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Design of the Front End Electronics for the Infrared Camera of JEM-EUSO, and manufacturing and verification of the prototype model

机译:JEM-EUSO红外摄像机的前端电子设备的设计,以及原型模型的制造和验证

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The Japanese Experiment Module (JEM) Extreme Universe Space Observatory (EUSO) will be launched and attached to the Japanese module of the International Space Station (ISS). Its aim is to observe UV photon tracks produced by ultra-high energy cosmic rays developing in the atmosphere and producing extensive air showers. The key element of the instrument is a very wide-field, very fast, large-lense telescope that can detect extreme energy particles with energy above 10~(19) eV. The Atmospheric Monitoring System (AMS), comprising, among others, the Infrared Camera (IRCAM), which is the Spanish contribution, plays a fundamental role in the understanding of the atmospheric conditions in the Field of View (FoV) of the telescope. It is used to detect the temperature of clouds and to obtain the cloud coverage and cloud top altitude during the observation period of the JEM-EUSO main instrument. SENER is responsible for the preliminary design of the Front End Electronics (FEE) of the Infrared Camera, based on an uncooled microbolometer, and the manufacturing and verification of the prototype model. This paper describes the flight design drivers and key factors to achieve the target features, namely, detector biasing with electrical noise better than 100μV from 1Hz to 10MHz, temperature control of the microbolometer, from 10°C to 40°C with stability better than 10mK over 4.8hours, low noise high bandwidth amplifier adaptation of the microbolometer output to differential input before analog to digital conversion, housekeeping generation, microbolometer control, and image accumulation for noise reduction. It also shows the modifications implemented in the FEE prototype design to perform a trade-off of different technologies, such as the convenience of using linear or switched regulation for the temperature control, the possibility to check the camera performances when both microbolometer and analog electronics are moved further away from the power and digital electronics, and the addition of switching regulators to demonstrate the design is immune to the electrical noise the switching converters introduce. Finally, the results obtained during the verification phase are presented: FEE limitations, verification results, including FEE noise for each channel and its equivalent NETD and microbolometer temperature stability achieved, technologies trade-off, lessons learnt, and design improvement to implement in future project phases.
机译:日本实验模块(JEM)极端宇宙空间天文台(EUSO)将推出并附在国际空间站(ISS)的日本模块上。其目的是观察由超高能量宇宙射线在大气中发育的UV光子轨迹,并产生广泛的空气淋浴。仪器的关键元件是一个非常宽的领域,非常快速,大的大望远镜,可以检测10〜(19)EV高于10〜(19)EV的能量。包括在其他人的大气监测系统(AMS),其中包括西班牙贡献的红外线相机(IRCAM)在理解望远镜的视野(FOV)的大气条件下起着重要作用。它用于检测云的温度,并在JEM-EUSO主仪器的观察期间获得云覆盖率和云顶级海拔。参赛者负责基于未处理的微泡计的红外相机的前端电子设备(费用)的初步设计,以及原型模型的制造和验证。本文介绍了实现目标特征的飞行设计驱动因素和关键因素,即探测器偏置电噪声,从1Hz到10MHz,微多升压器的温度控制,从10°C到40°C,稳定性优于10MK超过4.8小时,低噪声高带宽放大器适应微增压仪输出到差分输入,以便模拟到数字转换,家政一代,微汽力计控制和图像累积进行降噪。它还显示了在费用原型设计中实现的修改,以执行不同技术的权衡,例如使用线性或切换调节对温度控制的便利性,当微电位器和模拟电子器件都有时检查相机性能的可能性远离电源和数字电子产品,并添加开关调节器以证明设计的展示对电气噪声引入的电噪声。最后,提出了在验证阶段期间获得的结果:费用限制,验证结果,包括每个通道的费用噪声以及其等效的NetD和微致电计温度稳定性,技术权衡,经验教训和在未来项目中实施的设计改进和设计改进阶段。

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