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34 results about "Geopotential model" patented technology

In geophysics, a geopotential model is the theoretical analysis of measuring and calculating the effects of Earth's gravitational field.

GNSS-CCD-integrated zenith telescope high-precision vertical deflection fast measurement method

The invention discloses a GNSS-CCD-integrated zenith telescope high-precision vertical deflection fast measurement method. At a measurement station, the optical axis of a zenith telescope faces to the zenith and takes a picture of a zenith zone so that a CCD fixed star image is obtained, fixed star image coordinates are calculated, exposure epoch is controlled by geodetic coordinates and a GNSS time signal measured by GNSS, fixed star information in the zenith zone is acquired in an appropriate star catalogue according to the measurement station vertical deflection calculated by an EGM2008 geopotential model, coupling identification of fixed stars in a zenith tangent plane zone of a celestial sphere in the star catalogue and in the CCD fixed star image is realized, zenith astronomical coordinates are calculated by least spuare iterative computation, and vertical deflection of the observed point is calculated according to geodetic coordinates. Compared with the prior art, the method provided by the invention has the characteristics of simple operation, time and labor saving and high measurement precision and is suitable for high-precision vertical deflection fast measurement.
Owner:SHANDONG UNIV OF SCI & TECH

Method for improving ocean gravity field interpolation precision based on submarine topography three-dimensional optimization principle

The invention discloses a method for improving ocean gravity field interpolation precision based on a submarine topography three-dimensional optimization principle. The method comprises steps of submarine topography data and a global gravity field model being acquired; constructing a three-dimensional ocean gravity anomaly model according to the acquired submarine topographic data and the global gravity field model; performing interpolation calculation on the three-dimensional ocean gravity anomaly model to obtain a geoid three-dimensional correction model; and according to the geoid three-dimensional correction model, determining a gravity anomaly value at an unknown point in the prediction area to obtain a high-precision and high-spatial-resolution marine gravity anomaly map. According to the method, the submarine topography is introduced into a common two-dimensional Kriging formula, a novel submarine topography three-dimensional optimization method is constructed, the precision loss is minimized while the spatial resolution of the global marine gravity anomaly map is improved, the interpolation precision is high, the calculation speed is high, and an effective basis is providedfor improving the submarine gravity matching navigation precision.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY

Submarine navigation method and system based on multi-dimensional gravity gradient lighthouse

The invention relates to a submarine navigation method and a submarine navigation system based on a multi-dimensional gravity gradient lighthouse. The submarine navigation method comprises the following steps of: acquiring the position of a position point in the ocean; according to the position point, adopting a high-precision gravity field model to determine ocean gravity gradient data; screeningthe ocean gravity gradient data, and determining gravity gradient lighthouses; acquiring the position of the current sea region and the current position of a submarine; determining a matched gravitygradient lighthouse according to a gravity gradient lighthouse database, the position of the current sea region and the current position of the submarine; determining the position of the submarine according to the matched gravity gradient lighthouse and marine gravity gradient data measured by a ship-borne gradient gravimeter; and resetting an inertial navigation system according to the position of the submarine. According to the submarine navigation method and the submarine navigation system based on the multi-dimensional gravity gradient lighthouse, the safety and accuracy of navigation of the gravity lighthouse in a gravity gentle region can be improved.
Owner:中国人民解放军61540部队 +1

Method for improving ocean gravity reconstruction precision based on geoid three-dimensional correction principle

The invention discloses a method for improving ocean gravity reconstruction precision based on a geoid three-dimensional correction principle. The method comprises steps of a geoid and a global gravity field model being acquired; constructing a three-dimensional ocean gravity anomaly model according to the obtained geoid and global gravity field model; performing interpolation calculation on the three-dimensional ocean gravity anomaly model to obtain a geoid three-dimensional correction model; and according to the geoid three-dimensional correction model, determining a gravity abnormal value at an unknown point in the prediction area so as to improve the ocean gravity reconstruction precision. According to the statistical principle, prediction precision of the unknown point is improved byincreasing the amount of related information to optimize the estimated weight value, and precision loss is reduced to a large extent while the spatial resolution of the marine gravity reference map isimproved.
Owner:CHINA ACADEMY OF SPACE TECHNOLOGY

