所属单位：北京航空航天大学
教研室：仪器科学与光电工程学院
发表刊物：IEEE Transactions on Industrial Electronics
项目来源：中国国家自然科学基金， 项目号: 61203203, 61421063
关键字：Control moment gyro, gimbal servo system, hybrid magnetic bearing, magnetically suspended control
摘要：A successful application of the single-gimbal magnetically suspended control moment gyro (SGMSCMG) requires careful attention not only to the electromagnetic design and feedback control design aspects of the magnetic bearing (MB) but also to the decoupling control aspects between the high-speed MB rotor system and the low-speed gimbal servo system. The key parts with low loss of a large-scale SGMSCMG for the large spacecraft application are proposed. The low-loss MBs that consist of the thrust and radial active MBs with PM bias are proposed for themagnetically suspended controlmoment gyro.
备注：SCI, WOS: 000365019500013; EI, Accession Number: 20154901633523
合写作者：Yun Le,王卓, Shiqiang Zheng,Bangcheng Han*
论文类型：应用研究
文献类型：期刊
是否译文：否
发表时间：2015-12-07