CAJ | 학술논문

为了实现对空间光机系统在复杂环境下光学性能的快速评估,介绍了光机热一体化分析方法的原理和流程,以及在该原理基础上研发的光机热分析软件的主要算法和功能,阐述了作为其关键部分的光机热数据接口问题.以Hα和白光望远镜(HWT)为例,计算出该望远镜在不同系统温度下的光机热一体化分析结果.给出的光学传递函数和波像差变化结果表明:在不同系统温度下,HWT望远镜光学性能将发生相应变化.当系统温度约为20℃时,系统性能最佳,其波像差约为λ/10.当系统温度在15～25℃之间时,系统波像差约优于λ/6.基于光机热一体化分析方法的原理,给出了适用于空间光机系统的一套可行的技术途径.
위료실현대공간광궤계통재복잡배경하광학성능적쾌속평고,개소료광궤열일체화분석방법적원리화류정,이급재해원리기출상연발적광궤열분석연건적주요산법화공능,천술료작위기관건부분적광궤열수거접구문제.이Hα화백광망원경(HWT)위례,계산출해망원경재불동계통온도하적광궤열일체화분석결과.급출적광학전체함수화파상차변화결과표명:재불동계통온도하,HWT망원경광학성능장발생상응변화.당계통온도약위20℃시,계통성능최가,기파상차약위λ/10.당계통온도재15～25℃지간시,계통파상차약우우λ/6.기우광궤열일체화분석방법적원리,급출료괄용우공간광궤계통적일투가행적기술도경.
To realize the rapid evaluation of the optical performance of the high resolution space opto-mechanical system under complex environment, the main principle and process of the integrated optical-structural-thermal analysis were introduced. The primary algorithms and functions of the analysis tool developed on the principle of the integrated optical-structural-thermal were presented. As the key points, the data interface problems were illustrated. The Hα and white light telescope(HWT) was taken as an example of the integrated optical-structural-thermal analysis. The wave front error and the modulation transfer function results show that the optical performances of the HWT telescope change with the system temperature. The wave front error is about λ/10, which is best at the system temperature of 20℃. When the system temperature is between 15℃ and 25℃, the wave front error is better than λ/6.Based on the principle of the integrated optical-structural-thermal analysis, a practical technical route for the space opto-mechanical systems is presented.