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多普勒非对称空间外差干涉仪调制度分析 被引量:1
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作者 施海亮 李志伟 +1 位作者 罗海燕 熊伟 《航天返回与遥感》 CSCD 2018年第5期57-65,共9页
多普勒非对称空间外差光谱仪是近年得以迅速发展的新型中高层大气风场探测仪器,具有视场展宽、大光通量、高光谱分辨和多谱线同时探测等特点。该仪器的干涉调制度是影响风场反演精度的关键指标。文章基于非对称空间外差光谱技术基本原理... 多普勒非对称空间外差光谱仪是近年得以迅速发展的新型中高层大气风场探测仪器,具有视场展宽、大光通量、高光谱分辨和多谱线同时探测等特点。该仪器的干涉调制度是影响风场反演精度的关键指标。文章基于非对称空间外差光谱技术基本原理,推导了干涉仪视场展宽前后的干涉理论积分公式,分析了干涉调制度与仪器视场角、最优光程差的关系,通过对干涉方程中像元采样积分推导得到干涉调制度与采样间隔的理论形式,仿真了干涉调制度与仪器视场角、最优光程差和采样间隔的定量关系曲线,并通过实验室搭建试验装置对分析结果进行验证。研究结果表明:随着非对称空间外差干涉仪视场角和光程差偏置量的增加,干涉调制度降低;调制度沿着波数增大的方向上升,在同一波数处,随着采样间隔的增加,干涉调制度降低。理论分析和试验测量结果调制度最大偏差0.02,分析与实测结果一致性较好。 展开更多
关键词 多普勒外差干涉仪 调制度 视场角 最优光程差 相位频移 空间大气探测
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地基双波段非对称空间外差测风干涉仪设计
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作者 崔勇 高亮 +3 位作者 江伦 王锦疆 裴惠熠 方远翔 《应用光学》 北大核心 2025年第3期571-579,共9页
根据中高层大气风场探测需求,设计了一款可对557.7 nm氧原子绿线气辉及630.0 nm氧原子红线气辉同时进行探测的非对称空间外差测风干涉仪,探测范围为90 km~300 km。为实现对双波段的探测,根据干涉条纹调制度与最优光程差的关系,选择对双... 根据中高层大气风场探测需求,设计了一款可对557.7 nm氧原子绿线气辉及630.0 nm氧原子红线气辉同时进行探测的非对称空间外差测风干涉仪,探测范围为90 km~300 km。为实现对双波段的探测,根据干涉条纹调制度与最优光程差的关系,选择对双波段兼容的光程差。通过对扩视场棱镜的顶角及材料进行设计和选择,提高了干涉仪的视场范围。为减少热偏差对测风精度的影响,推导了热偏差与垫片材料、垫片厚度、干涉仪偏置量的关系式,并通过该式计算出相应的参数。此外,采用一种中阶梯光栅作为反射光栅,实现双波段同时探测。根据地基探测的需要,设计了前置镜组及后置镜组。最后对整体系统进行仿真并获取模拟条纹图,验证系统是否满足双波段探测需要。仿真结果表明:干涉仪的干涉模块在557.7 nm气辉波段的光程差的热偏差为3.22×10^(-6) mm/℃,相位热漂移为0.03 rad/℃;630 nm气辉波段的光程差的热偏差为9.45×10^(-7) mm/℃,相位热漂移为0.009 42 rad/℃,证明了该系统相较于早期的设计降低了热偏差对测量精度的影响,满足90 km~300 km测风要求。 展开更多
关键词 中高层大气 风速测量 非对称空间外差 干涉仪 光学设计
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Opto-mechanical-thermal integration analysis of Doppler asymmetric spatial heterodyne interferometer
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作者 WANG Jin-jiang JIANG Lun +3 位作者 TONG Shou-feng PEI Hui-yi CUI Yong GUO Ming-hang 《中国光学(中英文)》 EI CAS CSCD 北大核心 2024年第6期1489-1511,共23页
In order to improve the detection accuracy of Doppler asymmetric spatial heterodyne(DASH)interferometer in harsh temperatures,an opto-mechanical-thermal integration analysis is carried out.Firstly,the correlation betw... In order to improve the detection accuracy of Doppler asymmetric spatial heterodyne(DASH)interferometer in harsh temperatures,an opto-mechanical-thermal integration analysis is carried out.Firstly,the correlation between the interference phase and temperature is established according to the working principle and the phase algorithm of the interferometer.Secondly,the optical mechanical thermal analysis model and thermal deformation data acquisition model are designed.The deformation data of the interference module and the imaging optical system at different temperatures are given by temperature load simulation analysis,and the phase error caused by thermal deformation is obtained by fitting.Finally,based on the wind speed error caused by thermal deformation of each component,a reasonable temperature control scheme is proposed.The results show that the interference module occupies the main cause,the temperature must be controlled within(20±0.05)℃,and the temperature control should be carried out for the temperature sensitive parts,and the wind speed error caused by the part is 3.8 m/s.The thermal drift between the magnification of the imaging optical system and the thermal drift of the relative position between the imaging optical system and the detector should occupy the secondary cause,which should be controlled within(20±2)℃,and the wind speed error caused by the part is 3.05 m/s.In summary,the wind measurement error caused by interference module,imaging optical system,and the relative position between the imaging optical system and the detector can be controlled within 6.85 m/s.The analysis and temperature control schemes presented in this paper can provide theoretical basis for DASH interferometer engineering applications. 展开更多
关键词 Doppler asymmetric spatial heterodyne interferometer interference module imaging optical system opto-mechanical thermal integration analysis phase error temperature control
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