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Design and Simulation of a MEMS Control Moment Gyroscope for the Sub-Kilogram Spacecraft
A novel design of a microelectromechanical systems (MEMS) control moment gyroscope (MCMG) was proposed in this paper in order to generate a torque output with a magnitude of 10(−6) N·m. The MCMG consists of two orthogonal angular vibration systems, i.e., the rotor and gimbal; the coupling between wh...
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| Main Authors: | , , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Molecular Diversity Preservation International (MDPI)
2010
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| Assuntos: | |
| Acesso em linha: | https://ncbi.nlm.nih.gov/pmc/articles/PMC3274265/ https://ncbi.nlm.nih.gov/pubmed/22319346 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.3390/s100404130 |
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