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CN116736306A - Time sequence radar interference monitoring method based on third high-resolution - Google Patents

Time sequence radar interference monitoring method based on third high-resolution Download PDF

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CN116736306A
CN116736306A CN202311023457.XA CN202311023457A CN116736306A CN 116736306 A CN116736306 A CN 116736306A CN 202311023457 A CN202311023457 A CN 202311023457A CN 116736306 A CN116736306 A CN 116736306A
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target area
interference
phase
phase diagram
interference phase
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CN116736306B (en
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韩亚坤
戴可人
史先琳
温柠玲
刘晨
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Chengdu Univeristy of Technology
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/89Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • G01S13/90Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. synthetic aperture radar [SAR] techniques
    • G01S13/9021SAR image post-processing techniques
    • G01S13/9023SAR image post-processing techniques combined with interferometric techniques
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B15/00Measuring arrangements characterised by the use of electromagnetic waves or particle radiation, e.g. by the use of microwaves, X-rays, gamma rays or electrons
    • G01B15/06Measuring arrangements characterised by the use of electromagnetic waves or particle radiation, e.g. by the use of microwaves, X-rays, gamma rays or electrons for measuring the deformation in a solid
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
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  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

The invention discloses a time sequence radar interference monitoring method based on a third high-resolution method, which relates to the field of radar interference monitoring, and comprises the following steps: obtaining an interference phase diagram of the target area by using a third high-resolution method; obtaining a winding interference phase diagram of the target area according to the interference phase diagram of the target area and the digital elevation model data; obtaining a winding interference phase diagram of a target area with dense stripes removed; according to polynomial fitting, a linear regression model and a winding interference phase diagram of the target area for removing dense stripes, obtaining a winding interference phase diagram of the target area after correction; and acquiring a time sequence deformation rate chart of the high-resolution third image of the target area by adopting a time sequence radar interferometry method according to the winding interference phase chart corrected by the target area so as to realize the monitoring of the target area. The method can improve the quality of the third interference phase diagram by correcting the track error and the baseline error, thereby realizing high-precision monitoring of the surface deformation of the target area.

Description

一种基于高分三号的时序雷达干涉监测方法A time-series radar interference monitoring method based on Gaofen-3

技术领域Technical field

本发明涉及雷达干涉监测领域,具体涉及一种基于高分三号的时序雷达干涉监测方法。The invention relates to the field of radar interference monitoring, and specifically relates to a time-series radar interference monitoring method based on Gaofen-3.

背景技术Background technique

高分三号是我国首颗C波段、多极化、高分辨率(最高达到1米)的合成孔径雷达卫星,具有全天时全天候监测、高精度测量、多模式成像等突出优势,可以全天候和全天时实现全球海洋和陆地信息的监测。高分三号在自然灾害领域被应用于冰川运动、地面沉降、地震、滑坡、泥石流、洪涝等灾害的监测。Gaofen-3 is my country's first C-band, multi-polarization, high-resolution (up to 1 meter) synthetic aperture radar satellite. It has outstanding advantages such as all-day and all-weather monitoring, high-precision measurement, and multi-mode imaging, and can operate all day and night. And realize the monitoring of global ocean and land information around the clock. Gaofen-3 is used in the field of natural disasters to monitor glacier movements, land subsidence, earthquakes, landslides, debris flows, floods and other disasters.

现目前高分三号在雷达干涉监测领域,因存在轨道误差和基线误差,导致获取的高分三号影像干涉相位图的质量并不高,进而无法充分利用其进行目标区域的时序形变监测。Currently, in the field of radar interference monitoring, the quality of the Gaofen-3 image interference phase diagram obtained due to orbit errors and baseline errors is not high, making it impossible to fully utilize it for time-series deformation monitoring of the target area.

发明内容Contents of the invention

针对现有技术中的上述不足,本发明提供了一种基于高分三号的时序雷达干涉监测方法,能通过修正轨道误差和基线误差以提升高分三号干涉相位图质量,进而实现对目标区域地表形变的高精度监测。In view of the above-mentioned deficiencies in the existing technology, the present invention provides a time-series radar interference monitoring method based on Gaofen-3, which can improve the quality of Gaofen-3 interference phase diagram by correcting the orbit error and baseline error, thereby achieving target detection. High-precision monitoring of regional surface deformation.

为了达到上述发明目的,本发明采用的技术方案为:In order to achieve the above-mentioned object of the invention, the technical solutions adopted by the present invention are:

一种基于高分三号的时序雷达干涉监测方法,包括以下步骤:A time-series radar interference monitoring method based on Gaofen-3, including the following steps:

S1、利用高分三号获取目标区域的干涉相位图;S1. Use Gaofen-3 to obtain the interference phase map of the target area;

S2、根据步骤S1中目标区域的干涉相位图和数字高程模型数据获取目标区域的缠绕干涉相位图;S2. Obtain the winding interference phase diagram of the target area according to the interference phase diagram of the target area and the digital elevation model data in step S1;

S3、根据星历数据和步骤S2中目标区域的缠绕干涉相位图,获取目标区域去除密集条纹的缠绕干涉相位图;S3. According to the ephemeris data and the winding interference phase map of the target area in step S2, obtain the winding interference phase map of the target area with dense fringes removed;

S4、根据多项式拟合、线性回归模型和步骤S3中目标区域去除密集条纹的缠绕干涉相位图,获取目标区域修正后的缠绕干涉相位图;S4. According to the polynomial fitting, linear regression model and the winding interference phase image of the target area with dense stripes removed in step S3, obtain the corrected winding interference phase image of the target area;

S5、根据步骤S4中目标区域修正后的缠绕干涉相位图,采用时序雷达干涉测量方法获取目标区域的高分三号影像的时序形变速率图,以实现目标区域的监测。S5. According to the corrected winding interference phase diagram of the target area in step S4, use the time-series radar interferometry method to obtain the time-series deformation rate map of the Gaofen-3 image of the target area to achieve monitoring of the target area.

