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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...

पूर्ण विवरण

में बचाया:
ग्रंथसूची विवरण
मुख्य लेखकों: Chang, Honglong, Jiao, Wenlong, Fu, Qianyan, Xie, Jianbing, Yuan, Weizheng
स्वरूप: Artigo
भाषा:Inglês
प्रकाशित: Molecular Diversity Preservation International (MDPI) 2010
विषय:
ऑनलाइन पहुंच: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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