Estimation of the influence of errors of the SINS constructed on MEMS components on the accuracy of positioning a ultra-light class rocket

The object of the article is the movement of an ultra-light class liquid-propellant launch vehicle in near-earth space. The subject of the research is the accuracy of launching a spacecraft by a launch vehicle. The article studies the effect of errors in the instruments of a strap-down inertial navi...

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Autores principales: Артём Сергеевич Смирнов, Александр Вячеславович Голубек
Formato: article
Lenguaje:EN
RU
UK
Publicado: National Aerospace University «Kharkiv Aviation Institute» 2021
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Acceso en línea:https://doaj.org/article/d7928c13be4d42c3ba39c32b68d8fbb9
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