Aircraft vortices are generated by the liftproducing surfaces of the aircraft. The variability of near-surface conditions can change the drop rate and cause the cell of the wake vortex to twist and contort unpredictably. The pulsed Coherent Doppler Lidar Detection and Ranging is an indispensable access to real aircraft vortices behavior which transmitting a laser beam and detecting the radiation backscattered by atmospheric aerosol particles. Experiments for Coherent Doppler Lidar measurement of aircraft wake vortices has been successfully carried out at the Beijing Capital International Airport (BCIA). In this paper, the authors discuss the Lidar system, the observation modes carried out in the measurements at BCIA and the characteristics of vortices.
INTRODUCTIONWake vortices are generated by the lift-producing surfaces of the aircraft [1]. The lifting surfaces of all aircraft produce wake vortices to some extent [2,4]. The vortex created by a large aircraft can have a catastrophic effect on a small airplane following closely behind [3].The variability of near-surface conditions (temperature, humidity, wind shear, etc.) can change the drop rate and cause the vortex cell to twist and contort unpredictably [4]. Wake Vortex behaviors very close to the ground have very complex causes that could change abruptly and need for real time monitoring [5]. The CDL(Coherent Doppler Lidar) system is a useful tool that can measure wind, turbulence, aircraft wake vortices, and so forth [5][6][7][8][9][10].The pulsed Coherent Doppler Lidar Detection and Ranging is an indispensable access to real aircraft vortices behavior which transmitting a laser beam and detecting the radiation backscattered by atmospheric aerosol particles [11]. The Line-OfSight (LOS) velocity component of the air motion could get by analyzing the Doppler shift in the frequency of the backscattered signal [12]. From the LOS velocities and the broadening process of the backscattering spectrum the characteristic of the aircraft vortices can be deduced. The pulsed CDL system (Fig.l) is based on allfiber laser technology and fast digital signal processing technology. The laser equipped in the CDL system is 1.5-J..lm eye-safe fiber laser which has an adjustable pulse length of lOOns to 800 ns and a pulse repetition frequency of 10kHz. The measurement range of the CDL system is ±50mls, while the speed measurement uncertainty is 0.1 mls. The scanner and detection range of 3000m enable the system to detect the aircraft wake vortices. The fiber-based optical circuit works stable even under vibrating environment and temperature variation. The Fast Fourier Transform (FFT) spectral estimates are processed with FPGA in real time. All these design of the pulsed CDL system make it stable, reliable and high-integrated [13].2. METHODOLOGY The OUC Lidar team developed and carried out aircraft wake vortex field observation on the final approach to test out the performance of LOS velocity measurement in RHI (Range Height Indicator) and in ATOM (Along Track Observation...