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Lessons learned from systems engineering on the James Webb Space Telescope 詹姆斯-韦伯太空望远镜系统工程的经验教训
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-02-01 DOI: 10.1117/1.jatis.10.1.011208
Michael Menzel, Keith Parrish, Lee Feinberg, Paul Geithner, Julie Van Campen, Michael McElwain, Sandra Irish
The James Webb Space Telescope is NASA’s flagship mission and successor to the highly successful Hubble Space Telescope. It is an infrared observatory featuring a cryogenic 6.6 m aperture, deployable optical telescope element with a payload of four science instruments assembled into an integrated science instrument module that provide imagery and spectroscopy in the near infrared band between 0.6 and 5 μm and in the mid-infrared band between 5 and 28 μm. JWST was successfully launched on December 25, 2021, aboard an Ariane 5 launch vehicle. All 50 major deployments were successfully completed by January 8, 2022. The observatory performed all mid-course correction maneuvers and achieved its operational mission orbit around the Sun-Earth second Lagrange Point. All commissioning and calibration activities have been completed and JWST has begun its science mission. Its present performance meets or out-performs all requirements. Launching over 20 years after its mission concept review, the JWST Observatory is a first and only of its kind of facility. This program faced many unique challenges that were not only technical in nature but also organizational and managerial. We describe the challenges faced by the JWST systems engineering team, the way the team addressed them, and make recommendations for focus areas of future flagship missions, which will likely face similar challenges. It will not explicitly address the cost challenges of the mission. We first describe the mission and its over-arching challenges. We then describe the tailoring of systems engineering processes and methods used to address these challenges and effectiveness. The events, tasks, issues, and their resolutions and the resulting specific lessons learned from the project are discussed with the over-arching recommendations for future flagship missions that derive from these lessons.
詹姆斯-韦伯太空望远镜是美国国家航空航天局的旗舰任务,也是非常成功的哈勃太空望远镜的后继者。它是一个红外观测站,具有一个 6.6 米孔径的低温可展开光学望远镜组件,其有效载荷包括组装成一个综合科学仪器模块的四台科学仪器,可提供 0.6 至 5 μm 近红外波段和 5 至 28 μm 中红外波段的图像和光谱。JWST 于 2021 年 12 月 25 日由阿丽亚娜 5 号运载火箭成功发射。截至 2022 年 1 月 8 日,所有 50 项主要部署均已顺利完成。观测站进行了所有的中途修正机动,并实现了围绕日地第二拉格朗日点的运行任务轨道。所有调试和校准活动均已完成,JWST 已开始执行科学任务。其目前的性能达到或超过了所有要求。JWST 天文台在其任务概念审查 20 多年后才发射,是第一个也是唯一一个同类设施。该计划面临着许多独特的挑战,不仅是技术方面的,还有组织和管理方面的。我们介绍了 JWST 系统工程团队所面临的挑战、团队应对这些挑战的方法,并对未来旗舰任务的重点领域提出了建议,未来的旗舰任务可能也会面临类似的挑战。本报告不会明确讨论该任务的成本挑战。我们首先介绍这项任务及其面临的主要挑战。然后,我们将介绍为应对这些挑战而量身定制的系统工程流程和方法,以及这些流程和方法的有效性。我们还讨论了事件、任务、问题及其解决方案,以及从该项目中汲取的具体经验教训,并从这些经验教训中为未来的旗舰任务提出了总体建议。
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引用次数: 0
Spectral characterization of the Grism and Prism slitless spectrometers for the Nancy Grace Roman Space Telescope 南希-格蕾丝-罗曼太空望远镜的光栅和棱镜无缝分光计的光谱特性分析
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-02-01 DOI: 10.1117/1.jatis.10.1.014003
Evan Bray, Mateo Batkis, Victor J. Chambers, Margaret Dominguez, Bente Eegholm, Guangjun Gao, Qian Gong, Wesley Halliday, Elias Howe, Jeffrey Kruk, Eliot Malumuth, Sangeeta Malhotra, Catherine Marx, James Rhoads, Maxime Rizzo, Joshua E. Schlieder, Laurie Seide, Eric R. Switzer, Jay Voris
The Roman Space Telescope Grism and Prism assemblies will allow the wide-field instrument (WFI) to perform slitless, multi-object spectroscopy across the complete field of view. These optical elements play a critical role in the High Latitude Wide Area and High Latitude Time Domain Surveys, which are designed to produce robust spectroscopic redshifts for millions of objects over the mission lifetime. To facilitate the characterization of these assemblies, a dedicated test bed was designed and utilized to perform a wide variety of spectroscopic measurements over the full range of operational wavelengths and field angles. Characterized features include, but are not limited to dispersion magnitude, dispersion clocking, encircled energy, total throughput, and bandpass edges. We present the results of this experimental campaign in which the Grism and Prism assemblies met or exceeded many of their design requirements and discuss measurement limitations.
