The Lunar GNSS Receiver Experiment (LuGRE)

J. Parker, F. Dovis, Benjamin Anderson, L. Ansalone, B. Ashman, F. Bauer, G. D'Amore, C. Facchinetti, S. Fantinato, G. Impresario, Stephen A. McKim, Efer Miotti, James J. Miller, M. Musmeci, O. Pozzobon, Lauren Schlenker, A. Tuozzi, Lisa M. Valencia
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引用次数: 16

Abstract

The Lunar GNSS Receiver Experiment (LuGRE) is a joint NASA-Italian Space Agency (ASI) payload on the Firefly Blue Ghost Mission 1 (BGM1) with the goal to demonstrate GNSS-based positioning, navigation, and timing at the Moon. LuGRE was chosen by the NASA Commercial Lunar Payload Services (CLPS) program as one of ten payloads on its “19D” task order for delivery to the lunar surface in 2023. The LuGRE payload consists of a weak-signal GNSS receiver, a high-gain L-band patch antenna, a low-noise amplifier, and an RF filter. The receiver will track GPS L1 C/A and L5, and Galileo E1 and E5a signals and will return pseudorange, carrier phase, and Doppler measurements to the ground. It will also calculate least-squares point solutions and Kalman-filter based navigation solutions onboard. In addition, the receiver features the capability to record raw I/Q baseband samples for downlink and ground processing. way for use by future lunar Gateway, robotic and human landers, and rovers. This paper provides a detailed overview of the LuGRE payload, including its design, concept of operations, and its predicted ability to meet its core science objectives. The baseline science investigations and priorities are outlined. Simulated performance results are shown based on the latest calibrated models including signal strength, signal availability, onboard navigation performance and convergence properties, and ground-based post-processed navigation performance.
月球GNSS接收机实验(LuGRE)
月球GNSS接收器实验(LuGRE)是美国宇航局和意大利航天局(ASI)在“萤火虫蓝幽灵”任务1 (BGM1)上的联合有效载荷,目的是在月球上演示基于GNSS的定位、导航和授时。LuGRE被美国宇航局商业月球有效载荷服务(CLPS)项目选中,作为其“19D”任务订单中的10个有效载荷之一,将于2023年交付到月球表面。LuGRE有效载荷包括一个弱信号GNSS接收器、一个高增益l波段贴片天线、一个低噪声放大器和一个射频滤波器。接收机将跟踪GPS L1 C/A和L5,以及伽利略E1和E5a信号,并将伪距、载波相位和多普勒测量结果返回到地面。它还将计算最小二乘点解和基于卡尔曼滤波的机载导航解。此外,接收器具有记录原始I/Q基带样本用于下行链路和接地处理的能力。用于未来的月球门户、机器人和人类着陆器以及探测器。本文提供了LuGRE有效载荷的详细概述,包括其设计、操作概念以及满足其核心科学目标的预测能力。概述了基线科学调查和优先事项。给出了基于最新标定模型的仿真性能结果,包括信号强度、信号可用性、机载导航性能和收敛性能以及地基后处理导航性能。
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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