首页> 外文会议>OCEANS '79 >Preliminary Results of the NASA/Goddard Space Flight Center Short Pulse Radar Ocean Waves Sensing Program
【24h】

Preliminary Results of the NASA/Goddard Space Flight Center Short Pulse Radar Ocean Waves Sensing Program

机译:NASA / Goddard太空飞行中心短脉冲雷达海浪传感计划的初步结果

获取原文
获取外文期刊封面目录资料

摘要

The Goddard Space Flight Center 13.9 GHz 12 ns pulse compression radar was flown on extended NASA CV-990 aircraft missions in 1977 and 1978 for the primary purpose of advancing a simple microwave radar technique for measuring ocean wave directional spectra from aircraft and satellite platforms, and secondarily for advancing in general the state-of-knowledge of microwave interaction with sea and ice surfaces. The radar is a versatile, rather complex, instrument having basically three functional modes that are associated with three different antenna systems. These modes are: a. Altimeter (ALT. A12deg times 12degnadir-pointing horn antenna is used for significant wave height measurements to within the 1.5 m resolution capability of the radar. This well-known technique makes use of the time-stretch of the leading edge of the average pulse return in the presence of waves. b. Real Aperture Imaging Radar (SLAR). A1/2deg times 40degslotted waveguide antenna mounted on the aircraft instrument sled is used for wave imagery at low altitude (<10 k ft.). c. Directional Wave Spectrometer (DWS). In the Fall 1978 mission, a 6 rpm rotating printed circuit (PC) antenna, boresighted at a16degnadir angle and having a10degelevation and4degazimuth beamwidth, was used in the DWS mode. (In the 1977 mission an adjustable elevation angle PC antenna fixed at broadside azimuth was used to study incidence angle dependence.) The DWS concept, briefly, makes use of the azimuthal averaging of ocean wave contrast features to isolate Fourier contrast wave components traveling in the radar look direction. Spectral analysis of the return for the contrast wave modulation over360degazimuth angle yields a directional contrast spectrum that is in a first approximation proportional to the directional spectrum of total wave slope variance. Modulation signal-to-Rayleigh clutter noise ratios are improved by Doppler time domain filt--ering prior to the spectral analysis. A preliminary analysis of the digital data from flights in the Northeastern Pacific over several environmental buoys and ocean weather ship PAPA, and from a flight in the Norwegian Sea over an instrumented weather ship during storm conditions is presented. The directional modulation spectrum is related to the directional wave height spectrum through a physical scattering model: essential similarity with the directional slope spectrum is shown. The short pulse DWS and its sister dual-frequency DWS concepts are discussed with reference to future satellite DWS instrument design.
机译:戈达德太空飞行中心13.9 GHz 12 ns脉冲压缩雷达于1977年和1978年在NASA CV-990飞机上执行了扩展飞行任务,其主要目的是推进一种简单的微波雷达技术来测量飞机和卫星平台的海浪方向光​​谱,并且其次,通常是为了提高微波与海冰表面相互作用的知识水平。雷达是一种多功能的,相当复杂的仪器,基本上具有与三种不同的天线系统相关联的三种功能模式。这些模式是:高度计(ALT。Atex= 12deg乘以12deg天底指向的号角天线)用于在雷达分辨率为1.5 m的范围内进行有效的波高测量。这项众所周知的技术利用了时间拉伸b。实孔成像雷达(SLAR):安装在飞机仪器底座上的Atex / 1 / 2deg乘以40deg /缝隙波导天线用于低高度(<10 k ft。)处的波图像c。定向波谱仪(DWS)在1978年秋季的任务中,以6 rpm旋转印刷电路(PC)天线在 16deg 处瞄准了视线在DWS模式下,使用了最低底角且仰角为10 tex且仰角为4 tex的波束宽度(在1977年的任务中,使用了固定在宽边方位上的可调仰角PC天线来研究入射角的相关性。)DWS概念简要地利用了海浪对比度特征的方位平均来隔离Fou。沿雷达视线方向传播的rier对比波分量。对在360°方位角上的对比波调制返回的光谱进行频谱分析,得出了一个方向对比光谱,该方向对比光谱与总波斜率方差的方向光谱成第一近似关系。多普勒时域滤波提高了调制信号与瑞利杂波的噪声比, -- 在进行光谱分析之前初步分析了来自东北太平洋在多个环境浮标和海洋气象船PAPA上的飞行以及在暴风条件下在仪表船上在挪威海的飞行中的数字数据。通过物理散射模型,定向调制谱与定向波高谱相关:显示了与定向斜率谱的基本相似性。参照未来的卫星DWS仪器设计,讨论了短脉冲DWS及其姊妹双频DWS概念。

著录项

  • 来源
    《OCEANS '79》|1979年|p.365|共1页
  • 会议地点
  • 作者

  • 作者单位
  • 会议组织
  • 原文格式 PDF
  • 正文语种
  • 中图分类 海洋学;
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号