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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 lHz 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:日本实验舱(JEM)极端宇宙空间天文台(EUSO)将启动,并附加到国际空间站(ISS)的日本舱中。它的目的是观察由超高能宇宙射线在大气中发展并产生大量的风淋而产生的紫外线光子轨迹。仪器的关键元件是一个非常宽的视野,非常快的大型望远镜,可以检测能量高于10〜(19)eV的极端能量粒子。大气监测系统(AMS)包括西班牙的贡献,其中包括红外摄像机(IRCAM),在理解望远镜视场(FoV)中的大气条件方面起着根本性的作用。在JEM-EUSO主仪器的观测期内,它用于检测云的温度并获取云的覆盖范围和云顶高度。 SENER负责基于未冷却微测辐射热计的红外摄像机前端电子(FEE)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功能的飞行设计驱动力和关键因素,即探测器的偏置在1Hz至10MHz范围内的电噪声优于100μV,微测辐射热计的温度控制在10°C至40°C,稳定性优于10mK在4.8个小时内,低噪声高带宽放大器将微辐射热测量仪的输出适配为差分输入,然后进行模数转换,内务处理生成,微辐射热测量仪控制和图像积累,以降低噪声。它还显示了在FEE原型设计中实施的修改,以执行不同技术之间的权衡,例如使用线性或开关调节进行温度控制的便利性,以及在微测辐射热计和模拟电子设备均被使用时检查相机性能的可能性。进一步远离电源和数字电子设备,并且增加了开关稳压器以证明该设计不受开关转换器引入的电子噪声的影响。最后,介绍了在验证阶段获得的结果:FEE限制,验证结果,包括每个通道的FEE噪声及其等效的NETD和测微辐射热计温度稳定性,技术折衷,经验教训以及在未来项目中实施的设计改进阶段。

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