Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution

Abstract This study investigates two fundamental challenges in the initial alignment of strapdown inertial navigation systems and presents creative solutions to overcome these challenges. The first challenge is to determine the settling time in different operating conditions such as stationary, quas...

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Main Authors: Hassan Jameian, Behrouz Safarinejadian
Format: Article
Language:English
Published: Wiley 2021-04-01
Series:IET Radar, Sonar & Navigation
Online Access:https://doi.org/10.1049/rsn2.12045
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spelling doaj-41843839fa09426ebc0f540d7c134c152021-08-02T08:26:00ZengWileyIET Radar, Sonar & Navigation1751-87841751-87922021-04-0115441943010.1049/rsn2.12045Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solutionHassan Jameian0Behrouz Safarinejadian1Faculty of Electrical and Electronic Engineering Shiraz University of Technology Shiraz IranFaculty of Electrical and Electronic Engineering Shiraz University of Technology Shiraz IranAbstract This study investigates two fundamental challenges in the initial alignment of strapdown inertial navigation systems and presents creative solutions to overcome these challenges. The first challenge is to determine the settling time in different operating conditions such as stationary, quasistationary, in‐motion, etc. The proposed solution to this challenge is to adjust the settling time of the initial alignment adaptively by evaluating the initial attitude matrix computed using the vector observations instead of allocating a fixed interval time for settling time. The second challenge is the existence of uncertainties in the vector observations, which adversely affect the initial alignment performance. The proposed solution to this challenge is to evaluate the quality of the vector observations used in the initial alignment by a real‐time algorithm. Appropriate weights are assigned to vector observations instead of allocating a uniform weight to all vectors, depending on the vector observation's quality. The capability and performance of the proposed solutions are evaluated using different experimental scenarios such as three‐axis rate table and vehicle tests.https://doi.org/10.1049/rsn2.12045
collection DOAJ
language English
format Article
sources DOAJ
author Hassan Jameian
Behrouz Safarinejadian
spellingShingle Hassan Jameian
Behrouz Safarinejadian
Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
IET Radar, Sonar & Navigation
author_facet Hassan Jameian
Behrouz Safarinejadian
author_sort Hassan Jameian
title Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
title_short Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
title_full Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
title_fullStr Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
title_full_unstemmed Overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
title_sort overcoming the settling time challenge of initial alignment of strapdown inertial navigation system by a novel solution
publisher Wiley
series IET Radar, Sonar & Navigation
issn 1751-8784
1751-8792
publishDate 2021-04-01
description Abstract This study investigates two fundamental challenges in the initial alignment of strapdown inertial navigation systems and presents creative solutions to overcome these challenges. The first challenge is to determine the settling time in different operating conditions such as stationary, quasistationary, in‐motion, etc. The proposed solution to this challenge is to adjust the settling time of the initial alignment adaptively by evaluating the initial attitude matrix computed using the vector observations instead of allocating a fixed interval time for settling time. The second challenge is the existence of uncertainties in the vector observations, which adversely affect the initial alignment performance. The proposed solution to this challenge is to evaluate the quality of the vector observations used in the initial alignment by a real‐time algorithm. Appropriate weights are assigned to vector observations instead of allocating a uniform weight to all vectors, depending on the vector observation's quality. The capability and performance of the proposed solutions are evaluated using different experimental scenarios such as three‐axis rate table and vehicle tests.
url https://doi.org/10.1049/rsn2.12045
work_keys_str_mv AT hassanjameian overcomingthesettlingtimechallengeofinitialalignmentofstrapdowninertialnavigationsystembyanovelsolution
AT behrouzsafarinejadian overcomingthesettlingtimechallengeofinitialalignmentofstrapdowninertialnavigationsystembyanovelsolution
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