进一步地,步骤S2包括以下分步骤:Further, step S2 includes the following sub-steps:

S21、对步骤S1中目标区域的干涉影像进行配准和干涉组合,生成目标区域的单视缠绕干涉相位图;S21. Perform registration and interference combination on the interference images of the target area in step S1 to generate a single-view winding interference phase map of the target area;

S22、根据数字高程模型数据对分步骤S21中目标区域的单视缠绕干涉相位图进行去平地和地形改正,获取目标区域的缠绕干涉相位图。S22. Perform flattening and terrain correction on the single-view winding interference phase map of the target area in step S21 according to the digital elevation model data to obtain the winding interference phase map of the target area.

进一步地,步骤S3包括以下分步骤:Further, step S3 includes the following sub-steps:

S31、根据星历数据,利用轨道状态矢量估计获取目标区域的缠绕干涉相位图的第一初始基线;S31. According to the ephemeris data, use orbital state vector estimation to obtain the first initial baseline of the winding interference phase diagram of the target area;

S32、获取干涉条纹频率数据,并根据干涉条纹频率数据获取目标区域的缠绕干涉相位图的第二初始基线;S32. Obtain the interference fringe frequency data, and obtain the second initial baseline of the winding interference phase diagram of the target area based on the interference fringe frequency data;

S33、根据分步骤S31中的第一初始基线和分步骤S32中的第二初始基线,获取目标区域去除密集条纹的缠绕干涉相位图。S33. According to the first initial baseline in step S31 and the second initial baseline in step S32, obtain the winding interference phase map of the target area with dense fringes removed.

进一步地,步骤S31包括以下分步骤:Further, step S31 includes the following sub-steps:

S311、根据星历数据,拟合卫星的时间位置曲线;S311. Fit the time position curve of the satellite according to the ephemeris data;

S312、根据最小二乘法计算分步骤S311中卫星的时间位置曲线的未知参数,获取卫星的轨道曲线模型;S312. Calculate the unknown parameters of the time position curve of the satellite in step S311 according to the least squares method, and obtain the orbit curve model of the satellite;

S313、根据分步骤S312中卫星的轨道曲线模型,获取目标区域的缠绕干涉相位图的第一初始基线。S313. According to the orbit curve model of the satellite in step S312, obtain the first initial baseline of the winding interference phase diagram of the target area.

进一步地,在分步骤S311中,拟合卫星的时间位置曲线,表示为:Further, in sub-step S311, the time position curve of the satellite is fitted, which is expressed as:

其中:为天线中心的/>轴坐标值,/>为天线中心的/>轴的常数项系数,/>为天线中心的/>轴的一次项系数,/>为采样点时间,/>为天线中心的/>轴的二次项系数,/>为天线中心的/>轴的三次项系数,/>为天线中心的/>轴坐标值,/>为天线中心的/>轴的常数项系数,/>为天线中心的/>轴的一次项系数,/>为天线中心的/>轴的二次项系数,/>为天线中心的/>轴的三次项系数,/>为天线中心的/>轴坐标值,/>为天线中心的/>轴的常数项系数,/>为天线中心的/>轴的一次项系数,/>为天线中心的/>轴的二次项系数,/>为天线中心的/>轴的三次项系数。in: is the center of the antenna/> Axis coordinate value,/> is the center of the antenna/> The constant term coefficient of the axis,/> is the center of the antenna/> The linear term coefficient of the axis,/> is the sampling point time,/> is the center of the antenna/> The coefficient of the quadratic term of the axis,/> is the center of the antenna/> Coefficient of cubic term of axis,/> is the center of the antenna/> Axis coordinate value,/> is the center of the antenna/> The constant term coefficient of the axis,/> is the center of the antenna/> The linear term coefficient of the axis,/> is the center of the antenna/> The coefficient of the quadratic term of the axis,/> is the center of the antenna/> Coefficient of cubic term of axis,/> is the center of the antenna/> Axis coordinate value,/> is the center of the antenna/> The constant term coefficient of the axis,/> is the center of the antenna/> The linear term coefficient of the axis,/> is the center of the antenna/> The coefficient of the quadratic term of the axis,/> is the center of the antenna/> Coefficient of the cubic term of the axis.

进一步地,步骤S4包括以下分步骤:Further, step S4 includes the following sub-steps:

S41、对步骤S3中目标区域去除密集条纹的缠绕干涉相位图进行相位解缠,获取目标区域的解缠干涉相位图;S41. Perform phase unwrapping on the entangled interference phase image of the target area with dense fringes removed in step S3, and obtain the unwrapped interference phase image of the target area;

S42、根据多项式拟合分步骤S41中目标区域的解缠干涉相位图的相位跳变,获取轨道误差的残余相位;S42. Obtain the residual phase of the orbit error according to the phase jump of the unwrapped interference phase diagram of the target area in step S41 of polynomial fitting;

S43、根据分步骤S41中目标区域的解缠干涉相位图,利用线性回归模型获取大气误差;S43. Based on the unwrapped interference phase map of the target area in step S41, use the linear regression model to obtain the atmospheric error;

S44、根据多项式拟合分步骤S42中轨道误差的残余相位和分步骤S43中的大气误差,获取拟合结果;S44. Obtain the fitting result according to the residual phase of the orbit error in step S42 of polynomial fitting and the atmospheric error in step S43;

S45、根据分步骤S44中的拟合结果修正步骤S3中去除密集条纹的缠绕干涉相位图,获取目标区域修正后的缠绕干涉相位图。S45. Correct the winding interference phase image from which the dense fringes are removed in step S3 according to the fitting result in step S44, and obtain the corrected winding interference phase image of the target area.

