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[1]程 诚,林庆国,张志远.超导磁悬浮储能及姿控飞轮的永磁结构仿真[J].火箭推进,2019,45(01):36-41.
 CHENG Cheng,LIN Qingguo,ZHANG Zhiyuan.Simulation design of permanent magnetic structure in a HTS maglev energy storage and attitude control flywheel[J].Journal of Rocket Propulsion,2019,45(01):36-41.
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超导磁悬浮储能及姿控飞轮的永磁结构仿真

参考文献/References:

[1] 苏瑞丰,张科科,宋海伟.甚小型卫星发展综述[J].航天器工程,2013(6):104-111.
[2] 吴汉基,蒋远大,张志远,等.微小卫星的在轨推进技术[J].火箭推进,2006,32(3):40-43.
WU H J, JIANG Y D, ZHANG Z Y,et al.On-board propulsion technologies for micro/minisatellites[J].Journal of Rocket Propulsion,2006,32(3):40-43.
[3] PECZALSKI A, ELGERSMA M, DAN Q, et al.Micro-wheels for attitude control and energy storage in small satellites[J].IEEE Proceedings,2001,38(5):2483-2492.
[4] JANSEN R, DEVER T.G2 flywheel module design:AIAA2004-5603[R].[S.L.]:AIAA,2004.
[5] 韩邦成,房建成,吴一辉.单轴飞轮储能/姿态控制系统的仿真研究[J].系统仿真学报,2006,18(9):2511-2515.
[6] 白越,吴一辉,韩邦成.飞轮单轴姿态控制及储能系统[J].光学精密工程,2008,16(8):1446-1451.
[7] 程千兵,武俊峰,吴一辉,等.超导磁悬浮微飞轮系统设计与测试[J].低温物理学报,2011(6):422-426.
[8] 贾英宏,徐世杰.利用飞轮的航天器姿态跟踪与能量存储(英文)[J].航空学报,2005,18(1):1-7.
[9] 冯香枝.卫星储能/姿控两用飞轮在能量回馈状态下的姿态控制问题研究[D].上海:东华大学,2005.
[10] LEE E.A HTS/magnet flywheels with dual function of energy storage and attitude control[C]//International Energy Conversion Engineering Conference.Pasadena: California:[s.n.],2003.
[11] HONG Z, CAMPBELL A M, COOMBS T A.Numerical solution of critical state in superconductivity by finite element software[J].Superconductor Science & Technology, 2006, 19(12): 1246-1252.

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备注/Memo

收稿日期:2017-03-18
基金项目:上海市空间发动机工程技术研究中心资助项目(17DI2280800)
作者简介:程 诚(1987—),男,博士,研究领域为空间推进技术

更新日期/Last Update: 2019-02-20