OSIRIS-REx光学导航的操作工具和数据管理

L. McCarthy, J. Pelgrift, Erik J. Lessac-Chennen, E. Sahr, B. Carcich, C. Adam, D. Nelson, R. Gaskell, D. Lauretta
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摘要

起源,光谱解释,资源识别和安全-风化层探测器(OSIRIS-REx)航天器于2016年9月发射,并于2018年底抵达其目标,近地小行星(101955)Bennu。在执行了近两年的多阶段接近操作导航和测绘活动后,2020年10月20日,OSIRIS-REx成功执行了触控操作(TAG)机动,成为美国第一个从小行星收集样本的任务。由于本努是有史以来行星航天器访问过的最小的物体之一,该任务提出了许多导航挑战,光学导航(OpNav)技术对任务的成功执行至关重要。OSIRIS-REx的具体挑战需要灵活的OpNav规划、强大的数据管理以及快速、自动化的分析和数据产品交付能力。除了两个主要的图像处理工具,基于质心和基于地标的OpNav,还开发了许多支持和规划工具和程序。OSIRIS-REx的多年作战时间表、快速机动节奏和多阶段近距离作战性质促使了简化和反应性图像规划过程。开发了一套工具,以确保不断满足任务导航要求。在接近时,使用Op-N机会分析仪(OpOpp)来消除来自明亮背景恒星干扰的成像计划的冲突。使用内部畸变校准工具集进行飞行仪表校准。使用曝光时间计算器来确定最佳曝光时间,并验证图像将产生足够的OpNav图像数据。此外,利用飞点射击(FPS)软件分析和缓解轨迹和指向不确定性对图像规划和覆盖的影响。本文进一步详细描述了OSIRIS-REx OpNav子系统的操作挑战,以及为确保满足导航需求而开发的工具、程序和策略。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Operational Tools and Data Management for OSIRIS-REx Optical Navigation
The Origins, Spectral Interpretation, Resource Identification, and Security-Regolith Explorer (OSIRIS-REx) spacecraft was launched in September 2016 and arrived at its target, near-Earth asteroid (101955) Bennu in late 2018. After executing nearly two years of multi-phase proximity operations navigation and mapping campaigns, on October 20, 2020 OSIRIS-REx successfully performed the Touch-And-Go (TAG) maneuver to become the first American mission to collect a sample from an asteroid. As Bennu is one of the smallest objects ever to be visited by a planetary spacecraft, the mission presented many navigational challenges, and optical navigation (OpNav) techniques were essential to the successful execution of the mission. The specific challenges of OSIRIS-REx required nimble OpNav planning, robust data management, and quick, automated analyses and data-product delivery capabilities. In addition to the two primary image processing tools, centroid-based and landmark-based OpNav, a host of support and planning tools and procedures were developed. The multi-year operations timeline, fast maneuver cadence, and multi-phase nature of proximity operations for OSIRIS-REx motivated a streamlined and reactive image planning process. A suite of tools was developed to ensure that the mission navigation requirements were continually satisfied. On approach, the Op-N av Opportunity Analyzer (OpOpp) was used to deconflict the imaging schedule with interference from bright background stars. In-flight instrument calibration was performed using an in-house distortion calibration toolset. An Exposure Time Calculator was used to determine optimal exposure times and verify that the images would produce sufficient OpNav image data. Additionally, Fly-Point-Shoot (FPS) software was used to analyze and mitigate the effect of trajectory and pointing uncertainties on image planning and coverage. This paper describes in further detail the operational challenges of the OSIRIS-REx OpNav subsystem, as well as the tools, procedures, and strategies developed to ensure the satisfaction of navigation requirements.
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