进一步地,在分步骤S42中,拟合分步骤S41中目标区域的解缠干涉相位图的相位跳变,获取轨道误差的残余相位,表示为:Further, in sub-step S42, the phase jump of the unwrapped interference phase diagram of the target area in sub-step S41 is fitted to obtain the residual phase of the orbit error, which is expressed as:

其中:为解缠干涉相位图中轨道误差的残余相位,/>为雷达坐标系下的/>轴坐标,/>为雷达坐标系下的/>轴坐标,/>为残余相位的第一系数,/>为残余相位的第二系数,/>为残余相位的第三系数,/>为残余相位的第四系数,/>为残余相位的第五系数,/>为残余相位的第六系数。in: is the residual phase of the orbit error in the unwrapped interference phase diagram,/> is/> in the radar coordinate system Axis coordinates,/> is/> in the radar coordinate system Axis coordinates,/> is the first coefficient of the residual phase,/> is the second coefficient of the residual phase,/> is the third coefficient of the residual phase,/> is the fourth coefficient of the residual phase,/> is the fifth coefficient of the residual phase,/> is the sixth coefficient of the residual phase.

进一步地,在分步骤S43中,利用线性回归模型获取大气误差,表示为:Further, in step S43, the linear regression model is used to obtain the atmospheric error, which is expressed as:

其中:为解缠干涉相位图中的大气误差,/>为雷达坐标系下的/>轴坐标,为雷达坐标系下的/>轴坐标,/>为大气误差的第一系数,/>为大气误差的第二系数,为解缠干涉相位图中的高程信息。in: To unwrap the atmospheric errors in the interference phase diagram,/> is/> in the radar coordinate system axis coordinates, is/> in the radar coordinate system Axis coordinates,/> is the first coefficient of atmospheric error,/> is the second coefficient of atmospheric error, To unwrap the elevation information in the interference phase image.

进一步地,步骤S5包括以下分步骤:Further, step S5 includes the following sub-steps:

S51、根据振幅差离差指数和步骤S4中目标区域修正后的缠绕干涉相位图,选取滤波相位失相干缓慢目标点的候选点;S51. Select candidate points for filtered phase decoherence slow target points based on the amplitude difference dispersion index and the corrected winding interference phase diagram of the target area in step S4;

S52、根据分步骤S51中滤波相位失相干缓慢目标点的候选点,确定相位误差;S52. Determine the phase error according to the candidate points of the filtered phase decoherence slow target point in step S51;

S53、根据分步骤S52中的相位误差确定像素噪声水平的测度参数;S53. Determine the measurement parameters of the pixel noise level according to the phase error in step S52;

S54、根据分步骤S53中像素噪声水平的测度参数和分步骤S51中滤波相位失相干缓慢目标点的候选点,选取滤波相位失相干缓慢目标点;S54. Select the filtered phase decoherent slow target point according to the measurement parameters of the pixel noise level in step S53 and the candidate points of the filtered phase decoherent slow target point in step S51;

S55、根据分步骤S54中的滤波相位失相干缓慢目标点、3D解缠方法和步骤S4中目标区域修正后的解缠干涉相位图,获取目标区域的高分三号影像的时序形变速率图,以实现目标区域的监测。S55. According to the filtered phase decoherence slow target point in step S54, the 3D unwrapping method and the corrected unwrapped interference phase diagram of the target area in step S4, obtain the time series deformation rate diagram of the Gaofen-3 image of the target area, To achieve monitoring of target areas.

本发明具有以下有益效果:The invention has the following beneficial effects:

(1)本发明通过修正轨道误差和基线误差以提升高分三号干涉相位图质量,进而实现对目标区域地表形变的高精度监测;(1) This invention improves the quality of the Gaofen-3 interference phase map by correcting the orbit error and baseline error, thereby achieving high-precision monitoring of surface deformation in the target area;

(2)本发明通过利用轨道状态矢量估计和干涉条纹频率数据得到目标区域的缠绕干涉相位图的第一初始基线和第二初始基线,能对基线误差和轨道误差进行初步的修正,获取目标区域去除密集条纹的缠绕干涉相位图;(2) The present invention obtains the first initial baseline and the second initial baseline of the winding interference phase diagram of the target area by using orbit state vector estimation and interference fringe frequency data. It can make preliminary corrections to the baseline error and orbit error and obtain the target area. Winding interference phase images with dense fringe removal;

(3)本发明通过对初步修正后的干涉相位图进行相位解缠,并利用多项式拟合轨道误差的残余相位和大气误差,能对初步修正后的干涉相位图进行进一步的精细化修正,获取目标区域修正后的缠绕干涉相位图;(3) By phase unwrapping the preliminary corrected interference phase diagram and using polynomials to fit the residual phase of the orbit error and the atmospheric error, the present invention can further refine the preliminary corrected interference phase diagram and obtain Corrected winding interference phase diagram of the target area;

(4)本发明通过采用时序雷达干涉测量方法,能对获取目标区域修正后的缠绕干涉相位图进行相位改正和大气改正,获取目标区域的高分三号影像的时序形变速率图,以实现对目标区域的有效监测。(4) By using the time-series radar interferometry method, the present invention can perform phase correction and atmospheric correction on the corrected winding interference phase diagram of the target area, and obtain the time-series deformation rate diagram of the Gaofen-3 image of the target area, so as to achieve Effective monitoring of target areas.