Method and device for determining seal level elevation by extracting GPS (Global Position System) signal gravity frequency shift

The invention discloses a method and device for determining seal level elevation, in particular relates to a method and device for determining seal level elevation by extracting GPS (Global Position System) signal gravity frequency shift. In the method, gravity frequency shift can be extracted based on GPS observation data (obs documents and sp3 documents) provided by an IGS (International GNSS (Global Navigation Satellite System) Service), and the gravity potential and the elevation of a single station are further determined based on gravity frequency shift signals. In addition, by means of a gravity field model, a theoretical value of the gravity frequency shift can be calculated and the effectiveness of the extracted gravity frequency shift signals can be verified. Accordingly, the invention has the following advantages: 1, because leveling measurement between two points with longer distance can be carried out without uninterrupted transmission by a plurality (or multiple) intermediate instrument stations, manpower and material resources are saved, a measurement period is short and the measurement is precise; 2, the measurement on a seal level elevation difference can be carried out between two points in a mountainous area or a place with higher near-distance elevation difference; and 3, a globally unified elevation datum can be realized.
Owner:WUHAN UNIV

Sea area gravity anomaly inversion method and system based on satellite height measurement data

The invention provides a sea area gravity anomaly inversion method and a system based on satellite height measurement data, and the method comprises the steps: calculating the sea surface height gradient of a sub-satellite point according to the sea surface height data collected by a satellite altimeter at the sub-satellite point in a preset sea area, and calculating the model vertical line deviation gradient of the sub-satellite point according to the position of the sub-satellite point, subtracting the sea surface height gradient of the sub-satellite point from the model vertical line deviation gradient to obtain the residual gradient of the sub-satellite point; converting the residual gradient of the sub-satellite point into a vertical line deviation grid based on a weighted least square method, and obtaining the residual vertical line deviation of the grid; and calculating the residual gravity anomaly of the grid according to the residual vertical line deviation of the grid, calculating the model gravity anomaly of the grid based on the gravity field model, and adding the model gravity anomaly of the grid and the residual gravity anomaly to obtain the sea area gravity anomaly value of the grid. According to the method, the accurate sea area gravity abnormal value is obtained after strict theoretical derivation.
Owner:CHINESE ACAD OF SURVEYING & MAPPING

Gravitational field model-assisted inverse distance weighted geoid-like grid interpolation method

The invention belongs to the field of surveying and mapping science and technology, and discloses a gravitational field model-assisted inverse distance weighted geoid-like grid interpolation method, which comprises the following steps of: searching four grid nodes closest to an interpolation point in a geoid-like grid numerical model; setting the geodetic coordinates of four grid nodes and geoid-like elevation anomaly according to the geoid-like grid numerical model; calculating model elevation anomalies of the grid nodes and the interpolation points according to the geodetic coordinates of the interpolation points and the searched grid nodes by using a reference gravity field model bit coefficient; substracting the model elevation anomaly from the geoid elevation anomaly of the grid points to obtain the residual elevation anomaly of the four grid nodes; according to the residual elevation anomaly of the grid node, calculating the residual elevation anomaly of the interpolation point by adopting an inverse distance weighting method; and adding the residual elevation anomaly of the interpolation point to the model elevation anomaly of the point to obtain a final elevation anomaly interpolation result of the interpolation point. The method can greatly improve the precision of the elevation anomaly interpolation result.
Owner:SHANDONG JIAOTONG UNIV

