一种星载扇形波束散射计后向散射系数定标方法

By establishing a lookup table for the relative viewing angle and illumination integration parameters of the resolution unit, the problems of low processing efficiency and low resolution of the backscattering coefficient calibration method of the spaceborne fan beam scatterometer were solved, and efficient and accurate backscattering coefficient calibration was achieved.

CN117826102BActive Publication Date: 2026-07-17XIAN INSTITUE OF SPACE RADIO TECH

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
XIAN INSTITUE OF SPACE RADIO TECH
Filing Date
2023-12-19
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In the existing technology, the backscattering coefficient calibration method of the spaceborne sector beam scatterometer has low processing efficiency and low resolution, and cannot achieve accurate and efficient range-oriented equal-resolution multiple observations.

Method used

By establishing a lookup table for the relative viewing angle and relative position of the resolution unit and the illumination integration parameter of the resolution unit before data processing, and by using satellite ephemeris data and antenna parameters for data processing, the cumulative range of the power slice of the resolution unit and the corresponding beam center viewing angle are determined, and then converted into backscattering coefficients by combining the calibration parameters within the system.

Benefits of technology

This improved the efficiency and reliability of data processing, ensured that the backscattering coefficients of each resolution unit had the same resolution, adapted to changes in satellite orbital parameters, and achieved efficient backscattering coefficient calibration.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN117826102B_ABST
    Figure CN117826102B_ABST
Patent Text Reader

Abstract

一种星载扇形波束散射计后向散射系数定标方法,属于空间微波遥感技术领域。本发明包括:在星载扇形波束散射计数据处理前,建立分辨单元相对视角和切片相对位置查找表,建立分辨单元照射积分参数查找表。在地面数据处理阶段,根据每个时刻场景观测数据,基于观测几何查找表确定距离向分辨单元功率切片累积范围和对应波束中心视角,基于照射积分查找表确定各分辨单元对应照射积分参数。结合系统定标参数和在轨定标观测数据,根据雷达方程计算出各分辨单元后向散射系数,实现后向散射系数定标和定位。本发明通过克服现有处理方法的局限性,能够准确、可靠和高效地实现扇形波束散射计距离向不同分辨单元后向散射系数定标和定位。
Need to check novelty before this filing date? Find Prior Art