参考文献9

二级参考文献108

共引文献44

同被引文献76

  • 1恩德,陈才和,崔宇明,丁桂兰.集成光学迈克尔逊干涉型加速度地震检波器[J].中国激光,2005,32(3):399-403. 被引量:8
  • 2朱翔,方中华,孙胜利.光纤传像系统中的耦合技术研究[J].红外技术,2006,28(5):257-260. 被引量:9
  • 3王宏,欧阳征标,韩艳玲,阮双琛.含色散介质的一维光子晶体微腔的光学特性和模式调节[J].光学学报,2007,27(5):940-945. 被引量:17
  • 4刘木林,叶志请,闵秋应,刘晓山,吴木生,柯强.高斯光束斜入射法布里-珀罗干涉腔后的反射光强分布[J].光子学报,2007,36(8):1510-1514. 被引量:5
  • 5Keane M, Buckton D, Redfern M, et al: Axial detection of aircraft wake vortices using Doppler lidar[J]. Journal ofAircraft, 2002, 39(5): 850-861.
  • 6Patrick R Veillette. Data show that U.S wake-turbulence accidents are most frequent at low altitude and during approach and landing[J]. Flight Safety Digest, 2002, 21(3-4): 1-47.
  • 7Barbaresco F, Juge P, Klein M, et al: Optimising runway throughput through wake vortex detection, prediction and decision support tools[C]. Digital Communications- Enhanced Surveillance of Aircraft and Vehicles (TIWDC/ESAV), 2011.Tyrrhenian International Workshop on IEEE, 2011.27-32.
  • 8Darracq D, Corjon A, Fr, et al: Simulation of wake vortex detection with airborne Doppler lidar[J]. Journal of Aircraft, 2000, 37(6): 984-993.
  • 9Fiduccia P C, Bryant W, Lang S. Wake turbulence research program[J]. Journal of Air Traffic Control, 2004, 46(1): 17-21.
  • 10Hannon S M, Barr K S, Jacob D K, et al: Application of pulsed Doppler lidar in the airport terminal area [C]. Fourth International Asia-Pacific Environmental Remote Sensing Symposium 2004: Remote Sensing of the Atmosphere, Ocean, Environment, and Space: International Society for Optics and Photonics, 2005. 186-197.

引证文献7

二级引证文献35

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