EMD filtering method and system for time-varying gravity field

InactiveCN112800831AHigh SNR valueStrong ability to remove noiseCharacter and pattern recognitionNoise removalComputational physics
The invention discloses an EMD filtering method and system for a time-varying gravity field. The EMD filtering method for the time-varying gravity field comprises the following steps: acquiring equivalent water height data; the equivalent water height data is obtained by calculating the time-varying gravity field model data; respectively performing empirical mode decomposition on the equivalent water height data according to latitude zones to obtain a limited number of intrinsic mode function parts and a residual part; calculating a cross correlation coefficient between the equivalent water height data and each intrinsic mode function part; determining an intrinsic mode function part corresponding to a first local minimum point in all cross correlation coefficients as an aliasing mode part; and performing reconstruction based on the intrinsic mode function part and the residual part after the aliasing mode part to obtain denoised equivalent water height data. According to the invention, the noise removal capability can be enhanced, and the signal-to-noise ratio of the filtered signal is improved.
Owner:CHANGAN UNIV +2

Radial basis function grid method for constructing sea area vertical line deviation model based on frequency domain characteristics

The invention relates to a radial basis function grid method for constructing a sea area plumb line deviation model based on frequency domain characteristics, which is technically characterized by comprising the following steps of: removing plumb line deviation in a sea plumb line deviation observation value by utilizing medium-long wave frequency spectrum information provided by a global gravityfield model to obtain residual plumb line deviation at an observation point; based on the residual vertical line deviation at the observation point, applying a radial basis function interpolation algorithm to obtain the residual vertical line deviation at the point to be estimated; recovering the model values of the meridian component and the mortise unitary component residual error of the vertical line deviation of the to-be-estimated point to obtain the calculation values of the meridian component and the mortise unitary component residual error of the vertical line deviation of the to-be-estimated point at the to-be-estimated point. The method is reasonable in design, the ocean plumb line deviation observed value serves as basic data, the global gravity field spherical harmonic model iscombined, a radial basis function interpolation method based on frequency domain characteristics is adopted, and the high-precision and high-resolution sea area plumb line deviation model can be constructed.
Owner:THE CHINESE PEOPLES LIBERATION ARMY 92859 TROOPS

Earth gravity field model modeling method based on orbital mask differential operator

ActiveCN111198402AImproved level of precisionSuppression of high frequency errorsGravitational wave measurementAccelerometerComputational physics
The invention discloses an earth gravity field model modeling method based on an orbit mask differential operator, which relates to the technical field of satellite gravity detection. The method comprises the steps of: carrying out the data preprocessing of orbit state information, a satellite-borne accelerometer and satellite attitude data, calculating the movement speed of the satellite by usingan orbit mask differential operator so as to obtain the kinetic energy and the rotation position of the satellite, establishing an observation equation meeting the law of conservation of energy through satellite kinetic energy, a rotation position, a conservative force position and a non-conservative force position, estimating a position coefficient correction value under the least square criterion, and determining a final earth gravity field model by adding a reference gravity field model position coefficient. Compared with a traditional method for determining the earth gravity field model by utilizing the orbit Newton polynomial differential speed, the method provided by the invention effectively suppresses high-frequency error amplification to realize noise reduction, is high in flexibility and calculation efficiency, obtains a high-precision satellite speed observation value, and further improves the precision level of the earth gravity field model.
Owner:EAST CHINA UNIV OF TECH

Satellite gravitational gradient data precision verification method based on tensor invariant theory

The invention discloses a satellite gravitational gradient data precision verification method based on a tensor invariant theory. The method comprises the following steps: verifying the overall precision of a satellite gravitational gradient tensor and verifying the component independent precision of the satellite gravitational gradient tensor, wherein the component independent precision verification of the satellite gravitational gradient tensor comprises independent precision verification of each component of the satellite gravitational gradient tensor before and after calibration. Accordingto the satellite gravitational gradient data precision verification method based on a tensor invariant theory provided by the invention, on the basis of the tensor invariant theory, the tensor invariant characteristic of a satellite gravitational gradient observation value is applied to precision verification before and after calibration of a gravitational gradient measurement satellite gravimeter, and overall precision verification of the six components of the gravitational gradient tensor is achieved. By introducing a priori gravitational field model for calibration, precision independent verification of the six components of the main diagonal line and an off-diagonal line of the gravitational gradient tensor can be realized.
Owner:自然资源部国土卫星遥感应用中心

