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Ultra low range sidelobe level pulse compression waveform design for spaceborne meteorological radars.

机译:适用于星载气象雷达的超低频旁瓣电平脉冲压缩波形设计。

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摘要

Meteorological measurements from spaceborne radars present several advantages over current passive techniques, due to the radar capability to discriminate backscattered energy in range. However, the system configuration imposes stringent design requirements in order to guarantee cloud and rain detectability, in particular on the radar waveform. Since power is severely restricted on board a satellite, it is necessary to achieve an efficient range resolution with low transmitted power requirements. Pulse compression theory solves the previous conflicting demand, but the transmitted signal needs to be carefully designed in order to allow the significantly large dynamic range (between 60 and 80 dB depending on the type of meteorological target) needed to carry out the measurements. Several pulse compression range sidelobe reduction techniques of differing natures have been investigated and reported in the literature during the past 50 years. A detailed survey of the most relevant range sidelobe supression procedures has been carried out in order to identify the most suitable frequency modulation candidates which are potentially capable of meeting the stringent specifications of spaceborne radar meteorology. Novel pulse compression waveform design techniques have also been developed, employing linear FM predistortion functions and asymmetric frequency modulation laws, which provide excellent performance in terms of range sidelobe level (below -60 dB) and Doppler tolerance. Different options for the provision of a rain mode for the RA-2 Radar Altimeter (due to fly on European Space Agency ENVISAT satellite) are described, based on altimetry linear FM full-deramp technique concepts. Finally, amplitude modulated pulse compression waveform design alternatives are analysed for the MACSIM radar (Millimetre wave Active Cloud Structure Imaging Mission, European Space Agency Pre Phase A Study), which allow to measure different type of clouds within the Mission required radiometric resolution accuracy.
机译:由于雷达能够分辨范围内的反向散射能量,因此星载雷达的气象测量结果比当前的无源技术具有多个优势。但是,系统配置提出了严格的设计要求,以确保尤其是雷达波形上的云雾和雨水可检测性。由于卫星上的功率受到严格限制,因此有必要在低发射功率的情况下实现有效的距离分辨率。脉冲压缩理论解决了先前的矛盾需求,但是需要仔细设计传输信号,以允许执行测量所需的很大的动态范围(取决于气象目标的类型,介于60至80 dB之间)。在过去的50年中,已经研究并报道了几种不同性质的脉冲压缩范围旁瓣减小技术。为了确定最有可能满足星载雷达气象学的严格规范的最合适的频率调制候选者,已经对最相关的范围旁瓣抑制程序进行了详细调查。还开发了新颖的脉冲压缩波形设计技术,采用线性FM预失真功能和非对称频率调制定律,在范围旁瓣电平(低于-60 dB)和多普勒容差方面提供了出色的性能。基于测高仪线性调频全阻尼技术概念,描述了为RA-2雷达高度计提供降雨模式的不同选择(由于在欧洲航天局ENVISAT卫星上飞行)。最后,对MACSIM雷达(毫米波主动云结构成像任务,欧洲航天局A期研究)的振幅调制脉冲压缩波形设计替代方案进行了分析,该方案可以在任务所需的辐射分辨率精度内测量不同类型的云。

著录项

  • 作者

    i Solans, Lluis Vinagre.;

  • 作者单位

    University of London, University College London (United Kingdom).;

  • 授予单位 University of London, University College London (United Kingdom).;
  • 学科 Meteorology.
  • 学位 Ph.D.
  • 年度 1997
  • 页码 207 p.
  • 总页数 207
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:48:55

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