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Multi-sensor multi-target space-time deviation calibration and fusion method

A multi-sensor, fusion method technology, applied in the direction of instruments, radio wave reflection/re-radiation, utilization of re-radiation, etc., can solve the problem of not performing deviation compensation and fusion at the same time

Active Publication Date: 2021-01-29
HARBIN INST OF TECH
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  • Description
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Problems solved by technology

Existing sequential processing methods only estimate the sensor spatial bias without simultaneously performing bias compensation and fusion
In addition, these methods all assume that there is no time bias in the sensor

Method used

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Embodiment Construction

[0101] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0102] The embodiment of the present invention provides a multi-sensor multi-target space-time deviation calibration and fusion method. The present invention considers the scene where S sensors track N targets in the area. The sampling periods of the multi-sensors are different, and the sensors are provided in the polar coordinate system Dist...

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Abstract

The invention relates to a multi-sensor multi-target space-time deviation calibration and fusion method and a computer readable storage medium. The method comprises the steps: calculating dimension expansion state prediction and dimension expansion state prediction covariance of a target i at the k moment and dimension expansion observation prediction of a sensor s on the target i; defining a mapping p = p (m) for indicating the number of a corresponding target; calculating a cross covariance between the dimension expansion state estimation error of the target i and the dimension expansion state estimation error of the target p (m) at the moment k when m is equal to i + 1,..., i + N1 by adopting a recursive processing strategy; calculating a cross covariance between the dimension expansionstate prediction and the dimension expansion observation prediction and an auto-covariance of the dimension expansion observation prediction; and updating the dimension expansion state estimation andthe dimension expansion state estimation covariance of the target i at the moment k. According to the invention, sequential processing strategies are executed among different targets and different sensors at the same moment, so that the precision of multi-sensor space-time deviation estimation is improved while sequential estimation of each target state is realized.

Description

technical field [0001] The invention relates to the technical field of space target tracking, in particular to a multi-sensor multi-target space-time deviation calibration and fusion method and a computer-readable storage medium. Background technique [0002] Currently, in multi-sensor multi-target tracking systems, the collaborative fusion of data collected from multiple sensors improves the overall system performance. The prerequisite for accurate fusion is to estimate and compensate the space-time deviation in the asynchronous multi-sensor system, otherwise, the space-time deviation may lead to the degradation of the tracking performance of the system, and in severe cases, it will generate repeated tracks. [0003] For the problem of spatial deviation estimation and compensation, existing solutions include real-time quality control method, least square method and maximum likelihood registration method, etc. In addition, some scholars have proposed methods based on Kalman...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01S13/72
CPCG01S13/726
Inventor 周共健卜石哲
Owner HARBIN INST OF TECH
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