Method for realizing elevation measurement by using gravity, GNSS-RTK and gravity field model

The invention discloses a method for realizing elevation measurement by utilizing gravity, GNSS-RTK and a gravity field model. The method comprises the following steps of: 1, acquiring geodetic coordinates of a measurement point; 2, obtaining a gravity value of the measurement point; 3, acquiring elevation anomaly of the measurement point; 4, obtaining the gravitational potential difference of the measurement point; and 5, obtaining the normal height of a point to be measured. The method is simple in step and reasonable in design, the geodetic height of the measurement points is obtained through the GNSS-RTK measurement technology, the gravity potential difference between the measurement points is obtained through flowing gravity observation, the height anomaly of the measurement points is calculated through the gravity field model, and finally the normal height of the point to be measured is calculated, so that high-precision height measurement is achieved.
Owner:雷军珍

Gravity satellite east-west direction differential observation data construction and inversion method and system

The invention relates to a gravity satellite east-west direction differential observation data construction and inversion method and system. The method comprises the following steps: carrying out datainterpolation and gridding processing on the basis of the observation data measured by a GNSS and the observation data of an accelerometer, carrying out difference processing on the positions, speedsand accelerations of a plurality of adjacent grid points in the east-west direction to obtain east-west differential observation data, further constructing an observation equation based on the east-west differential observation data, performing respective time-varying field calculation on north-south and east-west observation equations, finally performing spectral combination calculation on north-south and east-west gravitational field models, and calculating a final time-varying gravitational field model. The east-west observation data construction and inversion technology can effectively solve the problem of south-north stripes of a satellite inversion gravity field, thereby improving the gravitational field calculation precision. Compared with other methods, the algorithm provided by the invention is simple to implement, and the stability and reliability of the gravitational field calculation result can be ensured on the whole.
Owner:中国人民解放军61540部队

Method for constructing global gravity field based on carrier phase differential velocity

ActiveCN111308570AHigh solution accuracyReduce systematic bias between epochsGravitational wave measurementAccelerometerCarrier signal
The invention discloses a method for constructing a global gravity field based on carrier phase differential velocity, which relates to the technical field of satellite gravity detection. The method comprises the following steps: S1, carrying out data preprocessing on a carrier phase, orbit state information, an accelerometer, satellite attitude and other original observation values; S2, obtainingsatellite kinetic energy and a rotation position by utilizing a carrier phase differential speed; and S3, establishing an observation equation through the satellite kinetic energy, the rotation position and various perturbation positions, and estimating a global gravity field potential coefficient under a least square criterion based on the energy conservation law. Compared with the traditional energy conservation method for inverting the gravity field model by using the orbit differential velocity, the algorithm provided by the invention does not need to estimate the phase ambiguity, reducesthe system deviation between epochs, is convenient to implement quality control on the motion velocity of the carrier, so that the resolving precision of the global gravity field model is improved.
Owner:EAST CHINA UNIV OF TECH

A submarine navigation method and system based on a multi-dimensional gravity gradient lighthouse

The invention relates to a submarine navigation method and system based on a multi-dimensional gravity gradient lighthouse. The method includes obtaining the position of a position point in the ocean; according to the position point, using a high-precision gravity field model to determine the ocean gravity gradient data; screening the ocean gravity gradient data to determine the gravity gradient lighthouse; acquiring the position of the current sea area and the submarine Determine the matching gravity gradient lighthouse according to the gravity gradient lighthouse database, the position of the current sea area and the current position of the submarine; determine the position of the submarine according to the ocean gravity gradient data measured by the matching gravity gradient lighthouse and the on-board gradient gravimeter; Reset the inertial navigation system based on the submarine's position. The invention provides a submarine navigation method and system based on a multi-dimensional gravity gradient lighthouse, which can improve the safety and accuracy of gravity lighthouse navigation in a gentle gravity area.
Owner:中国人民解放军61540部队 +1