附图说明Description of drawings

图1为一种基于高分三号的时序雷达干涉监测方法流程示意图。Figure 1 is a schematic flow chart of a time-series radar interference monitoring method based on Gaofen-3.

具体实施方式Detailed ways

下面对本发明的具体实施方式进行描述,以便于本技术领域的技术人员理解本发明,但应该清楚,本发明不限于具体实施方式的范围,对本技术领域的普通技术人员来讲,只要各种变化在所附的权利要求限定和确定的本发明的精神和范围内,这些变化是显而易见的,一切利用本发明构思的发明创造均在保护之列。The specific embodiments of the present invention are described below to facilitate those skilled in the art to understand the present invention. However, it should be clear that the present invention is not limited to the scope of the specific embodiments. For those of ordinary skill in the technical field, as long as various changes These changes are obvious within the spirit and scope of the invention as defined and determined by the appended claims, and all inventions and creations utilizing the concept of the invention are protected.

如图1所示,一种基于高分三号的时序雷达干涉监测方法,包括步骤S1-S5,具体如下:As shown in Figure 1, a time-series radar interference monitoring method based on Gaofen-3 includes steps S1-S5, as follows:

S1、利用高分三号获取目标区域的干涉相位图。S1. Use Gaofen-3 to obtain the interference phase map of the target area.

在本发明的一个可选实施例中,本发明选取待监测的目标区域,并利用高分三号获取目标区域的干涉相位图。本发明利用高分三号获取的干涉相位图存在轨道误差和基线误差,仅有少量干涉相位图可以被应用于时序雷达干涉监测领域。In an optional embodiment of the present invention, the present invention selects a target area to be monitored, and uses Gaofen-3 to obtain the interference phase map of the target area. The interference phase diagram obtained by the present invention using Gaofen-3 has orbit errors and baseline errors, and only a small number of interference phase diagrams can be applied to the field of time-series radar interference monitoring.

S2、根据步骤S1中目标区域的干涉相位图和数字高程模型数据获取目标区域的缠绕干涉相位图。S2. Obtain the winding interference phase diagram of the target area according to the interference phase diagram of the target area and the digital elevation model data in step S1.

在本发明的一个可选实施例中,本发明根据目标区域的干涉相位图生成目标区域的单视缠绕干涉相位图,并根据数字高程模型数据目标区域的单视缠绕干涉相位图进行去平地和地形改正,获取目标区域的缠绕干涉相位图。In an optional embodiment of the present invention, the present invention generates a single-view wrapping interference phase diagram of the target area based on the interference phase diagram of the target area, and performs flattening and summing based on the single-view wrapping interference phase diagram of the target area using digital elevation model data. Terrain correction is performed to obtain the winding interference phase map of the target area.

步骤S2包括以下分步骤:Step S2 includes the following sub-steps:

S21、对步骤S1中目标区域的干涉相位图进行配准和干涉组合,生成目标区域的单视缠绕干涉相位图。S21. Perform registration and interference combination on the interference phase images of the target area in step S1 to generate a single-view winding interference phase image of the target area.

具体地,本发明对目标区域的干涉相位图进行配准和干涉组合,生成目标区域的单视缠绕干涉相位图。Specifically, the present invention performs registration and interference combination on the interference phase images of the target area to generate a single-view winding interference phase image of the target area.

S22、根据数字高程模型数据对分步骤S21中目标区域的单视缠绕干涉相位图进行去平地和地形改正,获取目标区域的缠绕干涉相位图。S22. Perform flattening and terrain correction on the single-view winding interference phase map of the target area in step S21 according to the digital elevation model data to obtain the winding interference phase map of the target area.

S3、根据星历数据和步骤S2中目标区域的缠绕干涉相位图,获取目标区域去除密集条纹的缠绕干涉相位图。S3. According to the ephemeris data and the winding interference phase map of the target area in step S2, obtain the winding interference phase map of the target area with dense fringes removed.

在本发明的一个可选实施例中,本发明根据星历数据和目标区域的缠绕干涉相位图,采用状态矢量估计和干涉条纹频率数据结合的办法,对高分三号干涉相位图中存在的轨道误差和基线误差进行初步的修正,获取目标区域去除密集条纹的缠绕干涉相位图。In an optional embodiment of the present invention, based on the ephemeris data and the winding interference phase diagram of the target area, the present invention adopts a method of combining state vector estimation and interference fringe frequency data to detect the interference phase diagram existing in the Gaofen-3 The orbit error and baseline error are initially corrected, and the winding interference phase map of the target area is obtained with dense fringes removed.

步骤S3包括以下分步骤:Step S3 includes the following sub-steps:

S31、根据星历数据,利用轨道状态矢量估计获取目标区域的缠绕干涉相位图的第一初始基线。S31. According to the ephemeris data, use orbital state vector estimation to obtain the first initial baseline of the winding interference phase diagram of the target area.

步骤S31包括以下分步骤:Step S31 includes the following sub-steps:

S311、根据星历数据,拟合卫星的时间位置曲线。S311. Fit the time position curve of the satellite according to the ephemeris data.

