A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration

Because of the non-orthogonal configuration of multi-sensors, the redundant inertial navigation system (INS) has a more complex error model compared with the traditional orthogonal INS, and the complexity of sensors configuration also increases the difficulty of error separation. Based on sufficient...

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Main Authors: Chunfeng Gao, Guo Wei, Lin Wang, Qi Wang, Zhikun Liao
Format: Article
Language:English
Published: MDPI AG 2022-10-01
Series:Micromachines
Subjects:
Online Access:https://www.mdpi.com/2072-666X/13/10/1684
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author Chunfeng Gao
Guo Wei
Lin Wang
Qi Wang
Zhikun Liao
author_facet Chunfeng Gao
Guo Wei
Lin Wang
Qi Wang
Zhikun Liao
author_sort Chunfeng Gao
collection DOAJ
description Because of the non-orthogonal configuration of multi-sensors, the redundant inertial navigation system (INS) has a more complex error model compared with the traditional orthogonal INS, and the complexity of sensors configuration also increases the difficulty of error separation. Based on sufficient analysis of the error principle of redundant IMUs, a generalized high-accuracy calibration modeling method which is suitable for filtering method systematic calibration is summarized in this paper, and it has been applied to an RIMU prototype consisting of four ring laser gyros (RLGs) and four quartz accelerometers. Through the rotational excitation of the three-axis turntable in the laboratory, the high-precision filtering method systematic calibration of the RIMU is achieved, and static navigation and dynamic vehicle test experiments are also carried out. The experimental results reflect that the positioning accuracy can be obviously improved by using this new systematic calibration error model and the validity of this modeling method is also verified.
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spelling doaj.art-460b3053a28d4bd490e15cfec34972ff2023-11-24T01:22:43ZengMDPI AGMicromachines2072-666X2022-10-011310168410.3390/mi13101684A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal ConfigurationChunfeng Gao0Guo Wei1Lin Wang2Qi Wang3Zhikun Liao4Department of Optoelectronic Engineering, College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaDepartment of Optoelectronic Engineering, College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaDepartment of Optoelectronic Engineering, College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaDepartment of Optoelectronic Engineering, College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaDepartment of Optoelectronic Engineering, College of Advanced Interdisciplinary Studies, National University of Defense Technology, Changsha 410073, ChinaBecause of the non-orthogonal configuration of multi-sensors, the redundant inertial navigation system (INS) has a more complex error model compared with the traditional orthogonal INS, and the complexity of sensors configuration also increases the difficulty of error separation. Based on sufficient analysis of the error principle of redundant IMUs, a generalized high-accuracy calibration modeling method which is suitable for filtering method systematic calibration is summarized in this paper, and it has been applied to an RIMU prototype consisting of four ring laser gyros (RLGs) and four quartz accelerometers. Through the rotational excitation of the three-axis turntable in the laboratory, the high-precision filtering method systematic calibration of the RIMU is achieved, and static navigation and dynamic vehicle test experiments are also carried out. The experimental results reflect that the positioning accuracy can be obviously improved by using this new systematic calibration error model and the validity of this modeling method is also verified.https://www.mdpi.com/2072-666X/13/10/1684redundant sensorscalibrationinertial measurement unitring laser gyroscopesaccelerometersconstant bias
spellingShingle Chunfeng Gao
Guo Wei
Lin Wang
Qi Wang
Zhikun Liao
A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration
Micromachines
redundant sensors
calibration
inertial measurement unit
ring laser gyroscopes
accelerometers
constant bias
title A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration
title_full A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration
title_fullStr A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration
title_full_unstemmed A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration
title_short A Systematic Calibration Modeling Method for Redundant INS with Multi-Sensors Non-Orthogonal Configuration
title_sort systematic calibration modeling method for redundant ins with multi sensors non orthogonal configuration
topic redundant sensors
calibration
inertial measurement unit
ring laser gyroscopes
accelerometers
constant bias
url https://www.mdpi.com/2072-666X/13/10/1684
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