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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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Detalles Bibliográficos
Autores principales: Chang, Honglong, Jiao, Wenlong, Fu, Qianyan, Xie, Jianbing, Yuan, Weizheng
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Molecular Diversity Preservation International (MDPI) 2010
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC3274265/
https://www.ncbi.nlm.nih.gov/pubmed/22319346
http://dx.doi.org/10.3390/s100404130