罗曼太空望远镜的光栅和棱镜组件将使宽视场仪器(WFI)能够在整个视场内进行无缝多天体分光。这些光学元件在高纬度广域巡天和高纬度时域巡天中发挥着至关重要的作用,这两项巡天的目的是在飞行任务有效期内为数百万个天体产生可靠的光谱红移。为了便于对这些组件进行特征描述,设计并使用了一个专用的测试平台,以便在全部工作波长和场角度范围内进行各种光谱测量。表征的特征包括但不限于色散幅度、色散时钟、环绕能量、总吞吐量和带通边缘。我们介绍了这次实验活动的结果,其中 "光栅 "和 "棱镜 "组件达到或超过了许多设计要求,并讨论了测量的局限性。
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引用次数: 0
Benefits of adding radial phase dimples on scalar coronagraph phase masks 在标量日冕仪相位掩模上添加径向相位凹坑的好处
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-02-01 DOI: 10.1117/1.jatis.10.1.015001
Niyati Desai, Dimitri Mawet, Eugene Serabyn, Garreth Ruane, Arielle Bertrou-Cantou, Jorge Llop-Sayson, A. J. Eldorado Riggs
Current scalar coronagraph focal plane mask designs are performance-limited by chromaticity. We investigate the effects of adding central Roddier and dual zone phase dimples to scalar masks to improve broadband performance by suppressing the chromatic stellar leakage. We present hybrid designs with radial phase dimples integrated with the sawtooth vortex, wrapped vortex, and cosine phase mask. We show that, using these dimples, it is possible to substantially improve the broadband contrast performance of scalar phase masks. We also show that, although adding a phase dimple does not increase the sensitivity to low-order aberrations, suppressing the central leakage of scalar vortex coronagraphs does not restore the aberration sensitivities to their notional state.