本发明拟合卫星的时间位置曲线,表示为:The present invention fits the time position curve of the satellite, which is expressed as:

其中:为天线中心的/>轴坐标值,/>为天线中心的/>轴的常数项系数,/>为天线中心的/>轴的一次项系数,/>为采样点时间,/>为天线中心的/>轴的二次项系数,/>为天线中心的/>轴的三次项系数,/>为天线中心的/>轴坐标值,/>为天线中心的/>轴的常数项系数,/>为天线中心的/>轴的一次项系数,/>为天线中心的/>轴的二次项系数,/>为天线中心的/>轴的三次项系数,/>为天线中心的/>轴坐标值,/>为天线中心的/>轴的常数项系数,/>为天线中心的/>轴的一次项系数,/>为天线中心的/>轴的二次项系数,/>为天线中心的/>轴的三次项系数。in: is the center of the antenna/> Axis coordinate value,/> is the center of the antenna/> The constant term coefficient of the axis,/> is the center of the antenna/> The linear term coefficient of the axis,/> is the sampling point time,/> is the center of the antenna/> The coefficient of the quadratic term of the axis,/> is the center of the antenna/> Coefficient of cubic term of axis,/> is the center of the antenna/> Axis coordinate value,/> is the center of the antenna/> The constant term coefficient of the axis,/> is the center of the antenna/> The linear term coefficient of the axis,/> is the center of the antenna/> The coefficient of the quadratic term of the axis,/> is the center of the antenna/> Coefficient of cubic term of axis,/> is the center of the antenna/> Axis coordinate value,/> is the center of the antenna/> The constant term coefficient of the axis,/> is the center of the antenna/> The linear term coefficient of the axis,/> is the center of the antenna/> The coefficient of the quadratic term of the axis,/> is the center of the antenna/> Coefficient of the cubic term of the axis.

具体地,本发明根据星历数据可以获取高分三号干涉相位图中记录的卫星运行过程中天线中心的位置和采样点时间,能利用这些数据拟合上述时间位置曲线。Specifically, based on the ephemeris data, the present invention can obtain the position of the antenna center and the sampling point time recorded in the Gaofen-3 interference phase diagram during satellite operation, and can use these data to fit the above time position curve.

S312、根据最小二乘法计算分步骤S311中卫星的时间位置曲线的未知参数,获取卫星的轨道曲线模型。S312. Calculate the unknown parameters of the time position curve of the satellite in step S311 according to the least squares method, and obtain the orbit curve model of the satellite.

具体地,本发明获取五个天线中心的位置点数据,根据最小二乘法能求解时间位置曲线中的位置参数,即坐标轴对应的常数项系数、一次项系数、二次项系数和三次项系数,进而获取卫星轨道曲线模型。Specifically, the present invention obtains the position point data of the five antenna centers, and can solve the position parameters in the time position curve according to the least squares method, that is, the constant term coefficient, linear term coefficient, quadratic term coefficient and cubic term coefficient corresponding to the coordinate axis. , and then obtain the satellite orbit curve model.

S313、根据分步骤S312中卫星的轨道曲线模型,获取目标区域的缠绕干涉相位图的第一初始基线。S313. According to the orbit curve model of the satellite in step S312, obtain the first initial baseline of the winding interference phase diagram of the target area.

S32、获取干涉条纹频率数据,并根据干涉条纹频率数据获取目标区域的缠绕干涉相位图的第二初始基线。S32. Obtain the interference fringe frequency data, and obtain the second initial baseline of the winding interference phase diagram of the target area based on the interference fringe frequency data.

具体地,本发明通过极大似然估计频率法能获取干涉条纹频率数据。本发明通过快速傅里叶变换方法,将目标区域的缠绕干涉相位图从空间域转换到频率域以计算干涉条纹频率,表示为:Specifically, the present invention can obtain interference fringe frequency data through the maximum likelihood estimation frequency method. This invention uses the fast Fourier transform method to convert the winding interference phase map of the target area from the spatial domain to the frequency domain to calculate the interference fringe frequency, which is expressed as:

其中:为转换到频率域的目标区域的缠绕干涉相位图,/>为虚数单位,/>为轨道跳变相位,/>为形变相位,/>为雷达坐标系下的/>轴坐标,/>为雷达坐标系下的/>轴坐标,/>为距离向的频率,/>为方位向的频率,/>为残余相位。in: is the winding interference phase diagram of the target region converted to the frequency domain,/> is an imaginary unit,/> is the track jump phase,/> is the deformation phase,/> is/> in the radar coordinate system Axis coordinates,/> is/> in the radar coordinate system Axis coordinates,/> is the frequency in the distance direction,/> is the frequency in the azimuth direction,/> is the residual phase.

本发明能根据条纹频率推导第二初始基线与干涉条纹频率之间的关系,进而根据得到的干涉条纹频率数据获取目标区域的缠绕干涉相位图的第二初始基线。The present invention can deduce the relationship between the second initial baseline and the interference fringe frequency based on the fringe frequency, and then obtain the second initial baseline of the winding interference phase diagram of the target area based on the obtained interference fringe frequency data.

S33、根据分步骤S31中的第一初始基线和分步骤S32中的第二初始基线,获取目标区域去除密集条纹的缠绕干涉相位图。S33. According to the first initial baseline in step S31 and the second initial baseline in step S32, obtain the winding interference phase map of the target area with dense fringes removed.

S4、根据多项式拟合、线性回归模型和步骤S3中目标区域去除密集条纹的缠绕干涉相位图,获取目标区域修正后的缠绕干涉相位图。S4. According to the polynomial fitting, the linear regression model and the winding interference phase image of the target area with dense fringes removed in step S3, obtain the corrected winding interference phase image of the target area.

