Avionics and Autocontrol

Research on Analysis and Compensation Method of Remnant Magnetic Moment for Magnetically Suspended Reaction Flywheel

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  • School of Instrument Science and Opto-electronics Engineering, Beihang University, Beijing 100191, China

Received date: 2010-08-25

  Revised date: 2010-10-13

  Online published: 2011-05-19

Abstract

To analyze and minimally design the remnant magnetic moment (RMM) for a magnetically suspended reaction flywheel, a method based on the equivalent magnetic dipole model is proposed. Firstly, the space magnetic field distribution can be achieved by finite element analysis, and then through selecting the magnetic field distribution of three feature planes, the RMM can be derived. The values and range of the RMM of a prototype are investigated in different operation situations. Based on the above analysis, an optimal design and magnetic compensation method for reducing the RMM is proposed. The analytical results show that the RMM can be effectively reduced to a certain range by a magnetic symmetric design of the magnetic bearings and compensation with a permanent magnet. The experimental results of a prototype demonstrate the validity of the analysis and compensation method.

Cite this article

LE Yun, FANG Jiancheng, TANG Jiqiang, WANG Xi . Research on Analysis and Compensation Method of Remnant Magnetic Moment for Magnetically Suspended Reaction Flywheel[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011 , 32(5) : 881 -890 . DOI: CNKI:11-1929/V.20110504.1117.001

References

[1] 黄本诚, 马有礼. 航天器空间环境试验技术[M]. 北京: 国防工业出版社, 2002. Huang Bencheng, Ma Youli. Space environment test technology of spacecraft[M]. Beijing: National Defense Industry Press, 2002. (in Chinese)

[2] 黄琳, 荆武兴. 关于剩磁对卫星姿态确定与控制影响的研究[J]. 航空学报, 2006, 27(3): 390-394. Huang Lin, Jing Wuxing. Effects of remanence on attitude determination and control of satellite[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(3): 390-394. (in Chinese)

[3] Shrivastava S K, Modi V J. Satellite attitude dynamics and control in the presence of environmental torques—a brief survey[J]. Journal of Guidance, Control, and Dynamics, 1983, 6(6): 461-471.

[4] Yasushi H, Masao I, Norio S, et al. Development of magnetic bearing momentum wheel for ultra-precision spacecraft attitude control//Proceedings of the 7th International Symposium on Magnetic Bearings. 2000: 525-530.

[5] Usiskin C, Wilkes R. Measuring the magnetic dipole of a satellite//Proceedings of the Sixth Symposium on Ballistic Missile and Space Technology. 1961: 336-340.

[6] Roy T N. Spacecraft magnetic field modeling[J]. IEEE Transactions on Magnetics, 1977, 13(1): 914-919.

[7] Ausserlechner U, Steiner W, Kasperkovitz P. Vector measurement of the magnetic dipole moment by means of a vibrating sample magnetometer[J]. IEEE Transactions on Magnetics, 1977, 30(2): 1061-1063.

[8] Moskowitz R, Lynch R. Magnetostatic measurement of spacecraft magnetic dipole moment[J]. IEEE Transactions on Aerospace, 1964, 2(2): 412-419.

[9] 易忠. 卫星磁性仿真模型建立[J]. 航天器环境工程, 2004, 21(2): 8-16. Yi Zhong. The model of satellite magnetic simulation[J]. Spacecraft Environment Engineering, 2004, 21(2): 8-16. (in Chinese)

[10] Steyn W H, Hashida Y. In-orbit attitude performance of the 3-axis stabilized SNAP-1 nanosatellite. Proceedings of the 15th AIAA/USU Conference on Small Satellites. 2001: 1-10.

[11] Huang L, Jing W X. Correction of remanent disturbance torque//Proceedings of 1st International Symposium on Systems and Control in Aerospace and Astronautics. 2006:164-168.

[12] 易忠. 中低轨道卫星的磁补偿[J]. 航天器环境工程, 1997, 14(4): 31-37. Yi Zhong. Magnetic compensation of middle and low orbit satellite[J]. Spacecraft Environment Engineering, 1997, 14(4): 31-37. (in Chinese)

[13] 刘虎, 房建成. 新型永磁偏置轴向磁轴承的磁力特性[J]. 机械工程学报, 2010, 46(8): 167-174. Liu Hu, Fang Jiancheng. Magnetic force characteristics of a novel permanent magnet biased axial magnetic bearing[J]. Journal of Mechanical Engineering, 2010, 46(8): 167-174. (in Chinese)

[14] 齐燕文. 卫星磁试验设备和磁试验技术[J]. 航天器环境工程, 1998(2): 29-39. Qi Yanwen. The facility and method of magnetic test for satellite[J]. Spacecraft Environment Engineering, 1998(2): 29-39. (in Chinese)

[15] Korepanov V, Dudkin F, Melnik O, et al. Small satellites EMC study[J]. Advances in Space Research, 2001, 28(1): 221-225.

[16] Stern T G. Techniques for magnetic cleanliness on spacecraft solar arrays//Proceedings of the 2nd International Energy Conversion Engineering Conference. 2004.

[17] 肖琦, 史尧宜, 易忠, 等. 某型号卫星磁性分析与控制[J]. 航天器环境工程, 2009, 26(S1): 34-37. Xiao Qi, Shi Yaoyi, Yi Zhong, et al. Analysis and control of magnetic properties for satellite[J]. Spacecraft Environment Engineering, 2009, 26(S1): 34-37. (in Chinese)

[18] 齐燕文. 磁净化卫星的磁场控制方法[J]. 航天器环境工程, 2000, 17(3): 18-25. Qi Yanwen. The magnetic field control method of magnetic clean satellite[J]. Spacecraft Environment Engineering, 2000, 17(3): 18-25. (in Chinese)

[19] 李荣福. 地磁场中卫星磁测试环境与设备[J]. 航天器环境工程, 2008, 25(1): 72-79. Li Rongfu. Satellite magnetism tests for environment and equipments in geomagnetism[J]. Spacecraft Environment Engineering, 2008, 25(1): 72-79. (in Chinese)

[20] Harris P K. Near-field magnetic dipole moment analysis. NASA Technical Report, 2003.
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