A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS

In this paper, a modified generalized likelihood test (GLT) double faults isolation approach based on maximum likelihood estimation (MLE) and reduced-order parity vector (RPV) has been proposed. To improve the reliability of the strapdown inertial navigation system (SINS), redundant inertial sensors...

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Main Authors: Jianhua Cheng, Xiangyu Sun, Hongjie Mou
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
FI
GLT
MLE
RPV
KF
Online Access:https://ieeexplore.ieee.org/document/8585020/
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spelling doaj-294560c555414c6695a86898deedbd292021-03-29T22:06:57ZengIEEEIEEE Access2169-35362019-01-0175312533210.1109/ACCESS.2018.28890368585020A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINSJianhua Cheng0Xiangyu Sun1https://orcid.org/0000-0002-9982-1794Hongjie Mou2College of Automation, Harbin Engineering University, Harbin, ChinaCollege of Automation, Harbin Engineering University, Harbin, ChinaShandong Institute of Space Electronic Technology, Yantai, ChinaIn this paper, a modified generalized likelihood test (GLT) double faults isolation approach based on maximum likelihood estimation (MLE) and reduced-order parity vector (RPV) has been proposed. To improve the reliability of the strapdown inertial navigation system (SINS), redundant inertial sensors (gyros and accelerometers) are applied to SINS, which is called redundant SINS. The six-gyro SINS has been widely used because of its high reliability, low cost, and small volume. Using fault isolation, faulty sensors can be isolated when they are faulty in redundant SINS. The GLT double faults isolation approach based on MLE effectively isolates double faults due to its high sensitivity, small calculation, and easy implementation. However, this approach cannot correctly recognize detailed double faults in six-gyro SINS. Additionally, this approach cannot work during SINS motion. In this paper, first, based on MLE, double faults isolation function and faults isolation threshold are redesigned, and then, the application range of double faults isolation function is analyzed. Second, a modified RPV isolation approach is proposed to correctly recognize the detailed double faults. Third, the Kalman filter is employed to compensate the dynamic errors of sensors, making a new approach applicable to dynamic application. The simulation shows that the new approach is able to isolate double faults effectively for six-gyro SINS during SINS motion.https://ieeexplore.ieee.org/document/8585020/SINSFIGLTMLERPVKF
collection DOAJ
language English
format Article
sources DOAJ
author Jianhua Cheng
Xiangyu Sun
Hongjie Mou
spellingShingle Jianhua Cheng
Xiangyu Sun
Hongjie Mou
A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS
IEEE Access
SINS
FI
GLT
MLE
RPV
KF
author_facet Jianhua Cheng
Xiangyu Sun
Hongjie Mou
author_sort Jianhua Cheng
title A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS
title_short A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS
title_full A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS
title_fullStr A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS
title_full_unstemmed A Modified GLT Double Faults Isolation Approach Based on MLE and RPV for Six-Gyro Redundant SINS
title_sort modified glt double faults isolation approach based on mle and rpv for six-gyro redundant sins
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2019-01-01
description In this paper, a modified generalized likelihood test (GLT) double faults isolation approach based on maximum likelihood estimation (MLE) and reduced-order parity vector (RPV) has been proposed. To improve the reliability of the strapdown inertial navigation system (SINS), redundant inertial sensors (gyros and accelerometers) are applied to SINS, which is called redundant SINS. The six-gyro SINS has been widely used because of its high reliability, low cost, and small volume. Using fault isolation, faulty sensors can be isolated when they are faulty in redundant SINS. The GLT double faults isolation approach based on MLE effectively isolates double faults due to its high sensitivity, small calculation, and easy implementation. However, this approach cannot correctly recognize detailed double faults in six-gyro SINS. Additionally, this approach cannot work during SINS motion. In this paper, first, based on MLE, double faults isolation function and faults isolation threshold are redesigned, and then, the application range of double faults isolation function is analyzed. Second, a modified RPV isolation approach is proposed to correctly recognize the detailed double faults. Third, the Kalman filter is employed to compensate the dynamic errors of sensors, making a new approach applicable to dynamic application. The simulation shows that the new approach is able to isolate double faults effectively for six-gyro SINS during SINS motion.
topic SINS
FI
GLT
MLE
RPV
KF
url https://ieeexplore.ieee.org/document/8585020/
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