A method and system for calibrating an accelerometer using a satellite tracking satellite device

ActiveCN109581523BSolve problems that cannot meet better accuracy requirementsAvoid problems with terrain constraints, etc.Gravitational wave measurementAccelerometerSatellite tracking
The invention discloses a method and system for calibrating an accelerometer using a satellite-to-satellite tracking device. The method comprises the steps that original observation data on the satellite-to-satellite tracking device is acquired; coordinate transformation is performed on the original observation data to obtain observation data after the coordinate transformation; a gravity gradientcalculated value is calculated and obtained according to the observation data after the coordinate transformation and a gravity gradient observation equation; deviation calculation is performed on the gravity gradient calculated value and an actual gravity gradient observation value to obtain a deviation value; and the actual gravity gradient observation value is calibrated according to the deviation value. The method and system adopt the satellite-to-satellite tracking device to acquire the observation value, and calculate and obtain the gravity gradient calculated value, thereby effectivelysolving the problem that data generated simply by a gravity field model cannot meet better precision requirements, solving the problems such as terrain constraints, and achieving the purpose of high-precision calibration of the gravity accelerometer.
Owner:湖北省地震局

Method and device for determining seal level elevation by extracting GPS (Global Position System) signal gravity frequency shift

The invention discloses a method and device for determining seal level elevation, in particular relates to a method and device for determining seal level elevation by extracting GPS (Global Position System) signal gravity frequency shift. In the method, gravity frequency shift can be extracted based on GPS observation data (obs documents and sp3 documents) provided by an IGS (International GNSS (Global Navigation Satellite System) Service), and the gravity potential and the elevation of a single station are further determined based on gravity frequency shift signals. In addition, by means of a gravity field model, a theoretical value of the gravity frequency shift can be calculated and the effectiveness of the extracted gravity frequency shift signals can be verified. Accordingly, the invention has the following advantages: 1, because leveling measurement between two points with longer distance can be carried out without uninterrupted transmission by a plurality (or multiple) intermediate instrument stations, manpower and material resources are saved, a measurement period is short and the measurement is precise; 2, the measurement on a seal level elevation difference can be carried out between two points in a mountainous area or a place with higher near-distance elevation difference; and 3, a globally unified elevation datum can be realized.
Owner:WUHAN UNIV

Correction Method of Horizontal Component Error of Strapdown Gravity Meter Using Gravity Field Model

The invention belongs to the field of gravity measurement, specifically discloses a strapdown gravimeter horizontal component measurement error correction method through utilization of an earth gravity field model and aims at eliminating a low frequency error in a gravimeter measurement result horizontal component. The low frequency error results from an attitude error. The method comprises the steps of (1), preprocessing original data of a strapdown airborne gravimeter; (2), processing the original data of a GNSS to obtain carrier position, speed and acceleration information; (3), carrying out combined Kalman filtering on the strapdown gravimeter and the GNSS to obtain specific force; (4), computing difference between a specific force result and carrier acceleration of the GNSS to obtaina gravity vector estimated result; (5), carrying out lowpass filtering on the gravity vector result to eliminate a high frequency noise; and (6), carrying out highpass filtering on the gravity vectorresult to eliminate a low frequency part comprising the attitude error and replacing the low frequency part through utilization of a computing result of the earth gravity field model, thereby obtaining a horizontal component estimated result in which the attitude error is eliminated. The method is characterized by good theoretical basis, high operability and simple realization.
Owner:NAT UNIV OF DEFENSE TECH

Inertial navigation precision compensation method based on airspace Kriging grid method

