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Off-line fusion method for redundant measurement signals of gravity gradient sensor of rotary accelerometer

A technology of rotational acceleration and gravity gradient, applied in the field of off-line fusion of redundant measurement signals of rotational accelerometer gravity gradient sensor, can solve the problem of low suppression ratio of irrelevant noise and achieve the effect of improving the suppression ratio

Active Publication Date: 2020-10-27
TIANJIN NAVIGATION INSTR RES INST
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Problems solved by technology

Through data comparison, it is considered that a large amount of noise in the two sets of gravity gradient measurement signals is irrelevant, and the traditional average fusion method has a low suppression ratio for uncorrelated noise. Therefore, it is necessary to establish an effective signal extraction method. The irrelevant noise in the signal is filtered out to improve the measurement accuracy of the gravity gradient signal

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  • Off-line fusion method for redundant measurement signals of gravity gradient sensor of rotary accelerometer
  • Off-line fusion method for redundant measurement signals of gravity gradient sensor of rotary accelerometer
  • Off-line fusion method for redundant measurement signals of gravity gradient sensor of rotary accelerometer

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Embodiment Construction

[0026] The present invention will be described in further detail below in conjunction with the drawings and specific examples. The following examples are only descriptive, not restrictive, and cannot limit the protection scope of the present invention.

[0027] A method for off-line fusion of redundant measurement signals of rotational accelerometer gravity gradient sensor, see figure 2 , the method calculates the Fourier transform of two sets of measurement signals through off-line processing, compares the phase angle difference of the two signals at the same frequency with the preset threshold, and if it is less than the threshold, the signal at the frequency point is retained. If it is greater than the threshold, the signal at this frequency point is discarded, and finally the final output result of the gravity gradient sensor measurement signal is obtained by inverse Fourier transform. The specific steps are:

[0028] Step 1. Define the two sets of signals simultaneously ...

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Abstract

The invention relates to an off-line fusion method for redundant measurement signals of a gravity gradient sensor of a rotary accelerometer. The method comprises the steps: calculating Fourier transform of two groups of measurement signals through an offline processing method; comparing the phase angle difference of the two signals at the same frequency with a preset threshold value, if the phaseangle difference is smaller than the threshold value, reserving the signal at the frequency point, and if the phase angle difference is larger than the threshold value, abandoning the signal at the frequency point; and finally, obtaining a final output result of the gravity gradient sensor measurement signal through inverse Fourier transform. Compared with conventional smooth filtering, the methodhas the advantages that the rejection ratio of irrelevant noise can be effectively increased, and the requirement for high-precision gravity gradient measurement is met; and according to the method,under the condition that the original precision of the gravity gradient measurement signals is low, the fusion method can be matched with the noise conditions of the two groups of measurement signalsin a threshold value adjusting mode so as to obtain the optimal gravity gradient signal.

Description

technical field [0001] The invention belongs to the technical field of measurement signal processing of a gravity gradient sensor of a rotational accelerometer, and in particular relates to an off-line fusion method for redundant measurement signals of a gravity gradient sensor of a rotational accelerometer. Background technique [0002] Rotational accelerometer-type gravity gradiometer is an instrument for continuous measurement of micro-gravity gradient changes on the earth's surface. like figure 1 As shown, the gravity gradient measurement component as the core sensor is based on the accelerometer position differential measurement principle, and modulates the gravity gradient tensor component to the double frequency of the system rotation frequency by mechanical rotation. The accelerometer output and the gravity gradient tensor The relationship between the components can be expressed as: [0003] (a 1 +a 3 )-(a 2 +a 4 )=2R(Γ xx -Γ yy )sin2ωt+4RΓ xy cos2ωt (1) ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01V7/06
CPCG01V7/06
Inventor 李达杨晔李中高巍李城锁
Owner TIANJIN NAVIGATION INSTR RES INST
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