CCD真空低温光电快速测试系统的设计与验证OA
Design and verification of a fast vacuum cryogenic optoelectronic test system for CCD
星载科学级CCD成像电路需要精密调配多种参数,以期达到最佳效果.成像电路设计过程中需要根据实测结果去优化这些参数,其中的一些实验需在低温真空下进行.而传统测试设备体积大、热循环耗时长.本文研制了一套小型化的杜瓦装置,以适应CCD电路测试的需求.首先,搭建了"无油高真空+脉管制冷机+精密温控"的系统架构.接着,通过抽气动力学与冷量传递实验验证了系统性能.然后,依托该系统便捷装调的特性,快速迭代前端电路参数.最后,采用光子转移曲线(PTC)法,对CCD275分别在常温(298 K)和在轨低温(248 K)下进行对比实验,评估了不同参数在实现满阱读出时的效果.系统实现了优于5.0×10-5 Pa的极限真空及带载215 K的测试环境,具备快速抽排气、无需液氮、方便装调的优势.实验测定6片CCD275在 248 K低温@2.5 MHz读出频率下的有效满阱达到800~900 k e-/pixel/s.该系统大幅提升了CCD真空低温测试与参数迭代的效率,其测试结果满足卫星总体对信噪比和动态范围的要求,为未来更多科学级CCD的综合调试提供了一个高效、通用的系统解决方案.
A spaceborne scientific CCD(Charge-Coupled Device)needs a well-adapted peripheral circuit to achieve its best performance.In the design of peripheral imaging circuits,several parameters—such as series resistors,offset voltages,the overlap of driving clocks,etc.—must be optimized according to the feedback of actual tests.Some tests must be conducted under low-temperature conditions to match the en-vironment where the CCD is to be finally installed.Such low-temperature vacuum equipment previously used was designed for entire payloads,making it too bulky for individual CCD devices and front-end cir-cuits.Due to this bulky size,it took extra time and cost a huge amount of liquid nitrogen.Thus,a com-pact,cryocooler-based Dewar was designed in this paper.First,a system composed of an oil-free vacuum unit,a pulse tube cryocooler,and a precise temperature control unit was built.Then,the performance of the system was verified through vacuum pumping dynamics and cold-transfer experiments.Next,with the test system,the circuit parameters were modified and optimized according to the feedback of the experi-ments,which were rapidly repeated several times by taking advantage of the"quick-operation"feature of the test system.Finally,utilizing the photon transfer curve(PTC)method,comparative experiments were conducted on the CCD275 at both room temperature(298 K)and the on-orbit operating temperature(248 K)to evaluate the effectiveness of different parameters in achieving full-well readout.The system achieves an ultimate vacuum of better than 5.0×10-5 Pa and sustains a stable testing environment of 215 K under thermal load,offering rapid evacuation,low cost,convenient installation,and a dedicated design for CCD circuit tests.The tests and measurements on six CCD275 chips show that the effective full-well capacities are in the range of 800 000 to 900 000 electrons per pixel at 248 K with a readout frequency of 2.5 MHz.This system significantly enhances the efficiency of CCD testing and circuit modifications.The test results meet the application requirements for the signal-to-noise ratio and dynamic range.In conclu-sion,this paper discusses the design and implementation of the test system,providing a convenient and versatile testing and debugging solution for scientific-grade CCDs.
刘国华;杨森;王煜;林方
安徽大学 物质科学与信息技术研究院,安徽 合肥 230601中国科学院 西安光学精密机械研究所,陕西 西安 710119安徽大学 物质科学与信息技术研究院,安徽 合肥 230601中国科学院 安徽光学精密机械研究所,安徽 合肥 230031
信息技术与安全科学
星载CCD真空低温系统光子转移曲线(PTC)满阱容量高效测试
spaceborne CCDvacuum cryogenic systemPhoton Transfer Curve(PTC)full well ca-pacityhigh-efficiency testing
《光学精密工程》 2026 (14)
2192-2203,12
安徽省青年基金项目(No.2108085QF283)国家重点研发项目(No.2024YFC3712905)
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