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IMU error online calibration method based on factor graph

A calibration method and factor graph technology, applied in the field of integrated navigation, can solve the problems of adverse effects of high-precision navigation, single IMU device error, and affecting system accuracy

Active Publication Date: 2020-06-05
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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AI Technical Summary

Problems solved by technology

[0006] However, the disadvantage of method 1 is that the errors of the IMU due to the uncertainty of random startup and the errors of the calibration itself make the offline calibration results deviate from the errors when the IMU is actually used, which has a negative impact on real-time high-precision navigation; method 2 The disadvantage is that the consideration of the IMU device error is relatively simple. This method usually only calibrates the IMU error of the zero bias, and ignores the influence of the scale factor error and installation error on the navigation accuracy, so it will also affect the high precision. Navigation takes a toll
To sum up, the IMU error calibration method in the prior art has weak applicability, and cannot complete the online calibration of the IMU scale factor error and installation error, thus affecting the system accuracy

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  • IMU error online calibration method based on factor graph

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Embodiment Construction

[0114] In order to enable those skilled in the art to better understand the technical solutions of the present invention, the present invention will be further described in detail below in conjunction with specific embodiments.

[0115] An embodiment of the present invention provides an IMU (Inertial measurement unit inertial measurement unit) error online calibration method based on a factor graph, the process is as follows figure 1 shown, including:

[0116] Step 1: Acquire the measurements of the accelerometer and gyroscope in the inertial sensor

[0117] Step 2: Accelerometer Measurements and gyroscope measurements Pre-integrate propagation to the IMU.

[0118] 1) The error coefficient matrix of the accelerometer and gyroscope is calculated in the following form:

[0119]

[0120]

[0121] Among them, M a1 , M a2 , M a3 Represent the error coefficients of the X, Y, and Z axes of the accelerometer, M ω1 , M ω2 , M ω3 represent the error coefficients of...

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Abstract

The invention discloses an IMU error online calibration method based on a factor graph and relates to the field of combined navigation. According to the method, the scale factor error and the installation error of the IMU are modeled into a pre-integration model, and navigation information output by the IMU is fused with navigation information provided by other measurement sensors through an optimization theory based on a factor graph model. The error coefficient of the IMU can be obtained after optimization solution. Most traditional IMU error calibration methods are based on off-line calibration, and IMU errors are changed due to mechanical shock or other factors caused by carrier movement, so that the problem that the navigation precision is reduced is solved. The method can effectivelysolve the problem that the precision of the navigation system is reduced due to changes of IMU errors, and can be applied to various integrated navigation systems based on inertial navigation.

Description

technical field [0001] The invention relates to the field of integrated navigation, in particular to an IMU error online calibration method based on a factor graph. Background technique [0002] Due to its advantages of strong autonomy, good continuity and high stability, the integrated navigation system based on inertial navigation system has always been a research hotspot in the field of navigation technology. However, the inertial navigation system is essentially a dead reckoning system, and there is a problem of error accumulation over time. There are many error sources that affect the navigation accuracy, and the errors of the inertial device itself, such as: zero bias, scale factor error, installation error, etc., have a great impact on the navigation accuracy, and accurate calibration is required. [0003] In order to obtain various error coefficients of the IMU (Inertial measurement unit inertial measurement unit), there are currently two main methods: [0004] Met...

Claims

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Application Information

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IPC IPC(8): G01C25/00
CPCG01C25/005
Inventor 王炳清赖际舟余晓华吕品杨子寒
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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