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A novel system parameters design and performance analysis method for Distributed Satellite-borne SAR system

机译:分布式星载SAR系统系统参数设计与性能分析的新方法

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摘要

As a promising new technology emerged in recent years, the Distributed Satellite-borne SAR (DSS) system with Interferometric Synthetic Aperture Radar (InSAR) imaging capability has been recognized by the remote sensing community as an integrated part of the spaceborne earth observation system. However, most researches on DSS were focused on individual aspects of system design/analysis and data processing, while few studies have been dedicated to establishing a standard methodological framework for universal DSS system design. Aiming at this problem, the topics of DSS system error analysis and design method are investigated in this paper. Firstly, a rigorous error propagation model of height measurement is theoretically derived from the DSS InSAR imaging geometry, and the impact of each error sources in this model on the height measurement accuracy is analyzed individually. In particular, the baseline length and its measurement error in the InSAR imaging plane are identified as the dominant factors. Second, a new method for DSS system design is proposed based on our analyses with the error propagation model. This method consists of two important phases, namely collaboration design and monostatic design. The major objective of collaboration design is to determine the configuration and parameters for the coordination between satellites in the DSS system. Afterwards, the key parameters for single satellite and the payload are determined by the monostatic design. Thirdly, a system performance analysis method is developed to comprehensively evaluate the performance of the predesigned DSS system. In the next section, a typical example of DSS system design is given to demonstrate the effectiveness of the proposed system design and analysis methods. The target DSS system has the same goal and hardware configuration as the TanDEM-X mission. Finally, the conclusion is drawn with our major findings are presented.
机译:作为近年来出现的有希望的新技术,具有干涉合成孔径雷达(InSAR)成像功能的分布式星载SAR(DSS)系统已被遥感界认可为星载地球观测系统的组成部分。但是,关于DSS的大多数研究都集中在系统设计/分析和数据处理的各个方面,而很少有研究致力于建立通用DSS系统设计的标准方法框架。针对这一问题,本文对DSS系统错误分析和设计方法进行了研究。首先,从DSS InSAR成像几何学理论上推导了严格的高度测量误差传播模型,并分别分析了该模型中每个误差源对高度测量精度的影响。特别是,将InSAR成像平面中的基线长度及其测量误差确定为主要因素。其次,基于对误差传播模型的分析,提出了一种新的DSS系统设计方法。该方法包括两个重要阶段,即协作设计和单静态设计。协作设计的主要目标是确定DSS系统中卫星之间协调的配置和参数。然后,单卫星的关键参数和有效载荷由单基地设计确定。第三,开发了一种系统性能分析方法,以全面评估预先设计的DSS系统的性能。在下一部分中,将给出一个DSS系统设计的典型示例,以证明所提出的系统设计和分析方法的有效性。目标DSS系统的目标和硬件配置与TanDEM-X任务相同。最后,得出结论,并提出我们的主要发现。

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