月球表面导航伪卫星试验台研制

Brodie Wallace, Scott Palo, Penina Axelrad, John Marino, Nicholas Rainville, Ryan Kingsbury, Julia DiTomas, Mazen Shihabi, Dennis Ogbe
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引用次数: 0

摘要

在过去的几年里,随着美国宇航局致力于将宇航员送回月球表面,人们对月球的兴趣显著增加。从历史上看,月球任务主要由地球上的地面站支持,用于通信和无线电导航。然而,拟议的月球探测、科学和商业任务的数量和范围需要原位基础设施来提供持续的通信支持和精确导航服务。我们提出了一种基于月球表面的定位、导航和授时(PNT)和紧急广播伪卫星系统,作为一种经济有效的解决方案,以支持勘探关键区域的区域操作,并且已经探索了架构设计特征,定义了伪卫星操作概念,并确定了潜在的导航性能。这项研究的重点是开发一个月球伪卫星试验台,其主要目标有两个:展示月球表面通信和无线电导航技术,以及表征支持月球操作的低成本、商用射频(RF)硬件替代方案的性能。该工作包括四个主要阶段:(1)地面伪卫星试验台的集成;(2)在台式环境中开发和测试通信和无线电导航协议;(3)用不同的参考振荡器表征相对距离和时间同步性能;(4)使用多个伪卫星单元进行空中演示。伪随机噪声(PRN)码测距是一种基线相对定位方法,通过修改开源的全球导航卫星系统(GNSS)软件引擎获得信号跟踪、距离估计和绝对位置估计。硬件测试对测距性能进行了表征,平均测距误差小于1.3米,主要由时间同步偏移驱动。初步测试表明,低SWaP伪卫星可以在关键的月球区域提供通信覆盖和< 10米误差的绝对定位精度,有助于启动月球表面的探索和商业化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of a Lunar Surface Navigation Pseudolite Testbed
Interest in the Moon has grown significantly over the past few years as NASA works to return astronauts to the lunar surface. Historically, lunar missions have primarily been supported by Earth-based ground stations for communication and radionavigation. However, the quantity and scope of proposed lunar exploration, science, and commercial missions require in-situ infrastructure for continuous communication support and precision navigation services. We propose a lunar surface-based Position, Navigation, and Timing (PNT) and emergency broadcast pseudolite system as a cost-effective solution to support regional operations over exploration critical areas, and have previously explored architecture design characteristics, defined the pseudolite concept of operations, and identified potential navigation performance. This research is focused on developing a lunar pseudolite testbed with two primary objectives: demonstrating lunar surface communication and radionavigation techniques and characterizing the performance of low-cost, commercially available radio frequency (RF) hardware alternatives for supporting lunar operations. The work is comprised of four primary phases: (1) integration of the terrestrial pseudolite testbed, (2) development and testing of the communication and radionavigation protocols in a benchtop environment, (3) characterizing the relative range and time synchronization performance with different reference oscillators, and (4) over-the-air demonstrations with multiple pseudolite units. Pseudorandom noise (PRN) code ranging is the baseline relative positioning methodology, with signal tracking, range estimation, and absolute position estimates obtained by modifying open-source Global Navigation Satellite System (GNSS) software engines. Hardware tests were conducted to characterize the ranging performance, with average range error of less than 1.3 meters, primarily driven by time synchronization offsets. Initial tests demonstrate how low SWaP pseudolites can provide communication coverage and < 10 m error absolute positioning accuracy over critical lunar regions, helping to jumpstart exploration and commercialization on the lunar surface.
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