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Volker Tank 《Mikrochimica acta》1988,95(1-6):319-321
In optical interferometers the alteration of pathlengths is usually achieved by moving one of the two interferometer mirrors back and forth. Employing rotating retroreflectors (corner reflectors), two slightly different concepts have been developed to replace this stop and go movement by a continuous rotation. 相似文献
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The light intensity distribution (LID) reflected by a planar corner-cube retroreflector array with the size of centimeter and above (PCCRA) is calculated based on the Collins formula, coordinate transformation matrixes and vector algebra. The expression can be used for the PCCRAs with different parameters and different complex optical systems described by ABCD matrix. The expression indicates that the LID of a PCCRA is much different from a single corner-cube retroreflector (CCR) with equivalent aperture. Computer simulations are applied to explain the expression clearly. The results show that the LID of the PCCRA is more homogeneous than the single CCR with equivalent aperture under circumstances of both normal incident light and oblique incident light. In addition, the expression is proved by comparing the simulation result of the PCCRA only comprising a single CCR and the previous experimental result. 相似文献
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针对近年来应用颇多的两种较特殊的光学元件——角锥棱镜和柱面(透)镜技术表述的不同形式,为使之逐渐趋于规范和统一,参照国外现行的一些技术要求以及国内公司几年来实施的具体事例,给出若干说明、建议、指标和数据处理方法,尤其推荐用光束平行差的均方差来替代最大光束平行差的指标,是评定角锥棱镜技术特性中一项关键的新指标。 相似文献
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减小外差干涉一次谐波非线性误差的方法 总被引:2,自引:0,他引:2
为了补偿激光外差干涉纳米测量中的非线性误差,提出了一种减小非线性误差的一次谐波方法。基于全反射理论分析了镀膜实体角锥棱镜反射光偏振特性,并由此推导出角锥棱镜反射光偏振特性及测量角锥棱镜以其运动方向为轴线的轴向旋转对激光外差干涉非线性误差一次谐波的影响模型。理论分析表明,测量角锥棱镜以其运动方向为轴线的轴向旋转会减小非线性误差一次谐波,当测量角锥棱镜轴向旋转97°时,可使非线性误差一次谐波达到最小,约为原有非线性误差一次谐波分量的1/20倍。当激光器出射的两束线偏振光存在6°非正交误差时,镀膜实体测量角锥棱镜轴向旋转角度从0°增加到97°,非线性误差一次谐波由5.30 nm减小到0.30 nm。 相似文献
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Masanori Itaba Atsushi Minato Hiroki Azumi Satoru Ozawa Nobuo Sugimoto 《Optical Review》2002,9(1):25-28
Retroreflectors on satellites are used as targets for laser ranging and laser long-path absorption measurements of atmospheric trace species. To compensate for the velocity aberration, slight tuning of the design is necessary. The curvatures of mirrors, the angles between mirrors, and the direction of the retroreflector on the satellite must be tuned to optimize the optical efficiency of the retroreflector. An enumerative scheme is not applicable when the number of parameters is large. We proposed earlier a technique using a genetic algorithm for the optical design of a space retroreflector.1) In this paper, we have improved the method introducing a hybrid technique that is a combination of a genetic algorithm and simulated annealing. 相似文献
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An acute retroreflector having dihedral angles of 45, 60 and 90 deg exactly reflects incident rays in the opposite direction.
Beam pattern or wave front of the reflected light of the acute retroreflector can be controlled by tuning dihedral angles.
We present here a new method for calculating the reflected wave front of the acute retroreflector, in which the wave front
is calculated with high accuracy and in a shorter calculation time than by the conventional ray trace method. 相似文献
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