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Equations of Disturbed Motion of the Moving Part of the Gyroscope Suspension

The response of the float two-stage angular velocity sensor to the simultaneous perturbation from the rocket body—kinematic perturbation—and the penetrating acoustic radiation from the propulsion engines of the launch vehicle were determined. The solution of two equations was successively analyzed:...

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Detalles Bibliográficos
Autores principales: Korobiichuk, Igor, Mel’nick, Viktorij, Kosova, Vera, Maksymenko, Kateryna
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2022
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9571700/
https://www.ncbi.nlm.nih.gov/pubmed/36236540
http://dx.doi.org/10.3390/s22197442

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