Early Artemis Surface Navigation: Challenges, Approaches, and Opportunities

Evan Anzalone, Lemuel Carpenter, Cheryl Gramling, Laurie Mann, Thomas Moody
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Abstract

The early Artemis missions represent the return of humanity to the surface of the Moon and provide opportunities for meeting early science and exploration goals. Position, Navigation, and Timing (PNT) capabilities are a fundamental element and inform operational design, flight rules, and the ability to meet these. This paper provides an overview of the needs, potential implementations, challenges, and concepts of operations in the initial human surface missions, Artemis III and IV. These early excursions are a crucial learning opportunity to gain more experience in the actual operational environment for Artemis V and beyond where exploration objectives and complexity increases. As part of the study, the team defined a threshold performance navigation requirement (including position and orientation) to meet crew safe return and assessed a breadth of navigation approaches that could be deployed to augment the crew’s baseline navigation capability. Data was collected in terms of size, mass, power, operational constraints, environment constraints, interface, and performance to define the technical metrics. Given these, the trade team conducted polling among the various Artemis Campaign elements to capture preference, integration challenges, and operational impacts. These were used to develop weightings and inform a ranked order of solutions across each of the early missions. The results of the study recommended augmenting the initial orientation capability with additional navigation sensors to provide coarse position and heading information to the crew to enable a safe contingency walk-back when out of video range. The team identified opportunities for embedding this hardware in future scenarios to provide an integrated solution. With the deployment of the LunaNet’s Lunar Augmented Navigation System, the crew will be able to maintain accurate real-time navigation knowledge with minimal physical impacts. Discussion of future testing and continued analysis is included in this paper. These forward plans and long-term architecture systems will enable a powerful navigation approach for orbiting and surface users, enabling a high level of scientific return and crew safety.
早期阿尔忒弥斯水面导航:挑战、方法和机遇
早期的阿尔忒弥斯任务代表了人类重返月球表面,并为实现早期的科学和探索目标提供了机会。定位、导航和授时(PNT)能力是一个基本要素,为作战设计、飞行规则和满足这些要求的能力提供信息。本文概述了最初的人类表面任务,阿尔忒弥斯III和IV的需求、潜在实现、挑战和操作概念。这些早期的短途旅行是一个重要的学习机会,可以在阿尔忒弥斯V的实际操作环境中获得更多的经验,并且在探索目标和复杂性增加的情况下。作为研究的一部分,该团队定义了一个阈值性能导航要求(包括位置和方向),以满足机组人员的安全返回,并评估了可部署的导航方法的广度,以增强机组人员的基线导航能力。根据尺寸、质量、功率、操作约束、环境约束、接口和性能收集数据,以定义技术指标。考虑到这些,贸易团队对各种Artemis Campaign元素进行了民意调查,以获取偏好、整合挑战和操作影响。这些数据被用来制定权重,并为每个早期任务的解决方案排序。研究结果建议使用额外的导航传感器来增强初始定位能力,为机组人员提供粗略的位置和航向信息,以便在超出视频范围时安全返回。该团队确定了在未来场景中嵌入该硬件以提供集成解决方案的机会。随着LunaNet的月球增强导航系统的部署,机组人员将能够在最小的物理影响下保持准确的实时导航知识。本文还讨论了今后的测试和继续分析。这些前瞻性计划和长期架构系统将为轨道和地面用户提供强大的导航方法,从而实现高水平的科学返回和机组人员安全。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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