测量土壤湿度的充气天线微波辐射计

B. M. Kendall, Michael C. Bailey, L. Schroeder
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引用次数: 7

摘要

目前的技术无法以所需的空间地球分辨率获得土壤湿度的微波测量。在弗吉尼亚州汉普顿举行的低地球轨道微波辐射测量研讨会确定了以10公里分辨率测量土壤湿度作为一般科学驱动因素。最近,采用可展开充气天线结构的新型轻量化反射系统被开发出来,从而实现轻量化的实孔径辐射计。考虑到这一点,美国宇航局兰利研究中心进行了一项研究,以确定利用充气反射面天线技术开发微波辐射计系统的可行性,该系统可以在低地球轨道上获得高空间分辨率的土壤湿度辐射测量,并且可以在小型和经济有效的运载火箭上使用。需要的高分辨率和合理的条带宽度以及l波段土壤湿度测量频率决定了使用大型(30米级)真实孔径天线,结合推扫天线波束配置和1.4 GHz和4.3 GHz的噪声注入型辐射计设计,以产生370公里的交叉轨道条带,分辨率为10公里,可以与泰坦II级运载火箭一起包装发射。本研究包括充气式结构设计、控制分析、结构与热分析、天线与馈电设计、辐射计设计、有效载荷包装、轨道分析以及薄膜充气式材料的电磁损耗。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Inflatable antenna microwave radiometer for soil moisture measurement
Microwave measurements of soil moisture are not being obtained at the required spatial Earth resolution with current technology. The Low Earth Orbit Microwave Radiometry Workshop held in Hampton, Virginia, identified measurements of soil moisture at a resolution of 10 km as the general science driver. Recently, new novel designs for lightweight reflector systems have been developed using deployable inflatable antenna structures which could enable lightweight real-aperture radiometers. In consideration of this, a study was conducted at the NASA Langley Research Center to determine the feasibility of developing a microwave radiometer system using inflatable reflector antenna technology to obtain high spatial resolution radiometric measurements of soil moisture from low Earth orbit and which could be used with a small and cost effective launch vehicle. The required high resolution with reasonable swath width coupled with the L-band measurement frequency for soil moisture dictated the use of a large (30 meter class) real aperture antenna in conjunction with a pushbroom antenna beam configuration and noise-injection type radiometer designs at 1.4 and 4.3 GHz to produce a 370 kilometer cross-track swath with a 10 kilometer resolution that could be packaged for launch with a Titan II class vehicle. This study includes design of the inflatable structure, control analysis, structural and thermal analysis, antenna and feed design, radiometer design, payload packaging, orbital analysis, and electromagnetic losses in the thin membrane inflatable materials.<>
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