The invention discloses an inertial navigation precision compensation method based on an airspace Kriging grid method, and the method comprises the steps: removing a low-frequency information model value, calculated based on a global gravity field model, of a disturbance gravity component of an observation point from an observation value of the disturbance gravity component, and obtaining a residual value of the disturbance gravity component of the observation point; on the basis of the residual value of the disturbance gravity component of the observation point, calculating the residual value of the disturbance gravity component of the to-be-estimated point by applying an airspace Kriging grid algorithm; and combining the residual value of the disturbance gravity component of the to-be-estimated point with the low-frequency information model value of the disturbance gravity component of the to-be-estimated point calculated based on the global gravity field model to obtain a disturbance gravity component calculated value of the to-be-estimated point. According to the method, the low-frequency information of the disturbance gravity component is strictly correct in principle, the spectral characteristics of the disturbance gravity component are considered to suppress the grid error influence in a medium-long wave band, and the spatial Kriging technology is utilized to improve the model resolution.
Owner:CHANGSHA UNIVERSITY

Inertial instrument error correction method based on airspace bilinear grid function

The invention discloses an inertial instrument error correction method based on an airspace bilinear grid function, and the method comprises the steps: removing a low-frequency information model value, calculated based on a global gravity field model, of a disturbance gravity component of an observation point from an observation value of the disturbance gravity component, and obtaining a residual value of the disturbance gravity component of the observation point; on the basis of the residual value of the disturbance gravity component of the observation point, calculating the residual value of the disturbance gravity component of the to-be-estimated point by applying an airspace bilinear grid algorithm; and combining the residual value of the disturbance gravity component of the to-be-estimated point with the low-frequency information model value of the disturbance gravity component of the to-be-estimated point calculated based on the global gravity field model to obtain a disturbance gravity component calculated value of the to-be-estimated point. According to the method, the low-frequency information of the disturbance gravity component is strictly correct in principle, the spectral characteristics of the disturbance gravity component are considered to suppress the grid error influence in a medium-long wave band, and the spatial bilinear technology is utilized to improve the model resolution.
Owner:CHANGSHA UNIVERSITY

Inertial navigation precision compensation method of local polynomial model considering frequency domain characteristics

The invention discloses an inertial navigation precision compensation method of a local polynomial model considering frequency domain characteristics; the method comprises the following steps: removing a low-frequency information model value of a disturbance gravity component of an observation point calculated on the basis of a global gravity field model from an observation value of the disturbance gravity component to obtain a residual value of the disturbance gravity component of the observation point; applying a spatial domain local polynomial grid algorithm based on the residual value of the disturbance gravity component of the observation point, and calculating the residual value of the disturbance gravity component of the to-be-estimated point; and combining the residual value of the disturbance gravity component of the to-be-estimated point with the low-frequency information model value of the disturbance gravity component of the to-be-estimated point calculated based on the global gravity field model to obtain a disturbance gravity component calculated value of the to-be-estimated point. According to the method, the low-frequency information of the disturbance gravity component is strictly correct in principle, the spectral characteristics of the disturbance gravity component are considered to suppress the grid error influence in a medium-long wave band, and the spatial domain local polynomial technology is utilized to improve the model resolution.
Owner:CHANGSHA UNIVERSITY

Inertial navigation precision compensation method based on airspace moving average grid method

The invention discloses an inertial navigation precision compensation method based on an airspace moving average grid method, and the method comprises the steps: removing a low-frequency information model value, calculated based on a global gravity field model, of a disturbance gravity component of an observation point from an observation value of the disturbance gravity component, and obtaining a residual value of the disturbance gravity component of the observation point; on the basis of the residual value of the disturbance gravity component of the observation point, calculating the residual value of the disturbance gravity component of the to-be-estimated point by applying an airspace moving average grid algorithm; and combining the residual value of the disturbance gravity component of the to-be-estimated point with the low-frequency information model value of the disturbance gravity component of the to-be-estimated point calculated based on the global gravity field model to obtain a disturbance gravity component calculated value of the to-be-estimated point. The method can ensure that the low-frequency information of the disturbance gravity component is strict and correct in principle, considers the spectral characteristics of the disturbance gravity component to suppress the grid error influence in the medium-long wave band, and improves the model resolution by using the airspace moving average technology.
Owner:CHANGSHA UNIVERSITY

