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Precise Computation of Doppler Parameters for Spaceborne SAR in Elliptic Orbits

机译:椭圆轨道星载SAR多普勒参数的精确计算

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摘要

There are errors in the existing formulae for calculating the Doppler parameters for spaceborne SAR. Too large errors would adversely affect the convergence speed of the estimation algorithms for Doppler parameters. This paper derives several precise analytical formulae based on the results presented in the published literature. During the deduction process, the effect of flight-path angle is considered as a key issue. To the author’s knowledge, the effect was neglected in all of the relevant published literature. The consequence is that the existing formulae can only be approximately used in a nearly circular orbit. If the existing formulae are applied to a satellite with large eccentricity, the error may be too large. In contrast, the formulae derived in this paper can be used in any cases, for there are no errors in our formulae. The accuracy of the derived formulae and the effect of the flight-path angle are verified by a simulation experiment using the parameters of Radarsat.
机译:在计算星载SAR多普勒参数的现有公式中存在错误。太大的误差会不利地影响多普勒参数估计算法的收敛速度。本文根据已发表文献中提供的结果推导了几种精确的分析公式。在推导过程中,飞行路径角的影响被认为是关键问题。据作者所知,在所有相关的已出版文献中都忽略了这种影响。结果是现有公式只能近似地用于近乎圆形的轨道。如果将现有公式应用于具有较大偏心率的卫星,则误差可能会太大。相反,本文中得出的公式可在任何情况下使用,因为我们的公式没有错误。通过使用Radarsat的参数进行的模拟实验,验证了推导公式的准确性和飞行路径角的影响。

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  • 会议地点 Huangshan(CN)
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    Peng Zhou@School of Electronic Engineering,University of Electronic Science and Technology of China Chengdu,Sichuan 610054,P.R.China;

    School of Information and Control Engineering,China University of Petroleum Dongying,Shandong 257061,P.R.China--Yiming Pi@School of Electronic Engineering,University of Electronic Science and Technology of China Chengdu,Sichuan 610054,P.R.China--Jinfeng Wang@School of Electronic Engineering,University of Electronic Science and Technology of China Chengdu,Sichuan 610054,P.R.China--;

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