目前的标量日冕仪焦平面掩膜设计受到色度的性能限制。我们研究了在标量掩膜上添加中央罗迪尔和双区相位凹点的效果,以通过抑制色度恒星泄漏来提高宽带性能。我们提出了将径向相位凹点与锯齿涡、包裹涡和余弦相位掩模集成在一起的混合设计。我们的研究表明,利用这些凹点,可以大幅提高标量相位掩模的宽带对比度性能。我们还表明,虽然增加一个相位窝不会提高对低阶像差的灵敏度,但抑制标量漩涡日冕仪的中心泄漏并不能将像差灵敏度恢复到理论状态。
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引用次数: 0
Laboratory experiments of model-based reinforcement learning for adaptive optics control 基于模型强化学习的自适应光学控制实验室实验
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-02-01 DOI: 10.1117/1.jatis.10.1.019001
Jalo Nousiainen, Byron Engler, Markus Kasper, Chang Rajani, Tapio Helin, Cédric T. Heritier, Sascha P. Quanz, Adrian M. Glauser
Direct imaging of Earth-like exoplanets is one of the most prominent scientific drivers of the next generation of ground-based telescopes. Typically, Earth-like exoplanets are located at small angular separations from their host stars, making their detection difficult. Consequently, the adaptive optics (AO) system’s control algorithm must be carefully designed to distinguish the exoplanet from the residual light produced by the host star. A promising avenue of research to improve AO control builds on data-driven control methods, such as reinforcement learning (RL). RL is an active branch of the machine learning research field, where control of a system is learned through interaction with the environment. Thus, RL can be seen as an automated approach to AO control, where its usage is entirely a turnkey operation. In particular, model-based RL has been shown to cope with temporal and misregistration errors. Similarly, it has been demonstrated to adapt to nonlinear wavefront sensing while being efficient in training and execution. In this work, we implement and adapt an RL method called policy optimization for AO (PO4AO) to the GPU-based high-order adaptive optics testbench (GHOST) test bench at ESO headquarters, where we demonstrate a strong performance of the method in a laboratory environment. Our implementation allows the training to be performed parallel to inference, which is crucial for on-sky operation. In particular, we study the predictive and self-calibrating aspects of the method. The new implementation on GHOST running PyTorch introduces only around 700 μs of in addition to hardware, pipeline, and Python interface latency. We open-source well-documented code for the implementation and specify the requirements for the RTC pipeline. We also discuss the important hyperparameters of the method and how they affect the method. Further, the paper discusses the source of the latency and the possible paths for a lower latency implementation.
类地系外行星的直接成像是下一代地基望远镜最突出的科学驱动力之一。通常情况下,类地系外行星与其宿主恒星的角距很小,因此很难对其进行探测。因此,自适应光学(AO)系统的控制算法必须经过精心设计,以便将系外行星与主恒星产生的残余光区分开来。改进自适应光学系统控制的一个很有前途的研究方向是数据驱动控制方法,如强化学习(RL)。强化学习是机器学习研究领域的一个活跃分支,通过与环境的交互来学习对系统的控制。因此,RL 可以被看作是一种自动运行控制方法,其使用完全是一种交钥匙操作。特别是,基于模型的 RL 已被证明可以应对时间和错误注册错误。同样,它也被证明能适应非线性波前传感,同时在训练和执行方面也很高效。在这项工作中,我们实施了一种名为 "AO 策略优化"(PO4AO)的 RL 方法,并将其应用于欧洲南方天文台总部基于 GPU 的高阶自适应光学测试台(GHOST)。我们的实施允许训练与推理并行进行,这对于在天空运行至关重要。我们特别研究了该方法的预测和自校准方面。在运行 PyTorch 的 GHOST 上实现的新方法,除了硬件、流水线和 Python 接口延迟外,只引入了大约 700 μs 的延迟。我们为该方法的实现开源了文档齐全的代码,并明确了对 RTC 管道的要求。我们还讨论了该方法的重要超参数及其对该方法的影响。此外,本文还讨论了延迟的来源以及实现更低延迟的可能途径。
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引用次数: 0
Asgard/NOTT: L-band nulling interferometry at the VLTI. II. Warm optical design and injection system Asgard/NOTT:VLTI 的 L 波段归零干涉测量。II.暖光学设计和注入系统
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-02-01 DOI: 10.1117/1.jatis.10.1.015002
Germain Garreau, Azzurra Bigioli, Romain Laugier, Gert Raskin, Johan Morren, Jean-Philippe Berger, Colin Dandumont, Harry-Dean Kenchington Goldsmith, Simon Gross, Michael Ireland, Lucas Labadie, Jérôme Loicq, Stephen Madden, Guillermo Martin, Marc-Antoine Martinod, Alexandra Mazzoli, Ahmed Sanny, Hancheng Shao, Kunlun Yan, Denis Defrère
