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星载临边光谱仪反射镜组件优化设计分析

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针对星载临边光谱仪离轴凹面反射镜组件高性能要求,对反射镜及其支撑结构进行了详细的光机优化设计。选用微晶玻璃作为载荷材料,通过施加最小尺寸约束的变密度拓扑优化方法确定镜体背部加强筋的分布,将背部筋厚尺寸变量灵敏度分析与局部筋厚多尺寸优化相结合,得到轻量化率为60%的反射镜结构;通过引入综合评价因子Q定量评价优化方案,对支撑结构中主要结构参数进行了多目标优化,获得了性能良好的柔性支撑结构。对优化处理前后反射镜组件进行光机集成分析,结果显示组件重力载荷工况与热力耦合工况下,优化处理后组件静力学性能更优。有限元分析得到组件1阶固有频率为942。2 Hz,正弦扫频试验结果表明组件1阶固有频率为956。5 Hz,分析误差为1。5%,结构动态性能较优;未优化处理组件在重力载荷及热力耦合工况下面型精度较差,而优化处理后组件在重力载荷工况下面型精度均方根值和峰谷值分别为9。5 nm、46。7 nm,在热力耦合工况下面型精度均方根值和峰谷值最大分别为8。25 nm、40。6 nm,对两种工况下反射镜进行面型检测,均方根值误差分别仅为6。1%和6。9%,在误差允许范围内;弥散斑均布于艾里斑内部,表明该凹面反射镜组件结构优化设计符合指标要求。
Optimization Design of the Spaceborne Edge Spectral Imager Reflective Mirror Assembly
The off-axis concave mirror assembly of the Starborne Proximity Spectrometer(SPM)is a crucial component that significantly impacts its overall performance.Given the stringent requirements for high performance,a meticulous opto-mechanical optimization design was conducted for both the mirror and its support structure within the spectrometer.This comprehensive design process involved numerous iterations and simulations to ensure that the mirror assembly met all the specified criteria for optical and mechanical performance.Microcrystalline glass was selected as the ideal loading material for the concave mirror body due to its exceptional optical properties and mechanical strength.The distribution of reinforcement bars on the back of the mirror body was determined through a sophisticated variable density topology optimization method.This method incorporated sensitivity analysis of the back bar thickness dimensional variables,along with optimization of the local bar thickness and multiple dimensions.The result was a mirror structure with an impressive light weighting rate of 60%,which not only reduced the overall weight but also maintained excellent structural performance.The optimization design for the concave mirror assembly support structure was equally rigorous.To enhance the performance of the mirror and its support structure,mounting holes were added to the back of the concave mirror assembly.This modification allowed for better integration of the mirror within the spectrometer and improved the overall stability of the assembly.In the optimized design of the support structure,a flexible groove was innovatively introduced near the mounting holes.This flexible groove served to mitigate the adverse effects of thermal load on the mirror surface.The main structural parameters of the flexible groove were optimized in a multi-objective manner using a comprehensive evaluation factor Q.This factor allowed for quantitative evaluation of various optimization schemes,ensuring that the final design was both robust and efficient.As a result,a flexible support structure with outstanding performance under optimal structural parameters was obtained.The optical-mechanical integration analysis of the mirror assembly before and after the optimization process revealed significant improvements.The optimized assembly exhibited superior static mechanical performance and better optical performance under both gravity load conditions and thermal coupling conditions.This improvement was attributed to the refined design of the mirror and its support structure,which effectively minimized distortions and maintained high optical accuracy.To further validate the design,a finite element analysis of the concave reflector assembly was conducted.The results showed that the 1st-order intrinsic frequency of the assembly was 942.2 Hz.This value was verified through a sinusoidal sweep test,which revealed a 1st-order intrinsic frequency of 956.5 Hz,with an analytical error of only 1.5%.This indicated that the structure had excellent dynamic performance,which was crucial for ensuring the stability and reliability of the spectrometer during operation.In contrast,the unoptimized assembly exhibited poor typing accuracy under gravity load and thermal coupling conditions.However,the optimized assembly demonstrated significantly better performance under these conditions,particularly under thermal coupling.In the gravity loading condition,the root mean square and peak-to-valley values were 9.5 nm and 46.7 nm,respectively.Under thermal coupling conditions,these values improved to 8.25 nm and 40.6 nm,respectively.These results demonstrated that the mirrors under both conditions had high accuracy in the surface pattern and met the relevant design requirements.Surface pattern inspections of the mirrors under both conditions further confirmed the reliability of the optimized design.The RMS errors were 6.1%and 6.9%,respectively,which were within the allowable error range.This not only verified the accuracy of the integrated analysis but also demonstrated the robustness of the optimized design.Additionally,the dispersive spots generated by the optimized concave mirror assembly were all located within the Airy spots.This indicated that the optimized design met the requirements for the index of performance,ensuring that the spectrometer could provide highly accurate and reliable data on atmospheric pollutants.

Starborne proximity spectrometerStructural topology optimizationOptomechanical integration analysisReflectorsOptomechanical structures

叶帅、曾议、鲁晓峰、刘凤垒、朱磊、陈军、江宇、赵敏杰、周海金、司福祺

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中国科学技术大学,合肥 230026

中国科学院,合肥物质科学研究院安徽光学精密机械研究所 环境光学与技术重点实验室,合肥 230031

星载临边光谱仪 结构拓扑优化 光机集成分析 反射镜 光机结构

2024

光子学报
中国光学学会 中国科学院西安光学精密机械研究所

光子学报

CSTPCD北大核心
影响因子:0.948
ISSN:1004-4213
年,卷(期):2024.53(11)