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EXTREME ACCURACY STAR TRACKER IN SUPPORT OF HYPER PRECISION COLD ATOM INTERFEROMETRY

机译:支持超精密冷原子干涉测量的极端精度明星跟踪器

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HYPER stands for Hyper-precision cold atom interferometry in space. HYPER is a potential Future Flexi-mission of the European Space Agency, ESA, in the fundamental physics domain. Following a preliminary feasibility study (Ref 1) conducted in the Concurrent Design Facility of the European Space Technology Center, ESTEC, which was supported by Professor W. Ertmer of the "Institut fuer Quantenoptik, Hanover" and his team of scientists, ESA awarded Astrium Germany and its industrial team with a "follow-on" Feasibility Study Contract. As part of this team, Galileo Avionica was responsible for the design and performance requirements simulation of the optical bench and precision star tracker, two of the components at the heart of the HYPER payload. This paper provides first of all an essential but quick introduction to cold atom-wave interferometry which is at the core of the high-performance HYPER pay-load and provides the capability of measuring accelerations and rotations with extremely high accuracy. A summary of the scientific mission objectives, which entail the repeated measurement of extremely small rotations and accelerations over at least one-year period with respect to an inertial reference frame, is described. Thereafter, a short resume of the main mission requirements is given. Among these requirements are two "critical" requirements, which dominate the overall spacecraft design: 1. The superior thermo-mechanical stability between the HYPER instruments and a Precision Star Tracker, PST, which provides the inertial attitude reference in science mode (Spectral Density=2.75x10~(10) rad/Hz~(-0.5), in the frequency range between 3.2x10~(-5) Hz and 0.15 Hz); 2. The PST Absolute Measurement Accuracy (Spectral Density=1.75x10~(-9) rad/Hz~(-0.5), in the frequency range between 3.2x10~(-5) Hz and 5 Hz). Finally, this paper highlights the challenges the Industrial Team faced in meeting those requirements and describes the optical design of this extremely accurate Precision Star Tracker. The preliminary results of the performance requirements simulation are also presented.
机译:超高精度的高精度冷原子干涉测量法。超级是欧洲航天局的潜在未来的Flexi-Mission,ESA,在基本物理领域。在欧洲空间技术中心的并发设计设施中进行的初步可行性研究(REF 1),ESTEC在“Institut Fuer Quantenoptik,Hanover”和他的科学家团队,ESA授予Astrium德国及其工业团队“有关”可行性研究合同。作为这支球队的一部分,伽利略航空公司负责光学台面和精密星跟踪器的设计和性能要求,在高效载荷的核心中的两个组件。本文首先所有的必要但快速介绍冷原子波干涉测量其在高性能HYPER付费负载的核心,并提供了一种测量加速度和旋转精度非常高的能力的提供。描述了科学任务目标的概述,其需要在相对于惯性参考框架上至少一年的时间内重复测量极小的旋转和加速度。此后,给出了主要任务要求的简短简历。这些要求是两个“关键”要求,这些要求主导了整体航天器设计:1。高仪器和精密星跟踪器,PST之间的卓越热机械稳定性,为科学模式提供了惯性姿态参考(光谱密度= 2.75x10〜(10)rad / hz〜(-0.5),频率范围为3.2x10〜(-5)Hz和0.15 Hz); 2. PST绝对测量精度(光谱密度= 1.75x10〜(-9)Rad / Hz〜(-0.5),在3.2x10〜(-5)Hz和5 Hz之间的频率范围内。最后,本文突出了工业团队面临的挑战,迎接这些要求,并描述了这款极其准确的精确明星跟踪器的光学设计。还提出了性能要求仿真的初步结果。

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