Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters

Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters

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Bibliographic Details
Date:2018
Main Authors: N. V. Efimenko, N. V. Lutsenko
Format: Article
Language:English
Published: 2018
Series:International Scientific Technical Journal «Problems of Control and Informatics»
Online Access:http://jnas.nbuv.gov.ua/article/UJRN-0001246431
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Journal Title:Library portal of National Academy of Sciences of Ukraine | LibNAS

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Library portal of National Academy of Sciences of Ukraine | LibNAS
id open-sciencenbuvgovua-35208
record_format dspace
spelling open-sciencenbuvgovua-352082024-02-27T22:19:58Z Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters N. V. Efimenko N. V. Lutsenko 2786-6491 2018 en International Scientific Technical Journal «Problems of Control and Informatics» http://jnas.nbuv.gov.ua/article/UJRN-0001246431 Article
institution Library portal of National Academy of Sciences of Ukraine | LibNAS
collection Open-Science
language English
series International Scientific Technical Journal «Problems of Control and Informatics»
spellingShingle International Scientific Technical Journal «Problems of Control and Informatics»
N. V. Efimenko
N. V. Lutsenko
Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
format Article
author N. V. Efimenko
N. V. Lutsenko
author_facet N. V. Efimenko
N. V. Lutsenko
author_sort N. V. Efimenko
title Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
title_short Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
title_full Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
title_fullStr Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
title_full_unstemmed Determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the Rodrig–Hamilton parameters
title_sort determination of the parameters of the angular motion of the spacecraft from the information of the star sensor using the dynamic equation of the solid body rotation in the rodrig–hamilton parameters
publishDate 2018
url http://jnas.nbuv.gov.ua/article/UJRN-0001246431
work_keys_str_mv AT nvefimenko determinationoftheparametersoftheangularmotionofthespacecraftfromtheinformationofthestarsensorusingthedynamicequationofthesolidbodyrotationintherodrighamiltonparameters
AT nvlutsenko determinationoftheparametersoftheangularmotionofthespacecraftfromtheinformationofthestarsensorusingthedynamicequationofthesolidbodyrotationintherodrighamiltonparameters
first_indexed 2025-07-17T17:49:02Z
last_indexed 2025-07-17T17:49:02Z
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