A fast measurement method for high-precision vertical line deviation integrated with gnss and ccd zenith

The invention discloses a high-precision vertical line deviation rapid measurement method integrating GNSS and CCD zenith tube, which shoots the zenith area by making the optical axis of the zenith tube point to the zenith direction at the station to obtain CCD Stellar images, and the image coordinates of the stars are calculated, the exposure epoch is controlled by the geodetic coordinates measured by GNSS and the GNSS time signal, combined with the vertical line deviation of the station calculated by the EGM2008 gravity field model, the zenith is obtained in the applicable star catalog Regional star information, realize the matching and identification of stars in the zenith tangent plane area of ​​​​the celestial sphere in the star catalog and stars in the CCD star image, use the least square method to iteratively calculate the zenith astronomical coordinates, and combine the geodetic coordinates to calculate the vertical line deviation of the observation point. Compared with the prior art, the present invention has the advantages of simple operation, time-saving and labor-saving, and high measurement accuracy, and is suitable for rapid measurement of high-precision vertical line deviation.
Owner:SHANDONG UNIV OF SCI & TECH

Local gravity field modeling method and system based on ground gravity measurement data

PendingCN113466959AHigh precisionSolving difficult problems where classical spherical harmonic methods cannot be appliedGravitational wave measurementMathematical modelObservation data
The invention provides a local gravity field modeling method and system based on ground gravity measurement data, and the method comprises the steps: collecting ground gravity observation data in a research region, carrying out the preprocessing, determining the spatial resolution of a gravity field model and the maximum expansion order of the gravity field model, carrying out the low-pass filtering of the preprocessed data, filtering out a part higher than a maximum expansion order in the ground gravity observation data to obtain filtered gravity observation data in a research area, then determining a closed boundary of the research area, obtaining an orthogonal primary function group and an optimal primary function number through calculation, obtaining an expansion coefficient of a Slepian method through calculation, consequently, obtaining a mathematical model describing the gravitational field in the research area, and finally, according to the mathematical model of the gravitational field, calculating to obtain a gravitational field signal of any point in the research area. According to the method, the problem that a classic spherical harmonic method cannot be applied in a spherical local range is solved by constructing the orthogonal basis function in the research area.
Owner:INST OF GEOPHYSICS CHINA EARTHQUAKE ADMINISTRATION

Method for determining 1985 elevation reference gravitational potential of China

The invention relates to a method for determining the 1985 elevation reference gravitational potential of China, which comprises the following steps of constructing a combined gravitational field model, adopting the corresponding order of a GRACE / COCE gravitational field model for the first k orders, and adopting the corresponding order of an EGM2008 gravitational field model for the k-2190 orders of the combined gravitational field model, for different k values, calculating the precision of the corresponding combined gravitational field model, selecting the gravitational field model with the highest precision as an optimal combination order gravitational field model, obtaining the longitude and latitude of the target area, and calculating the elevation reference gravitational potential of the target area through the optimal combination order gravitational field model. According to the method, the combined gravitational field model is jointly constructed based on the GRACE or COCE gravitational field model and the EGM2008 gravitational field model, the short wave precision of the gravitational field model can be better improved, and the model precision is further improved. The optimal combined order gravitational field model is adopted to calculate the elevation reference gravitational potential of the target area, the elevation reference gravitational potential of China can be determined with higher precision, and effective unification of the 1985 elevation reference and the global elevation reference in China is achieved.
Owner:NAT GEOMATICS CENT OF CHINA

Inertial navigation precision compensation method considering frequency domain characteristics based on radial basis function

