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Implementation of the Chicago sum frequency laser at Palomar laser guide star test bed

机译:Palomar激光导航星试验床上芝加哥和频率激光的实施

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Work is underway at the University of Chicago and Caltech Optical Observatories to implement a sodium laser guide star adaptive optics system for the 200 inch Hale telescope at Palomar Observatory. The Chicago sum frequency laser (CSFL) consists of two pulsed, diode-pumped, mode-locked Nd:YAG lasers working at 1.064 micron and 1.32 micron wavelengths. Light from the two laser beams is mixed in a non-linear crystal to produce radiation centered at 589 nm with a spectral width of 1.0 GHz (FWHM) to match that of the Sodium-D2 line. Currently the 1.064 micron and 1.32 micron lasers produce 14 watts and 8 watts of TEM-00 power respectively. The laser runs at 500 Hz rep. rate with 10% duty cycle. This pulse format is similar to that of the MIT-Lincoln labs and allows range gating of unwanted Rayleigh scatter down an angle of 60 degrees to zenith angle. The laser system will be kept in the Coude lab and will be projected up to a laser launch telescope (LLT) bore-sited to the Hale telescope. The beam-transfer optics, which conveys the laser beam from the Coude lab to the LLT, consists of motorized mirrors that are controlled in real time using quad-cell positioning systems. This needs to be done to prevent laser beam wander due to deflections of the telescope while tracking. There is a central computer that monitors the laser beam propagation up to the LLT, the interlocks and safety system status, laser status and actively controls the motorized mirrors. We plan to install a wide-field visible camera (for high flying aircraft) and a narrow field of view (FoV) IR camera (for low-flying aircraft) as part of our aircraft avoidance system.
机译:在芝加哥大学和CALTECH光学观察区正在进行工作,为Palomar天文台进行200英寸Hale望远镜的钠激光导向星自适应光学系统。芝加哥和频率激光器(CSFL)由两个脉冲,二极管泵浦的模式锁定的Nd:YAG激光器工作在1.064微米和1.32微米波长下。来自两个激光束的光在非线性晶体中混合,以产生以589nm为中心的辐射,光谱宽度为1.0GHz(FWHM)以与钠-D2线的匹配。目前,1.064微米和1.32微米激光器分别产生14瓦和8瓦的TEM-00功率。激光在500 Hz rep中运行。占占空比10%的速度。该脉冲格式类似于MIT-LINCOLN LABS的脉冲格式,并且允许不需要的瑞利范围的范围门,从60度到天顶角的角度。激光系统将保存在Coude Lab中,并将被预测到激光发射望远镜(LLT)孔口到HALE望远镜。将激光束从Coude Lab传送到LLT的光束传输光学器件由使用四单元定位系统实时控制的电动镜子组成。这需要进行,以防止由于望远镜的偏转而导致激光束徘徊在跟踪时。有一个中央计算机,将激光束传播监控到LLT,互锁和安全系统状态,激光状态,并主动控制电动镜。我们计划为飞机避免系统的一部分安装宽敞的可见摄像机(用于高飞飞机)和狭窄的视野(FOV)IR相机(用于低飞行飞机)。

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