Asgard/NOTT (previously Hi-5) is a European Research Council (ERC)-funded project hosted at KU Leuven and a new visitor instrument for the Very Large Telescope Interferometer (VLTI). Its primary goal is to image the snow line region around young stars using nulling interferometry in the L′-band (3.5 to 4.0) μm, where the contrast between exoplanets and their host stars is advantageous. The breakthrough is the use of a photonic beam combiner, which only recently allowed the required theoretical raw contrast of 10−3 in this spectral range. Nulling interferometry observations of exoplanets also require a high degree of balancing between the four pupils of the VLTI in terms of intensity, phase, and polarization. The injection into the beam combiner and the requirements of nulling interferometry are driving the design of the warm optics and the injection system. The optical design up to the beam combiner is presented. It offers a technical solution to efficiently couple the light from the VLTI into the beam combiner. During the coupling, the objective is to limit throughput losses to 5% of the best expected efficiency for the injection. To achieve this, a list of different loss sources is considered with their respective impact on the injection efficiency. Solutions are also proposed to meet the requirements of beam balancing for intensity, phase, and polarization. The different properties of the design are listed, including the optics used, their alignment and tolerances, and their impact on the instrumental performances in terms of throughput and null depth. The performance evaluation gives an expected throughput loss <6.4% of the best efficiency for the injection and a null depth of ∼2.10−3, mainly from optical path delay errors outside the scope of this work.
Asgard/NOTT(前身为Hi-5)是欧洲研究理事会(ERC)资助的一个项目,由鲁汶大学主持,是甚大望远镜干涉仪(VLTI)的一个新访客仪器。该项目的主要目标是利用 L′波段(3.5 至 4.0)μm 的消隐干涉测量法对年轻恒星周围的雪线区域进行成像,因为系外行星与其宿主恒星之间的对比度在该波段具有优势。突破性进展是使用了光子合束器,该合束器直到最近才能够在这一光谱范围内达到所需的 10-3 的理论原始对比度。系外行星的消隐干涉测量观测还要求 VLTI 的四个瞳孔在强度、相位和偏振方面保持高度平衡。向合束器注入光束和消隐干涉测量的要求推动了暖光学和注入系统的设计。本文介绍了直至合束器的光学设计。它提供了将 VLTI 的光有效耦合到合束仪的技术解决方案。在耦合过程中,目标是将吞吐量损失限制在最佳预期注入效率的 5%。为实现这一目标,考虑了一系列不同的损耗源及其对注入效率的影响。此外,还提出了一些解决方案,以满足光束平衡对强度、相位和偏振的要求。还列出了设计的不同特性,包括所使用的光学器件、它们的校准和公差,以及它们在吞吐量和无效深度方面对仪器性能的影响。性能评估结果表明,预计注入的吞吐量损失小于最佳效率的 6.4%,空洞深度为 2.10-3 ∼,主要来自本工作范围之外的光路延迟误差。
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引用次数: 0
Reflectance properties of the Acktar Magic Black™ coating for the radiation near the Lyman-α line of hydrogen: measurements and phenomenological model of the BRDF 阿克塔尔 Magic Black™ 涂层对氢的莱曼-α 线附近辐射的反射特性:测量结果和 BRDF 现象模型
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-02-01 DOI: 10.1117/1.jatis.10.1.018004
Marek Strumik, Martyna Wardzińska, Maciej Bzowski, Przemysław Wachulak, Roman Wawrzaszek, Tomasz Fok, Andrzej Bartnik, Karol Mostowy, Henryk Fiedorowicz, Łukasz Węgrzyński, Mateusz Majszyk
Optical surfaces of space instruments usually need to be blackened to minimize adverse effects affecting their performance in photometric, spectrometric, and imaging applications. Blackening is often obtained by application of coatings that strongly absorb the incoming photon flux and diffusively scatter the incident photons. We discuss reflectance measurements and a phenomenological model of the bidirectional reflectance distribution function (BRDF) for the Magic Black™ coating, which is a commercial product supplied by the Acktar company. The coating has a vast satellite-instrument heritage and is planned to be used in the GLOWS photometer onboard the upcoming NASA Interstellar Mapping and Acceleration Probe nmission. The reflectance measurements were conducted at ∼121.6 nm, corresponding to the Lyman-α line for hydrogen, which is important in astrophysics. This line is commonly considered a crossover between the far ultraviolet and extreme ultraviolet spectral ranges. To generate radiation in this range, a laser-plasma source based on the gas-puff target was used. Six samples coated with Acktar Magic Black™ were studied in an optical system with a back-illuminated CCD camera as a detector. The measurements were used to derive the phenomenological BRDF model based on a series of analytic fits to the measurements, which makes it easily applicable in both numerical simulations and manual calculations. The formulas provide an approximation in the full hemispheric domain, i.e., both for the in-specular-plane and out-of-specular-plane behaviors of the BRDF for the coating. A similar fit-based phenomenological model is also described for the visible range (the wavelength of 532 nm) as a byproduct of our analysis for the UV range.
