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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:...
| Autores principales: | , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
MDPI
2022
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| 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 |