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A process for the processing of tops (terrain observation by progressive scan) - sar (synthetic aperture radar) - raw data and the use of the method

机译:处理顶部(通过逐行扫描进行地形观察)的过程-sar(合成孔径雷达)-原始数据和方法的使用

摘要

It is carried out a sub-aperture - processing. Within each subaperture, a range compression and a correction of the target range variation is carried out. For the processing of the azimuth signal, a baseband - azimuth - scaling is used, with a long azimuth reference function, and thus a large azimuth dimension be prevented. The scaling - removal is not constant and depends on the distance, which is not equal to the original distance vector. It is calculated in such a way that in combination with a later derotation step, a constant azimuth scanning is achieved for all distances. The selected derotation function, which in the azimuth time range is applied, makes it possible for all the objects are located in the baseband, whereby in this manner the effective chirp - rate is changed. Since the phase as a result of the azimuth scaling - steps -2tes purely is square, therefore, an optimal filter can be used, the chirp - rate is taken into account the effective. An ifft results in a focused image and a final phase function in the time domain makes possible a phase conservation.Use in the sar -, sonar - and seismic raw data, they ethyl 1-cyclopropyl-7-fluoro-8-trifluoromethyl-1,4-dihydro-4-oxo-3-quinolinecarboxylate in the top - mode, as well as other modes, the pivoting of the antenna diagram in the azimuth - and / or the elevation direction use.
机译:进行子光圈-处理。在每个子孔径内,进行范围压缩和目标范围变化的校正。对于方位信号的处理,使用具有长方位参考功能的基带-方位-缩放,因此防止了较大的方位尺寸。缩放比例-移除不是恒定的,并且取决于距离,该距离不等于原始距离向量。以这样的方式进行计算:与随后的旋转步骤相结合,可以在所有距离上实现恒定的方位角扫描。在方位角时间范围内应用选定的防旋转功能,使所有物体都位于基带中,从而以这种方式改变了有效线性调频率。由于方位角缩放的结果-步幅-2tes纯粹是正方形,因此,可以使用最佳滤波器,因此线性调频率被考虑在内。 ifft产生聚焦的图像,并且在时域中的最终相位函数使相位守恒成为可能。在sar,声纳和地震原始数据中,它们使用的是乙基1-环丙基-7-氟-8-三氟甲基-1在顶部模式以及其他模式中,天线图在方位角上的枢轴旋转和/或仰角方向使用。

著录项

  • 公开/公告号DE102007031020B3

    专利类型

  • 公开/公告日2008-12-24

    原文格式PDF

  • 申请/专利权人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V.;

    申请/专利号DE20071031020

  • 发明设计人

    申请日2007-07-04

  • 分类号G01S13/90;G01S15/89;

  • 国家 DE

  • 入库时间 2022-08-21 19:09:44

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