空间仪器的光学表面通常需要进行黑化处理,以尽量减少影响其光度、光谱和成像应用性能的不利影响。黑化通常是通过使用能强烈吸收入射光子通量并扩散散射入射光子的涂层来实现的。我们将讨论 Magic Black™ 涂层的反射率测量结果和双向反射率分布函数 (BRDF) 现象模型。该涂层拥有大量的卫星仪器遗产,计划用于即将发射的美国宇航局星际绘图和加速探测器上的GLOWS光度计。反射率测量是在∼121.6 nm处进行的,与天体物理学中重要的氢的莱曼-α线相对应。这条线通常被认为是远紫外和极紫外光谱范围的交叉点。为了产生这一范围内的辐射,我们使用了基于气泡目标的激光等离子体源。在一个光学系统中对六个涂有 Acktar Magic Black™ 涂层的样品进行了研究,该系统使用背照式 CCD 相机作为探测器。测量结果被用于推导基于一系列分析拟合测量结果的现象 BRDF 模型,这使得该模型易于应用于数值模拟和手动计算。这些公式提供了全半球域的近似值,即对涂层的镜内平面和镜外平面 BRDF 行为都提供了近似值。我们还为可见光范围(波长为 532 nm)描述了类似的拟合现象模型,作为我们对紫外范围分析的副产品。
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引用次数: 0
Pathfinder value for integration and test of the Webb Telescope optical system 韦伯望远镜光学系统集成和测试的开拓者价值
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-01-01 DOI: 10.1117/1.jatis.10.1.011206
Tony L. Whitman
The James Webb Space Telescope has extended our knowledge of the universe since the first images appeared last year with optical performance reaching the diffraction limit. The optical alignment and quality were tested prior to launch at cryogenic temperatures with a complex test configuration for this unique telescope architecture. This article reviews the strategic choices for pathfinding the integration and test processes for this telescope and the lessons learned prior to integrating and testing the flight hardware, leading to a successful integration and test campaign of the flight telescope. The biggest lesson was learning the value of investing in pathfinding integration and test activities.
詹姆斯-韦伯太空望远镜的光学性能达到了衍射极限,自去年第一批图像问世以来,它扩展了我们对宇宙的认识。在发射前,我们在低温条件下对光学对准和质量进行了测试,并针对这种独特的望远镜结构进行了复杂的测试配置。这篇文章回顾了为这台望远镜的集成和测试过程探路的战略选择,以及在集成和测试飞行硬件之前所吸取的经验教训,从而成功地完成了飞行望远镜的集成和测试活动。最大的教训是认识到投资于探路集成和测试活动的价值。
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引用次数: 0
2023 List of Reviewers 2023 年审查员名单
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-01-01 DOI: 10.1117/1.jatis.10.1.010102
JATIS thanks the reviewers who served the journal in 2023.
