A General Euler Angle Error Model of Strapdown Inertial Navigation Systems

Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. M...
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Autor*in:	Jianli Li [verfasserIn] Pengfei Dang [verfasserIn] Yiqi Li [verfasserIn] Bin Gu [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2018

Schlagwörter:	attitude error model navigation error propagation relative Euler angle error convected Euler angle error

Übergeordnetes Werk:	In: Applied Sciences - MDPI AG, 2012, 8(2018), 1, p 74
Übergeordnetes Werk:	volume:8 ; year:2018 ; number:1, p 74

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DOI / URN:	10.3390/app8010074

Katalog-ID:	DOAJ053512413

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520			\|a Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model.
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spelling	10.3390/app8010074 doi (DE-627)DOAJ053512413 (DE-599)DOAJ6adc2abc150f42d19d7f269f71f7c869 DE-627 ger DE-627 rakwb eng TA1-2040 QH301-705.5 QC1-999 QD1-999 Jianli Li verfasserin aut A General Euler Angle Error Model of Strapdown Inertial Navigation Systems 2018 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model. attitude error model navigation error propagation relative Euler angle error convected Euler angle error Technology T Engineering (General). Civil engineering (General) Biology (General) Physics Chemistry Pengfei Dang verfasserin aut Yiqi Li verfasserin aut Bin Gu verfasserin aut In Applied Sciences MDPI AG, 2012 8(2018), 1, p 74 (DE-627)737287640 (DE-600)2704225-X 20763417 nnns volume:8 year:2018 number:1, p 74 https://doi.org/10.3390/app8010074 kostenfrei https://doaj.org/article/6adc2abc150f42d19d7f269f71f7c869 kostenfrei http://www.mdpi.com/2076-3417/8/1/74 kostenfrei https://doaj.org/toc/2076-3417 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2018 1, p 74
allfields_unstemmed	10.3390/app8010074 doi (DE-627)DOAJ053512413 (DE-599)DOAJ6adc2abc150f42d19d7f269f71f7c869 DE-627 ger DE-627 rakwb eng TA1-2040 QH301-705.5 QC1-999 QD1-999 Jianli Li verfasserin aut A General Euler Angle Error Model of Strapdown Inertial Navigation Systems 2018 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model. attitude error model navigation error propagation relative Euler angle error convected Euler angle error Technology T Engineering (General). Civil engineering (General) Biology (General) Physics Chemistry Pengfei Dang verfasserin aut Yiqi Li verfasserin aut Bin Gu verfasserin aut In Applied Sciences MDPI AG, 2012 8(2018), 1, p 74 (DE-627)737287640 (DE-600)2704225-X 20763417 nnns volume:8 year:2018 number:1, p 74 https://doi.org/10.3390/app8010074 kostenfrei https://doaj.org/article/6adc2abc150f42d19d7f269f71f7c869 kostenfrei http://www.mdpi.com/2076-3417/8/1/74 kostenfrei https://doaj.org/toc/2076-3417 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2018 1, p 74
allfieldsGer	10.3390/app8010074 doi (DE-627)DOAJ053512413 (DE-599)DOAJ6adc2abc150f42d19d7f269f71f7c869 DE-627 ger DE-627 rakwb eng TA1-2040 QH301-705.5 QC1-999 QD1-999 Jianli Li verfasserin aut A General Euler Angle Error Model of Strapdown Inertial Navigation Systems 2018 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model. attitude error model navigation error propagation relative Euler angle error convected Euler angle error Technology T Engineering (General). Civil engineering (General) Biology (General) Physics Chemistry Pengfei Dang verfasserin aut Yiqi Li verfasserin aut Bin Gu verfasserin aut In Applied Sciences MDPI AG, 2012 8(2018), 1, p 74 (DE-627)737287640 (DE-600)2704225-X 20763417 nnns volume:8 year:2018 number:1, p 74 https://doi.org/10.3390/app8010074 kostenfrei https://doaj.org/article/6adc2abc150f42d19d7f269f71f7c869 kostenfrei http://www.mdpi.com/2076-3417/8/1/74 kostenfrei https://doaj.org/toc/2076-3417 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2018 1, p 74
allfieldsSound	10.3390/app8010074 doi (DE-627)DOAJ053512413 (DE-599)DOAJ6adc2abc150f42d19d7f269f71f7c869 DE-627 ger DE-627 rakwb eng TA1-2040 QH301-705.5 QC1-999 QD1-999 Jianli Li verfasserin aut A General Euler Angle Error Model of Strapdown Inertial Navigation Systems 2018 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model. attitude error model navigation error propagation relative Euler angle error convected Euler angle error Technology T Engineering (General). Civil engineering (General) Biology (General) Physics Chemistry Pengfei Dang verfasserin aut Yiqi Li verfasserin aut Bin Gu verfasserin aut In Applied Sciences MDPI AG, 2012 8(2018), 1, p 74 (DE-627)737287640 (DE-600)2704225-X 20763417 nnns volume:8 year:2018 number:1, p 74 https://doi.org/10.3390/app8010074 kostenfrei https://doaj.org/article/6adc2abc150f42d19d7f269f71f7c869 kostenfrei http://www.mdpi.com/2076-3417/8/1/74 kostenfrei https://doaj.org/toc/2076-3417 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2055 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 8 2018 1, p 74
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topic_facet	attitude error model navigation error propagation relative Euler angle error convected Euler angle error Technology T Engineering (General). Civil engineering (General) Biology (General) Physics Chemistry
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callnumber-first	T - Technology
author	Jianli Li
spellingShingle	Jianli Li misc TA1-2040 misc QH301-705.5 misc QC1-999 misc QD1-999 misc attitude error model misc navigation error propagation misc relative Euler angle error misc convected Euler angle error misc Technology misc T misc Engineering (General). Civil engineering (General) misc Biology (General) misc Physics misc Chemistry A General Euler Angle Error Model of Strapdown Inertial Navigation Systems
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topic_title	TA1-2040 QH301-705.5 QC1-999 QD1-999 A General Euler Angle Error Model of Strapdown Inertial Navigation Systems attitude error model navigation error propagation relative Euler angle error convected Euler angle error
topic	misc TA1-2040 misc QH301-705.5 misc QC1-999 misc QD1-999 misc attitude error model misc navigation error propagation misc relative Euler angle error misc convected Euler angle error misc Technology misc T misc Engineering (General). Civil engineering (General) misc Biology (General) misc Physics misc Chemistry
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title	A General Euler Angle Error Model of Strapdown Inertial Navigation Systems
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title_full	A General Euler Angle Error Model of Strapdown Inertial Navigation Systems
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title_sort	general euler angle error model of strapdown inertial navigation systems
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title_auth	A General Euler Angle Error Model of Strapdown Inertial Navigation Systems
abstract	Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model.
abstractGer	Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model.
abstract_unstemmed	Attitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model.
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container_issue	1, p 74
title_short	A General Euler Angle Error Model of Strapdown Inertial Navigation Systems
url	https://doi.org/10.3390/app8010074 https://doaj.org/article/6adc2abc150f42d19d7f269f71f7c869 http://www.mdpi.com/2076-3417/8/1/74 https://doaj.org/toc/2076-3417
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A General Euler Angle Error Model of Strapdown Inertial Navigation Systems

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