在本发明的一个可选实施例中,本发明对初步修正后的干涉相位图进行相位解缠,并根据多项式拟合、线性回归模型和目标区域去除密集条纹的缠绕干涉相位图,能拟合轨道误差的残余相位和大气误差,消除轨道误差中的非线性误差,以对初步修正后的干涉相位图进行进一步的精细化修正,获取目标区域修正后的解缠干涉相位图。In an optional embodiment of the present invention, the present invention performs phase unwrapping on the preliminary corrected interference phase diagram, and can fit the entangled interference phase diagram with dense fringes removed based on polynomial fitting, linear regression model and target area. The residual phase of the orbit error and the atmospheric error are eliminated to eliminate the nonlinear error in the orbit error to further refine the preliminary corrected interference phase map and obtain the corrected unwrapped interference phase map of the target area.

步骤S4包括以下分步骤:Step S4 includes the following sub-steps:

S41、对步骤S3中目标区域去除密集条纹的缠绕干涉相位图进行相位解缠,获取目标区域的解缠干涉相位图。S41. Perform phase unwrapping on the entangled interference phase image of the target area with dense fringes removed in step S3, and obtain the unwrapped interference phase image of the target area.

S42、根据多项式拟合分步骤S41中目标区域的解缠干涉相位图的相位跳变,获取轨道误差的残余相位。S42. Obtain the residual phase of the orbit error according to the phase transition of the unwrapped interference phase diagram of the target area in step S41 of polynomial fitting.

本发明拟合分步骤S41中目标区域的解缠干涉相位图的相位跳变,获取轨道误差的残余相位,表示为:The present invention fits the phase jump of the unwrapped interference phase diagram of the target area in step S41, and obtains the residual phase of the orbit error, which is expressed as:

其中:为解缠干涉相位图中轨道误差的残余相位,/>为雷达坐标系下的/>轴坐标,/>为雷达坐标系下的/>轴坐标,/>为残余相位的第一系数,/>为残余相位的第二系数,/>为残余相位的第三系数,/>为残余相位的第四系数,/>为残余相位的第五系数,/>为残余相位的第六系数。in: is the residual phase of the orbit error in the unwrapped interference phase diagram,/> is/> in the radar coordinate system Axis coordinates,/> is/> in the radar coordinate system Axis coordinates,/> is the first coefficient of the residual phase,/> is the second coefficient of the residual phase,/> is the third coefficient of the residual phase,/> is the fourth coefficient of the residual phase,/> is the fifth coefficient of the residual phase,/> is the sixth coefficient of the residual phase.

S43、根据分步骤S41中目标区域的解缠干涉相位图,利用线性回归模型获取大气误差。S43. According to the unwrapped interference phase diagram of the target area in step S41, use the linear regression model to obtain the atmospheric error.

本发明利用线性回归模型获取大气误差,表示为:This invention uses a linear regression model to obtain the atmospheric error, which is expressed as:

其中:为解缠干涉相位图中的大气误差,/>为雷达坐标系下的/>轴坐标,为雷达坐标系下的/>轴坐标,/>为大气误差的第一系数,/>为大气误差的第二系数,为解缠干涉相位图中的高程信息。in: To unwrap the atmospheric errors in the interference phase diagram,/> is/> in the radar coordinate system axis coordinates, is/> in the radar coordinate system Axis coordinates,/> is the first coefficient of atmospheric error,/> is the second coefficient of atmospheric error, To unwrap the elevation information in the interference phase image.

S44、根据多项式拟合分步骤S42中轨道误差的残余相位和分步骤S43中的大气误差,获取拟合结果。S44. Obtain the fitting result according to the residual phase of the orbit error in step S42 and the atmospheric error in step S43 of polynomial fitting.

S45、根据分步骤S44中的拟合结果修正步骤S3中去除密集条纹的缠绕干涉相位图,获取目标区域修正后的缠绕干涉相位图。S45. Correct the winding interference phase image from which the dense fringes are removed in step S3 according to the fitting result in step S44, and obtain the corrected winding interference phase image of the target area.

S5、根据步骤S4中目标区域修正后的缠绕干涉相位图,采用时序雷达干涉测量方法获取目标区域的高分三号影像的时序形变速率图,以实现目标区域的监测。S5. According to the corrected winding interference phase diagram of the target area in step S4, use the time-series radar interferometry method to obtain the time-series deformation rate map of the Gaofen-3 image of the target area to achieve monitoring of the target area.

在本发明的一个可选实施例中,本发明根据目标区域修正后的缠绕干涉相位图,采用时序雷达干涉测量方法对获取目标区域修正后的缠绕干涉相位图进行相位改正和大气改正,获取目标区域的高分三号影像的时序形变速率图,以实现目标区域的监测。In an optional embodiment of the present invention, based on the corrected winding interference phase diagram of the target area, the present invention uses a time-series radar interferometry method to perform phase correction and atmospheric correction on the corrected winding interference phase diagram of the target area to obtain the target. The time series deformation rate diagram of the Gaofen-3 image in the area is used to monitor the target area.

步骤S5包括以下分步骤:Step S5 includes the following sub-steps:

S51、根据振幅差离差指数和步骤S4中目标区域修正后的缠绕干涉相位图,选取滤波相位失相干缓慢目标点的候选点。S51. Select the candidate point of the filtered phase decoherence slow target point according to the amplitude difference dispersion index and the corrected winding interference phase diagram of the target area in step S4.

S52、根据分步骤S51中滤波相位失相干缓慢目标点的候选点,确定相位误差。S52. Determine the phase error according to the candidate points of the filtered phase decoherence slow target point in step S51.

S53、根据分步骤S52中的相位误差确定像素噪声水平的测度参数。S53. Determine the measurement parameter of the pixel noise level according to the phase error in step S52.

S54、根据分步骤S53中像素噪声水平的测度参数和分步骤S51中滤波相位失相干缓慢目标点的候选点,选取滤波相位失相干缓慢目标点。S54. Select the filtered phase decoherence slow target point according to the measurement parameters of the pixel noise level in step S53 and the candidate points of the filtered phase decoherence slow target point in step S51.

