Abstract

<jats:p>Analysis and simulation of the Strapdown Inertial Navigation System (SINS) error genesis revealed that the East Feedback Contour has the greatest influence on the development of an error in this model, and angular velocity sensor Δω𝒚 is the critical element. In order to prevent the development of an error, structural correction in the East Feedback Contour, and elements that are more critical, namely in angular velocity measurement sensors is the best option.

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The different versions of the original document can be found in:

https://doaj.org/toc/2255-9876 under the license cc-by-nc-nd
http://www.degruyter.com/view/j/tae.2018.6.issue-1/tae-2018-0006/tae-2018-0006.pdf,
http://dx.doi.org/10.2478/tae-2018-0006
https://academic.microsoft.com/#/detail/2899437540 under the license http://creativecommons.org/licenses/by/4.0
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Published on 01/01/2018

Volume 2018, 2018
DOI: 10.2478/tae-2018-0006
Licence: Other

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