Common optical path installation and adjustment method and system for stationary orbit microwave-infrared composite detection system

By establishing an assembly and adjustment benchmark using lidar and laser tracker, and combining it with a multi-stage assembly and adjustment strategy, the high-precision assembly and adjustment problem of the geostationary orbit microwave-infrared composite detection system was solved, enabling rapid and accurate adjustment of the infrared detection system and improving the system's imaging quality and assembly and adjustment efficiency.

CN122410657APending Publication Date: 2026-07-17SHANGHAI SATELLITE ENG INST
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Patent Information

Application Number
CN202610471795.7
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2026-04-10
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies struggle to achieve high-precision and rapid assembly and adjustment of geostationary orbit microwave-infrared composite detection systems, especially in controlling the relative pose deviations of each component of the infrared detection system and in measuring and transmitting the assembly and adjustment references for the entire system. Traditional optical system assembly and adjustment methods cannot meet the assembly and adjustment requirements of this composite detection system.

Method used

A lidar and laser tracker are used to establish an assembly and adjustment benchmark. Combined with a four-axis turntable, collimator, infrared blackbody and PI hexapod platform, a multi-stage assembly and adjustment strategy is adopted to achieve precise positioning and rapid adjustment of the infrared detection system. This includes establishing a global coordinate system for assembly and adjustment, benchmark transfer, calculation of component position and orientation, and iterative feedback optimization assembly and adjustment.

Benefits of technology

It improves the accuracy and efficiency of assembly and adjustment, reduces the difficulty and cost of assembly and adjustment, ensures the imaging quality of the system, and overcomes the problems of strong subjectivity and low efficiency in traditional methods.

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Abstract

本发明提供了一种静止轨道微波‑红外复合探测系统共光路装调方法及系统,方法通过激光雷达扫描微波副反射面面型建立装调全局坐标系,利用激光测量靶球统一激光跟踪仪与激光雷达测量坐标系;经激光跟踪仪测量并装调红外折镜、汇聚透镜组件至设计位置,通过四轴转台调节平行光管对准成像光路搭建检测光路;将红外后光路组件装于PI六足平台,结合红外图像调制传递函数值迭代调节至成像达标,最后紧固组件完成装调。系统设对应六大功能模块执行该方法。本发明实现复杂光路精密对准,装调精度与效率高,工程易实现、可操作性强,适用于该复合探测系统共光路装调。
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Citation Information

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