Field Testing of Lunar Access and Navigation Device (LAND)

C. Liebe, J. Alexander, M. Aung, H. Goldberg, A. Johnson, R. Lam, E. Maize, P. Meras, J. Montgomery, Pilar Tejada Palacios, G. Spiers, M. Wilson
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引用次数: 2

Abstract

A laser radar system has been constructed. It is based on a commercial PC with digitizer, pulse delay instrument, National Instruments IO card and an optical head from a previous laser radar program. The laser radar was mounted on a gyro stabilized gimbal on the nose of a helicopter and flown in the Mojave Desert in September 2006. The collected data will be used to test algorithms for future precision lunar landers, which may be utilizing a laser radar as the primary landing sensor. This paper will describe the laser radar and PC based acquisition system used for the data collection, and provide an overview of the supporting test sensors and architecture. Preliminary data collected during the helicopter field testing will also be presented.
月球进入和导航装置(陆地)现场测试
建立了激光雷达系统。它基于商用PC机,带有数字化仪、脉冲延迟仪、美国国家仪器公司的IO卡和以前激光雷达项目的光学头。激光雷达安装在直升机机头的陀螺稳定万向架上,并于2006年9月在莫哈韦沙漠飞行。收集的数据将用于测试未来精密月球着陆器的算法,该着陆器可能使用激光雷达作为主要着陆传感器。本文将介绍用于数据采集的激光雷达和基于PC机的采集系统,并概述配套的测试传感器和体系结构。在直升机现场测试期间收集的初步数据也将被展示。
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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