S55、根据分步骤S54中的滤波相位失相干缓慢目标点、3D解缠方法和步骤S4中目标区域修正后的解缠干涉相位图,获取目标区域的高分三号影像的时序形变速率图,以实现目标区域的监测。S55. According to the filtered phase decoherence slow target point in step S54, the 3D unwrapping method and the corrected unwrapped interference phase diagram of the target area in step S4, obtain the time series deformation rate diagram of the Gaofen-3 image of the target area, To achieve monitoring of target areas.

具体地,本发明根据分步骤S54中的滤波相位失相干缓慢目标点,能对目标区域修正后的解缠干涉相位图进行相位改正,根据3D解缠方法对相位改正后的干涉相位图进行相位解缠,并利用空间相关误差改正方法对解缠后的干涉相位图进行大气改正,以获取目标区域的高分三号影像的时序形变速率图,进而实现对目标区域的准确监测。Specifically, the present invention can perform phase correction on the corrected unwrapped interference phase diagram of the target area according to the filtered phase decoherence slow target point in step S54, and perform phase correction on the phase-corrected interference phase diagram according to the 3D unwrapping method. Unwrapping, and using the spatial correlation error correction method to perform atmospheric correction on the unwrapped interference phase map to obtain the time-series deformation rate map of the Gaofen-3 image in the target area, thereby achieving accurate monitoring of the target area.

本发明是参照根据本发明实施例的方法、设备(系统)、和计算机程序产品的流程图和/或方框图来描述的。应理解可由计算机程序指令实现流程图和/或方框图中的每一流程和/或方框、以及流程图和/或方框图中的流程和/或方框的结合。可提供这些计算机程序指令到通用计算机、专用计算机、嵌入式处理机或其他可编程数据处理设备的处理器以产生一个机器,使得通过计算机或其他可编程数据处理设备的处理器执行的指令产生用于实现在流程图一个流程或多个流程和/或方框图一个方框或多个方框中指定的功能的装置。The invention is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the invention. It will be understood that each process and/or block in the flowchart illustrations and/or block diagrams, and combinations of processes and/or blocks in the flowchart illustrations and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing device to produce a machine, such that the instructions executed by the processor of the computer or other programmable data processing device produce a use A device for realizing the functions specified in one process or multiple processes of the flowchart and/or one block or multiple blocks of the block diagram.

这些计算机程序指令也可存储在能引导计算机或其他可编程数据处理设备以特定方式工作的计算机可读存储器中,使得存储在该计算机可读存储器中的指令产生包括指令装置的制造品,该指令装置实现在流程图一个流程或多个流程和/或方框图一个方框或多个方框中指定的功能。These computer program instructions may also be stored in a computer-readable memory that causes a computer or other programmable data processing apparatus to operate in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including the instruction means, the instructions The device implements the functions specified in a process or processes of the flowchart and/or a block or blocks of the block diagram.

这些计算机程序指令也可装载到计算机或其他可编程数据处理设备上,使得在计算机或其他可编程设备上执行一系列操作步骤以产生计算机实现的处理,从而在计算机或其他可编程设备上执行的指令提供用于实现在流程图一个流程或多个流程和/或方框图一个方框或多个方框中指定的功能的步骤。These computer program instructions may also be loaded onto a computer or other programmable data processing device, causing a series of operating steps to be performed on the computer or other programmable device to produce computer-implemented processing, thereby executing on the computer or other programmable device. Instructions provide steps for implementing the functions specified in a process or processes of a flowchart diagram and/or a block or blocks of a block diagram.

本发明中应用了具体实施例对本发明的原理及实施方式进行了阐述,以上实施例的说明只是用于帮助理解本发明的方法及其核心思想;同时,对于本领域的一般技术人员,依据本发明的思想,在具体实施方式及应用范围上均会有改变之处,综上所述,本说明书内容不应理解为对本发明的限制。The present invention uses specific embodiments to illustrate the principles and implementation methods of the present invention. The description of the above embodiments is only used to help understand the method of the present invention and its core idea; at the same time, for those of ordinary skill in the art, based on this The idea of the invention will be subject to change in the specific implementation and scope of application. In summary, the contents of this description should not be understood as limiting the invention.

本领域的普通技术人员将会意识到,这里所述的实施例是为了帮助读者理解本发明的原理,应被理解为本发明的保护范围并不局限于这样的特别陈述和实施例。本领域的普通技术人员可以根据本发明公开的这些技术启示做出各种不脱离本发明实质的其它各种具体变形和组合,这些变形和组合仍然在本发明的保护范围内。Those of ordinary skill in the art will appreciate that the embodiments described here are provided to help readers understand the principles of the present invention, and it should be understood that the scope of the present invention is not limited to such specific statements and embodiments. Those of ordinary skill in the art can make various other specific modifications and combinations based on the technical teachings disclosed in the present invention without departing from the essence of the present invention, and these modifications and combinations are still within the protection scope of the present invention.

