飞机尾涡相干激光探测系统设计与性能分析  

Design and Performance Analysis of Aircraft Wake Vortex Coherent Laser Detection System

作　　者：徐世龙[1,2] 胡以华[1,2] 郭力仁 

机构地区：[1]脉冲功率激光技术国家重点实验室(电子工程学院),安徽合肥230037 [2]电子制约技术安徽省重点实验室,安徽合肥230037

出　　处：《激光与光电子学进展》2014年第8期100-105,共6页Laser & Optoelectronics Progress

基　　金：国家自然科学基金(60672154);安徽省自然科学基金(10040606Q61)

摘　　要：为保证飞行安全,并尽可能地提高机场跑道容量,对飞机尾涡相干激光探测系统进行了设计。从飞机尾涡激光探测的总体要求出发,提出相干激光探测系统结构,同时针对激光光源参数以及平衡探测光路结构进行设计,给出整个系统的设计参数。通过对所设计系统的探测信噪比以及测速精度的仿真分析表明,所设计的飞机尾涡相干激光探测系统能够满足尾涡探测的需求,当脉冲能量达到25 mJ以上时,雷达在探测距离7 km内的探测信噪比大于3 dB;在2 km内测速精度优于0.2 m/s。In order to ensure flight safety and to improve the capability of the airport runway as far as possible, an aircraft wake vortex coherent laser detection system is designed. Begin with the requirements of wake vortex laser detection, the structure of the system is proposed. The parameters of the laser source and the optical path of the double balance detection are designed at the same time. The performance simulation proves that this detection system can meet the detection requirements. When the output energy is higher than 25 m J, the detection signal-to-noise-ratio （SNR） can be up to 3 dB at the distance of 7 km and the detection accuracy is better than 0.2 m/s within 2 km.

关 键 词：飞机尾涡 激光雷达 相干探测 飞行安全 跑道容量 

分 类 号：V328.3[航空宇航科学与技术—人机与环境工程]