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基于FPGA的磁悬浮飞轮用自修复磁轴承控制器的设计 被引量:4

Design of FPGA-based self-repairing AMB controller for MSFW
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摘要 磁悬浮飞轮是对卫星等航天器进行高精度姿态控制的执行机构,为了提高空间用磁悬浮飞轮控制系统的可靠性和灵活性,对基于FPGA的磁轴承数字控制器进行研究。首先,对磁轴承系统进行建模,并选择合适的控制策略;利用片上软硬件协同设计的思想,提出了一种基于FPGA和LEON3处理器软核的磁轴承数字控制器。然后,搭建了实验系统测试系统的实际性能。最后,提出了一种基于FPGA的自修复磁轴承控制器。基于FPGA的磁轴承控制器相对基于DSP+FPGA的控制器失效率降低了10%,控制板面积减小30%。实验结果表明,在基于FPGA的磁轴承控制器控制下,在磁悬浮飞轮工作转速范围内,飞轮转子跳动量<20μm,力矩输出误差<4×10-3N.m,正反转不一致性<10%,达到了较高的控制精度。 Magnetically Suspended Flywheel (MSFW) is an actuator for the high precision attitude control of spacecrafts such as satellites.In order to improve the reliability and flexibility of a MSFW control system for space applications,a FPGA-based digital controller for Active Magnetic Bearing (AMB) is investigated. Firstly, the model of the magnetic bearing system is set up and several kinds of suitable control strategies are chosen. Then, by using the idea of on-chip hardware and software co-design, an AMB controller based on a FPGA and a LEON3 soft processor is presented,and a prototyping platform is built to test control algorithms and to verify the system performance. Finally, a self-repairing FPGA-based AMB controller is proposed. Comparing with the DSP-FPGA-based AMB controller, the FPGA-based controller has decreased the failure rate by 10% and the board area by 30%. Experimental results indicate that the beating of flywheel rotor and the torque output error are less than 20 μm and 4×10-3N·m,respectively, and the inconsistency between positive and inversion is less than 10% under the control of the FPGA-based AMB controller and the working speed scope of MSFW.These data prove that the proposed controller has achieved a higher precision.
作者 刘刚 潘明健
出处 《光学精密工程》 EI CAS CSCD 北大核心 2009年第11期2762-2770,共9页 Optics and Precision Engineering
基金 国家973重点基础研究发展规划资助项目(No.2009CB724001) 国家863高技术研究发展计划资助项目(No.2008AA12A200)
关键词 磁悬浮飞轮 主动磁轴承 现场可编程门阵列 软处理器核 自修复 Magnetically Suspended Flywheel(MSFW) active magnetic bearing Field Pragramm Gate Array(FPGA) soft processor self-repairing
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参考文献11

  • 1任建伟,万志,李宪圣,任建岳.空间光学遥感器的辐射传递特性与校正方法[J].光学精密工程,2007,15(8):1186-1190. 被引量:36
  • 2史光辉.卫星对地观测高分辨率光学系统和设计问题[J].光学精密工程,1999,7(1):16-34. 被引量:33
  • 3高云国.现代小卫星及其相关技术[J].光学精密工程,1999,7(5):16-21. 被引量:15
  • 4KRACH F, FRACKELTON B, CARLETTA J, et al.. FPGA based implementation of digital control for magnetic bearings[C]. IEEE Proc. Of the American Control Conference ,2003 :1080-1085.
  • 5JASTRZEBSKI R, POLLANEN R, PYRHONEN O. Analysis of system architecture of FPGA based embedded controller for magneti-cally suspended rotor[C]. IEEE Proceedings of the International Symposium on System-on-Chip ,2005:128-132.
  • 6FANG ZH W,CARI.ETTA J E,VEILLETTE R J. A methodology for FPGA based control implementation[J]. IEEE Transactions on Control Systems Technology, 2005,13(6) :977-987.
  • 7ZHURAVLYOV Y N. n LQ-Control of Magnetic Bearing[J]. IEEE Transactions on Control Systems Technology, 2000,8(2) : 344-350.
  • 8DUZELLIER S. Radiation effects of electronic devices in space [J]. Aerospace and Technology, 2004(9) :93-99.
  • 9LAPLANTE P H. Computing requirements of self-repairing space systems[J]. Journal of Aerospace Computing, Information, and Communication, 2005(2) :154-168.
  • 10MATTHIAS D, CHRISTIAN P, MARCO P. Partially reconfigurable cores for xilinx virtex [C]. 12th International Conference on Field- Programmable Logic and Applications. Sokolova, 2002.

二级参考文献30

共引文献75

同被引文献37

  • 1房建成,杨磊,孙津济,韩邦成.一种新型磁悬浮飞轮用永磁偏置径向磁轴承[J].光学精密工程,2008,16(3):444-451. 被引量:18
  • 2龙亚文,谢振宇,徐欣.磁悬浮轴承H_∞鲁棒控制策略研究[J].振动与冲击,2013,32(23):115-120. 被引量:11
  • 3杨孟飞,郭树玲,孙增圻.航天器控制应用的星载计算机技术[J].航天控制,2005,23(2):69-73. 被引量:22
  • 4吴旭东,解学书.H_∞鲁棒控制中的加权阵选择[J].清华大学学报(自然科学版),1997,37(1):27-30. 被引量:145
  • 5FORSBERG H, BJUREUS P, SODERQUIST I, et al..Next generation COTS-commercial IP blocks in avionics .Digital Avionics Systems Conference, 2004,2:8.A.1-81-12.
  • 6SHIBAYAMA N, AKAZAWA N,KOYAMA M, et al..Space verification of on-board computer integrated with commercial IC[J].Mitsubishi Heavy Industry.Ltd.Technical Review, 2005, 42(5):1-5.
  • 7RICHARD E,ALLEN V, BAUER T, et al..Responsive, low-cost access to space with ELVIS an expendable launch vehicle with integrated spacecraft .Annual USU/AIAA Small Satellite Conference, 2003.
  • 8MONTENEQRO S,ROSER H P,HUBER F.BOSS: software and FPGA middlemware for the "flying laptop" micro satellite .Proceedings of DASIA, 2005, 401-405.
  • 9任小西.基于可重构计算的高可靠性星载计算机体系结构研究 .长沙:湖南大学,2007.
  • 10陶涛,刁小燕,张维煌,等.基于DRFNN逆的交流主动磁轴承解耦控制[C].第31届中国控制大会,合肥,2012,7:4628-4633.

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