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Spaceborne synthetic aperture radar polarized system parameter design method

A technology of synthetic aperture radar and polarization system, which is applied in the field of electronic information and can solve problems such as image pollution

Active Publication Date: 2018-08-14
昆山亿趣信息技术研究院有限公司
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0003] Although the polarization technology has obvious advantages, the images acquired by the polarization radar system will inevitably be polluted by the disturbance parameters of the system

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  • Spaceborne synthetic aperture radar polarized system parameter design method
  • Spaceborne synthetic aperture radar polarized system parameter design method
  • Spaceborne synthetic aperture radar polarized system parameter design method

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Embodiment Construction

[0050] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0051] The polarization system parameter design method of the spaceborne synthetic aperture radar proposed by the present invention establishes a correlation model between the evaluation index of the specific terminal application and the polarization system parameter from the perspective of the synthetic aperture radar system designer. The correlation model includes theoretical model formulas and numerical transfer relations. Based on the correlation model, the parameter design requirements of the polarization system for the corresponding terminal applications can be put forward. The present invention will be described in detail below in conjunction with specific embodiments.

[0052] For the application of polarization target decomposition, the present invention establishes polarization crosstalk δ 1 The theoretical formu...

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Abstract

The invention belongs to the technical field of electronic information and specifically refers to a spaceborne synthetic aperture radar polarized system parameter design method. The invention puts forward the polarized system parameter design method which is aimed at four terminal applications that are respectively polarization object decomposition, land surface classification, military object detection and vegetation height inversion. Polarization system parameters comprise one or more of polarization crosstalk, channel imbalance and system noise. The design method is to establish a correlation model between a terminal application evaluation index and the polarization system parameters. The correlation model includes theoretical model formulas or numerical value transfer relationships. According to the correlation model, polarization system parameter design requirements of corresponding terminal applications can be put forward. The invention provides the polarized system parameter design method for a spaceborne synthetic aperture radar system designer, and that a designed synthetic aperture radar system can provide data service according to application requirements can be ensured.

Description

technical field [0001] The invention belongs to the technical field of electronic information, and specifically relates to a method for designing a polarization system parameter of a spaceborne synthetic aperture radar. Background technique [0002] The images acquired by the full polarization synthetic aperture radar system can reflect the different scattering mechanisms and polarization characteristics of ground objects. Using fully polarized SAR images can be used in many applications, such as polarized target decomposition, surface classification, military target detection, vegetation height inversion, etc. These applications will help people understand changes in the ecological climate environment, resource distribution, and defend territorial security. [0003] Although the polarization technology has obvious advantages, the image acquired by the polarization radar system will inevitably be polluted by the disturbance parameters of the system. The polarization system...

Claims

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Application Information

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IPC IPC(8): G01S7/02
CPCG01S7/02
Inventor 徐丰王潇王海鹏金亚秋
Owner 昆山亿趣信息技术研究院有限公司
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