The invention discloses an inertial navigation precision compensation technology compensation method considering frequency domain characteristics based on a radial basis function; the method comprises the following steps: removing a low-frequency information model value of a disturbance gravity component of an observation point calculated based on a global gravity field model from an observation value of the disturbance gravity component; obtaining a residual value of the disturbance gravity component of the observation point; on the basis of the residual value of the disturbance gravity component of the observation point, calculating the residual value of the disturbance gravity component of the to-be-estimated point by applying an airspace radial basis function grid algorithm and combining the residual value of the disturbance gravity component of the to-be-estimated point with the low-frequency information model value of the disturbance gravity component of the to-be-estimated point calculated based on the global gravity field model to obtain a disturbance gravity component calculated value of the to-be-estimated point. The method can ensure that the low-frequency information of the disturbance gravity component is strict and correct in principle, considers the spectral characteristics of the disturbance gravity component to suppress the grid error influence in a medium-long wave band, and improves the model resolution by using the spatial domain radial basis function technology.
Owner:CHANGSHA UNIVERSITY

Verification Method of Satellite Gravitational Gradient Data Accuracy Based on Tensor Invariant Theory

The invention discloses a method for verifying the accuracy of satellite gravitational gradient data based on the tensor invariant theory, comprising the following steps: verifying the overall accuracy of the satellite gravitational gradient tensor and verifying the component-independent accuracy of the satellite gravitational gradient tensor; Component-independent accuracy verification of the tensor includes independent accuracy verification of each component of the satellite gravitational gradient tensor before and after calibration. The method for verifying the accuracy of satellite gravitational gradient data based on the tensor invariant theory disclosed by the present invention uses the tensor invariant characteristics of satellite gravitational gradient observations to calibrate gravity gradient measurement satellite gravity gradiometers based on the tensor invariant theory In the previous and subsequent accuracy verification, the overall accuracy verification of the six components of the gravitational gradient tensor was realized; by introducing a priori gravity field model for calibration, the six components of the main diagonal and off-diagonal of the gravitational gradient tensor can be verified. Accuracy independently verified.
Owner:自然资源部国土卫星遥感应用中心

Inverse distance weighted grid method for constructing sea area plumb line deviation model based on frequency domain characteristics

The invention relates to an inverse distance weighted grid method for constructing a sea area plumb line deviation model based on frequency domain characteristics, which comprises the following stepsof removing plumb line deviation in a sea plumb line deviation observation value by utilizing medium-long wave frequency spectrum information provided by a global gravity field model, and calculatingto obtain residual plumb line deviation at an observation point; on the basis of the residual vertical line deviation at the observation point, calculating to obtain the residual vertical line deviation at the to-be-estimated point by applying an inverse distance weighted interpolation algorithm; and recovering the model value of the residual error of the meridian component and the mortise unitarycomponent of the vertical line deviation of the to-be-estimated point, and calculating to obtain the vertical line deviation value at the to-be-estimated point. The method is reasonable in design, the ocean plumb line deviation observed value serves as basic data, the global gravity field spherical harmonic model is combined, the inverse distance weighted interpolation method based on the frequency domain characteristics is adopted, the high-precision and high-resolution sea area plumb line deviation model is constructed, and the method can be widely applied to the field of ocean surveying and mapping.
Owner:THE CHINESE PEOPLES LIBERATION ARMY 92859 TROOPS

Gravity modeling method and device based on inverse distance weighting method and quadric surface method

The invention relates to a gravity modeling method and device based on an inverse distance weighting method and a quadric surface method, computer equipment and a storage medium. The method comprises the following steps: acquiring gravity modeling data from a to-be-modeled area; carrying out gravity field modeling on the gravity field modeling data by adopting an inverse distance weighting method to obtain a preliminary gravity field model and an error sequence of the preliminary gravity field model; fitting modeling is conducted on the error sequence according to a quadric surface method, and an error model of the to-be-modeled area is obtained; and compensating the error of the preliminary gravity field model according to the error model of the to-be-modeled area to obtain an error-compensated gravity field model. The method can improve the precision of the gravity field model.
Owner:NAT UNIV OF DEFENSE TECH
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