Claims (9)

1. A time sequence radar interference monitoring method based on a third high-resolution method is characterized by comprising the following steps:
s1, acquiring an interference phase diagram of a target area by using a third high-resolution method;
s2, obtaining a winding interference phase diagram of the target area according to the interference phase diagram of the target area and the digital elevation model data in the step S1;
s3, obtaining a winding interference phase diagram of the target area with dense stripes removed according to the ephemeris data and the winding interference phase diagram of the target area in the step S2;
s4, according to polynomial fitting, a linear regression model and the winding interference phase diagram of the target area with dense stripes removed in the step S3, obtaining a winding interference phase diagram after the target area is corrected;
s5, acquiring a time sequence deformation rate chart of the high-resolution third image of the target area by adopting a time sequence radar interferometry method according to the winding interference phase chart corrected by the target area in the step S4 so as to realize the monitoring of the target area.
2. The method for interference monitoring of time sequence radar based on third high score according to claim 1, wherein the step S2 comprises the following sub-steps:
s21, registering and interference combining the interference images of the target area in the step S1 to generate a single-view winding interference phase diagram of the target area;
s22, carrying out land leveling and topography correction on the single-view winding interference phase diagram of the target area in the bisection step S21 according to the digital elevation model data, and obtaining the winding interference phase diagram of the target area.
3. The method for interference monitoring of time sequence radar based on third high score according to claim 1, wherein the step S3 comprises the following sub-steps:
s31, according to ephemeris data, acquiring a first initial baseline of a winding interference phase diagram of a target area by using orbit state vector estimation;
s32, obtaining interference fringe frequency data, and obtaining a second initial baseline of a winding interference phase diagram of the target area according to the interference fringe frequency data;
s33, obtaining a winding interference phase diagram of the target area with dense stripes removed according to the first initial baseline in the substep S31 and the second initial baseline in the substep S32.
4. A method of time-series radar interferometry based on third-order high score according to claim 3, wherein step S31 comprises the sub-steps of:
s311, fitting a time position curve of the satellite according to ephemeris data;
s312, calculating unknown parameters of the time position curve of the satellite in the substep S311 according to a least square method, and obtaining an orbit curve model of the satellite;
s313, acquiring a first initial baseline of a winding interference phase diagram of the target area according to the orbit curve model of the satellite in the substep S312.
5. The method for interference monitoring of time-series radar based on third-order high score according to claim 4, wherein in the substep S311, a time-position curve of the satellite is fitted, expressed as:
wherein:for the antenna centre +.>Axis coordinate value->For the antenna centre +.>Constant term coefficient of axis,/>For the antenna centre +.>Primary term coefficient of axis,/>For sampling point time, +.>For the antenna centre +.>Quadratic term coefficient of axis,/>For the antenna centre +.>The cubic term coefficient of the axis,/>For the antenna centre +.>Axis coordinate value->For the antenna centre +.>Constant term coefficient of axis,/>For the antenna centre +.>Primary term coefficient of axis,/>For the antenna centre +.>Quadratic term coefficient of axis,/>For the antenna centre +.>The cubic term coefficient of the axis,/>For the antenna centre +.>Axis coordinate value->For the antenna centre +.>Constant term coefficient of axis,/>For the antenna centre +.>Primary term coefficient of axis,/>For the antenna centre +.>Quadratic term coefficient of axis,/>For the antenna centre +.>The cubic term coefficient of the axis.
6. The method for interference monitoring of time sequence radar based on third high score according to claim 1, wherein the step S4 comprises the following sub-steps:
s41, performing phase unwrapping on the wrapping interference phase map with the dense stripes removed from the target area in the step S3 to obtain an unwrapped interference phase map of the target area;
s42, obtaining the residual phase of the track error according to the phase jump of the unwrapped interference phase diagram of the target area in the polynomial fitting substep S41;
s43, obtaining an atmospheric error by using a linear regression model according to the unwrapped interference phase diagram of the target area in the substep S41;
s44, obtaining a fitting result according to the residual phase of the orbit error in the polynomial fitting substep S42 and the atmospheric error in the substep S43;
s45, correcting the winding interference phase diagram with the dense stripes removed in the step S3 according to the fitting result in the substep S44, and obtaining a winding interference phase diagram corrected by the target area.
7. The method for monitoring interference of time-series radar based on third high-resolution method according to claim 6, wherein in the substep S42, phase jumps of unwrapped interference phase diagrams of the target area in the substep S41 are fitted, and residual phases of track errors are obtained, which are expressed as:
wherein:for unwrapping the residual phase of the track error in the interferometric phase map,/for example>Is +.>Axis coordinates->Is +.>Axis coordinates->First to be residual phaseCoefficient of->As a second coefficient of the residual phase,is the third coefficient of the residual phase, +.>Is the fourth coefficient of the residual phase, +.>Is the fifth coefficient of the residual phase, +.>Is the sixth coefficient of the residual phase.
8. The method for interference monitoring of time-series radar based on third-order high score according to claim 6, wherein in the substep S43, the atmospheric error is obtained by using a linear regression model, expressed as:
wherein:to unwrap atmospheric errors in the interferogram, +.>Is +.>Axis coordinates->Is +.>Axis coordinates->Is the first coefficient of atmospheric error, +.>Is a second coefficient of the atmospheric error,to unwrap elevation information in the interferometric phase map.
9. The method for interference monitoring of time sequence radar based on third high score according to claim 1, wherein the step S5 comprises the following sub-steps:
s51, selecting candidate points of a filtering phase coherence loss slow target point according to the amplitude difference dispersion index and the winding interference phase diagram corrected by the target area in the step S4;
s52, determining a phase error according to candidate points of the filtering phase loss coherent slow target point in the substep S51;
s53, determining a measure parameter of the pixel noise level according to the phase error in the substep S52;
s54, selecting a filtering phase incoherent slow target point according to the measure parameter of the pixel noise level in the substep S53 and the candidate point of the filtering phase incoherent slow target point in the substep S51;
s55, acquiring a time sequence deformation rate diagram of a high-resolution third image of the target area according to the filtering phase coherence loss slow target point in the substep S54, the 3D unwrapping method and the unwrapped interference phase diagram corrected by the target area in the step S4 so as to realize the monitoring of the target area.
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