JATIS 感谢 2023 年为期刊服务的审稿人。
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引用次数: 0
Webb Space Telescope primary mirror development: summary and lessons learned 韦伯太空望远镜主镜开发:总结和经验教训
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-01-01 DOI: 10.1117/1.jatis.10.1.011207
H. Philip Stahl
The primary mirror is central to the success of the Webb Space Telescope and the product of 100s of engineers and technologists who invented technologies and processes for its manufacture and test. We summarize the Webb mirror technology development program, explain how the technology was demonstrated to be TRL-6 (including the importance of an Engineering Development Unit), and list some of the author’s personal lessons learned.
主反射镜是韦伯太空望远镜取得成功的核心,也是数百名工程师和技术人员的成果,他们发明了制造和测试主反射镜的技术和流程。我们总结了韦伯望远镜反射镜技术开发项目,解释了该技术是如何被证明达到 TRL-6 的(包括工程开发单位的重要性),并列出了作者个人的一些经验教训。
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引用次数: 0
Maunakea Spectroscopic Explorer exposure time calculator for end-to-end simulator: to optimizing spectrograph design and observing simulation 用于端到端模拟器的 Maunakea 光谱探测器曝光时间计算器:优化摄谱仪设计和观测模拟
IF 2.3 3区 工程技术 Q2 Engineering Pub Date : 2024-01-01 DOI: 10.1117/1.jatis.10.1.018001
Tae-Geun Ji, Jennifer Sobeck, Changgon Kim, Hojae Ahn, Mingyeong Yang, Taeeun Kim, Sungwook E. Hong, Kei Szeto, Jennifer L. Marshall, Christian Surace, Soojong Pak
The Maunakea Spectroscopic Explorer (MSE) project will provide multi-object spectroscopy in the optical and near-infrared bands using an 11.25-m aperture telescope, repurposing the original Canada–France–Hawaii Telescope site. MSE will observe 4332 objects per single exposure with a field of view of 1.5 square degrees, utilizing two spectrographs with low-moderate (R∼3000, 6000) and high (R≈30,000) spectral resolution. In general, an exposure time calculator (ETC) is used to estimate the performance of an observing system by calculating the signal- to-noise ratio (S/N) and exposure time. We present the design of the MSE ETC, which has four calculation modes (S/N, exposure time, S/N trend with wavelength, and S/N trend with magnitude) and incorporates the MSE system requirements as specified in the conceptual design. The MSE ETC currently allows for user-defined inputs of the target AB magnitude, water vapor, air mass, and sky brightness AB magnitude (additional user inputs can be provided depending on the computational mode). The ETC is built using Python 3.7 and features a graphical user interface that allows for cross-platform use. The development process of the ETC software follows an Agile methodology and utilizes the unified modeling language diagrams to visualize the software architecture. We also describe the testing and verification of the MSE ETC.
毛纳凯亚光谱探测器(MSE)项目将利用一台 11.25 米口径的望远镜,在光学和近红外波 段提供多天体光谱分析,该望远镜的原址是加拿大-法国-夏威夷望远镜原址。MSE 每次曝光将观测 4332 个天体,视场为 1.5 平方度,使用两台光谱分辨率为中低 (R∼3000,6000)和高(R≈30000)的摄谱仪。一般来说,曝光时间计算器(ETC)通过计算信噪比(S/N)和曝光时间来估算观测系统的性能。我们介绍了 MSE ETC 的设计,它有四种计算模式(信噪比、曝光时间、随波长变化的信噪比趋势和随幅值变化的信噪比趋势),并结合了概念设计中规定的 MSE 系统要求。MSE ETC 目前允许用户自定义输入目标 AB 级、水蒸气、空气质量和天空亮度 AB 级(根据计算模式还可提供其他用户输入)。ETC 使用 Python 3.7 构建,具有图形用户界面,可跨平台使用。ETC 软件的开发过程遵循敏捷方法学,并利用统一建模语言图表来实现软件架构的可视化。我们还介绍了 MSE ETC 的测试和验证。
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引用次数: 0
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Journal of Astronomical Telescopes Instruments and Systems
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