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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Formato: | article |
Lenguaje: | EN RU UK |
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National Aerospace University «Kharkiv Aviation Institute»
2021
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Materias: | |
Acceso en línea: | https://doaj.org/article/d7928c13be4d42c3ba39c32b68d8fbb9 |
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