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Lidar to Weather Balloon Profile Comparison for Support of Orion Crew Exploration Vehicle Landings

机译:激光雷达到气象气球轮廓的比较,以支持猎户座乘员探索飞行器着陆

摘要

A comparison study by the National Aeronautics and Space Administration Dryden FlightResearch Center, Edwards, CA and the Naval Post Graduate School Center for InterdisciplinaryRemotely-Piloted Aircraft Studies, Marina, CA was conducted to show the advantages of anairborne wind profiling lidar system in reducing drift uncertainty along a reentry vehicle descenttrajectory. This effort was in support of the once planned Orion Crew Exploration Vehicleground landing. A Twin Otter Doppler Wind Lidar was flown on multiple flights along theapproximate ground track of an ascending weather balloons launched from the Marina MunicipalAirport. The airborne lidar used was a 5-milli-Joules, 2-micron infrared laser with a 10-centimeter telescope and a two-axis scanner. Each lidar wind profile contains data for an altituderange between the surface and flight altitude of 2,700 meters, processed on board every 20seconds.
机译:美国加利福尼亚州爱德华兹州国家航空和航天局Dryden飞行研究中心与美国加利福尼亚州马里纳海军研究生研究生院跨学科飞机研究中心进行了比较研究,以显示机载风廓线激光雷达系统在减少漂移不确定性方面的优势沿着再入车辆下降轨迹。这项工作是为了支持曾经计划好的猎户座乘员探索车着陆。双水獭多普勒风激光雷达沿着滨海市政机场升起的气象气球的近似地面轨道飞行了多次。所使用的机载激光雷达是5毫焦耳,2微米的红外激光,带有10厘米望远镜和两轴扫描仪。每个激光雷达风廓线都包含每20秒在飞机上处理的2700米表面和飞行高度之间的高度范围的数据。

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