An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System

This paper develops an improved hybrid calibration scheme for the strapdown inertial navigation system (SINS) that combines the advantages of an optimal rotational norm calibration method and an improved system-level calibration method. To accurately determine the scale factors and misalignment erro...

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Main Authors: Suier Wang, Gongliu Yang, Lifen Wang
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8877775/
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spelling doaj-cbc889b789724592b2ff5547b3ecf1ab2021-03-29T23:19:06ZengIEEEIEEE Access2169-35362019-01-01715166915168110.1109/ACCESS.2019.29484988877775An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation SystemSuier Wang0https://orcid.org/0000-0001-7671-6847Gongliu Yang1Lifen Wang2https://orcid.org/0000-0002-1628-0284Instrumentation and Opto-Electronic Engineering, Beihang University, Beijing, ChinaInstrumentation and Opto-Electronic Engineering, Beihang University, Beijing, ChinaDepartment of Aerospace Science and Technology, Space Engineering University, Beijing, ChinaThis paper develops an improved hybrid calibration scheme for the strapdown inertial navigation system (SINS) that combines the advantages of an optimal rotational norm calibration method and an improved system-level calibration method. To accurately determine the scale factors and misalignment error of gyros triad, the optimal rotation norm calibration method is applied. Similarly, the improved system-level calibration method based on the 24-dimensional error state Kalman filter (ESKF) plays an important role in accelerometer calibration and gyro biases calibration. The clockwise and counterclockwise multi-cycles rotation scheme is designed to eliminate the effects of the Earth's rate and gyros biases, and then provide accurate rotational norm to completely determine the gyros triad scale factors and misalignment. In addition, the improved ESKF system-level calibration method is employed to estimate accelerometer parameters and gyros biases. Simulation test verify the validity of the proposed method, and the calibration experiences and the verification tests of the two high-precision optical gyros inertial measurement units (IMU) are carried out. For comparison, the traditional 30-dimensional system-level calibration is also performed. The attitude error of high maneuvering swing test indicate that the gyros calibration accuracy of hybrid calibration scheme is better than that of traditional system-level calibration scheme. Furthermore, the positioning error of pure inertial navigation solution in static and dynamic condition for two calibration methods indicate that the hybrid calibration scheme significantly improves the positioning accuracy, especially in the dynamic experiment, that is, the proposed scheme provides a more accurate calibration of the IMU.https://ieeexplore.ieee.org/document/8877775/Hybrid calibrationstrapdown inertial navigation systemoptimal rotation norm calibrationimproved system-level calibration
collection DOAJ
language English
format Article
sources DOAJ
author Suier Wang
Gongliu Yang
Lifen Wang
spellingShingle Suier Wang
Gongliu Yang
Lifen Wang
An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
IEEE Access
Hybrid calibration
strapdown inertial navigation system
optimal rotation norm calibration
improved system-level calibration
author_facet Suier Wang
Gongliu Yang
Lifen Wang
author_sort Suier Wang
title An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
title_short An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
title_full An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
title_fullStr An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
title_full_unstemmed An Improve Hybrid Calibration Scheme for Strapdown Inertial Navigation System
title_sort improve hybrid calibration scheme for strapdown inertial navigation system
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2019-01-01
description This paper develops an improved hybrid calibration scheme for the strapdown inertial navigation system (SINS) that combines the advantages of an optimal rotational norm calibration method and an improved system-level calibration method. To accurately determine the scale factors and misalignment error of gyros triad, the optimal rotation norm calibration method is applied. Similarly, the improved system-level calibration method based on the 24-dimensional error state Kalman filter (ESKF) plays an important role in accelerometer calibration and gyro biases calibration. The clockwise and counterclockwise multi-cycles rotation scheme is designed to eliminate the effects of the Earth's rate and gyros biases, and then provide accurate rotational norm to completely determine the gyros triad scale factors and misalignment. In addition, the improved ESKF system-level calibration method is employed to estimate accelerometer parameters and gyros biases. Simulation test verify the validity of the proposed method, and the calibration experiences and the verification tests of the two high-precision optical gyros inertial measurement units (IMU) are carried out. For comparison, the traditional 30-dimensional system-level calibration is also performed. The attitude error of high maneuvering swing test indicate that the gyros calibration accuracy of hybrid calibration scheme is better than that of traditional system-level calibration scheme. Furthermore, the positioning error of pure inertial navigation solution in static and dynamic condition for two calibration methods indicate that the hybrid calibration scheme significantly improves the positioning accuracy, especially in the dynamic experiment, that is, the proposed scheme provides a more accurate calibration of the IMU.
topic Hybrid calibration
strapdown inertial navigation system
optimal rotation norm calibration
improved system-level calibration
url https://ieeexplore.ieee.org/document/8877775/
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