Micro/Nano Technology and Fine Mechanics Design of reaction flywheel systems for small satellites

WANG Hui; WU Jun-feng; LI Yin; WU Yi-hui

doi:10.3788/OPE.20142202.0331

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Micro/Nano Technology and Fine Mechanics Design of reaction flywheel systems for small satellites

Micro/Nano Technology and Fine Mechanics | 更新时间：2020-08-13

- Micro/Nano Technology and Fine Mechanics Design of reaction flywheel systems for small satellites
- Optics and Precision Engineering Vol. 22, Issue 2, Pages: 331-337(2014)
- 作者机构：
  
  1. 中国科学院大学北京,中国,100049
  2. 中国科学院长春光学精密机械与物理研究所应用光学国家重点实验室,吉林长春,130033
- 作者简介：
- 基金信息：
- DOI：10.3788/OPE.20142202.0331
  CLC： V448.222
- Received：21 July 2013，
  
  Published：20 February 2014
- 稿件说明：
移动端阅览
王辉,武俊峰,李胤等. 小卫星用反作用飞轮系统设计[J]. 光学精密工程, 2014,22(2): 331-337

WANG Hui, WU Jun-feng, LI Yin etc. Micro/Nano Technology and Fine Mechanics Design of reaction flywheel systems for small satellites[J]. Editorial Office of Optics and Precision Engineering, 2014,22(2): 331-337
王辉,武俊峰,李胤等. 小卫星用反作用飞轮系统设计[J]. 光学精密工程, 2014,22(2): 331-337 DOI： 10.3788/OPE.20142202.0331.

WANG Hui, WU Jun-feng, LI Yin etc. Micro/Nano Technology and Fine Mechanics Design of reaction flywheel systems for small satellites[J]. Editorial Office of Optics and Precision Engineering, 2014,22(2): 331-337 DOI： 10.3788/OPE.20142202.0331.

摘要

考虑小卫星用反作用飞轮系统小型化的要求

提出了飞轮电机体积最小时的电枢尺寸确定方法

并设计了一种定子无铁芯式反作用飞轮系统。为防止磁路饱和

将多学科优化设计方法应用于飞轮转子结构和电机磁场联合设计中

并采用外罚函数法及序列二次规划算法(SQP)组合优化策略对飞轮系统进行多目标优化设计。选取飞轮转子质量最小和电机气隙磁通密度最大为优化目标

以最大等效应力、一阶共振频率、极转动惯量、磁饱和等作为约束条件

将iSIGHT软件作为优化平台

集成有限元软件ANSYS实现了优化过程

最后依据优化结果制造出飞轮样机。优化结果表明

优化后飞轮转子质量由0.73 kg减小到0.67 kg

减小了8.22%

气隙磁通密度由0.376 T增大到0.401 T

增大了6.65%。设计的优化方法提高了飞轮设计的合理性

推动了飞轮系统的小型化研究。

Abstract

According to the requirement of reaction flywheels in small satellites for small sizes

the design method for an armature size was proposed when the electrical motor was at a minimal volume

and a stator coreless reaction flywheel system was designed based on the method. To avoid the magnetic saturation

the multidisciplinary design optimization method was applied to the design of flywheel rotor and magnetic field of the motor. A optimization strategy combined with Exterior Penalty(EP) function and Sequential Quadratic Programming(SQP) was proposed to optimize the system as well. With optimization

the minimum mass and maximum air-gap magnetic flux density of the rotor were chosen as the objects

respectively

and the maximum equivalent stress

resonance frequency

the polar moment of inertia and the magnetic saturation were taken as constrains. Then

the software iSIGHT with finite element analysis (ANSYS) were integrated to achieve the optimization. Finally

a flywheel prototype was designed based on the optimal results. The results indicate that the total mass of the flywheel rotor has been decreased from 0.73 kg to 0.67 kg (reduced by 8.22%) and the flux density has been increased from 0.376 T to 0.401 T (increased by 6.65%). The optimal design method can improve the rationality of flywheel design

and will promote the progress of the miniaturization investigation of flywheel systems.

关键词

Keywords

references

ISMAIL Z, VARATHARAJOO R. A study of reaction wheel congurations for a 3-axis satellite attitude control [J]. Advances in Space Research, 2010, 45(6): 750-759.

MOHAMMED S, BENYETTOU M, BENTOUTOU Y, et al.. Three-axis active control system for gravity gradient stabilized microsatellite [J]. Acta Astronaut, 2009, 64(8): 796-809.

武俊峰,吴一辉,安静,等.姿控飞轮变结构变速积分控制的实现[J].光学精密工程,2010,18(1): 149-155.

WU J F,WU Y H,AN J, et al.. Implementation of variable structure and speed-changed integration control for flywheels [J]. Opt. Precision Eng., 2010, 18(1): 149-155.(in Chinese)

唐任远.现代永磁电机理论与设计[M].北京:机械工业出版社,1997.

TANG R Y. Modern Permanent Magnet Machines Theory and Design [M]. Beijing: China Machine Press, 1997. (in Chinese)

邱国平,邱明.永磁直流电机实用设计及应用技术[M].北京:机械工业出版社,2009.

QIU G P, QIU M. Permanent Magnet DC Motor Practical Design and Application Technology [M]. Beijing: Machinery Industry Press, 2009.(in Chinese)

吴一辉,高庆嘉,白越.反作用飞轮驱动电机的电磁设计[J].光学精密工程,2010,18(6): 1317-1325.

WU Y H, GAO Q J, BAI Y. Electromagnetic design of driving motors in reaction wheels [J]. Opt.Precision Eng., 2010, 18(6): 1317-1325.(in Chinese)

刘强,房建成.磁悬浮飞轮用可重复抱式锁紧装置[J].光学精密工程,2012, 20(8): 1802-1810.

LIU Q, FANG J CH. Repeated clamping locking device for magnetic bearing flywheel [J]. Opt.Precision Eng., 2012, 20(8): 1802-1810. ( in Chinese)

汤继强,韩雪飞,刘强.微框架效应磁悬浮飞轮转子轮缘优化设计[J].光学精密工程,2012, 20(9): 1991-1998.

TANG J Q,HAN X F,LIU Q. Optimal design of rotor rim for magnetically suspended flywheel with vernier gimballing capacity [J]. Opt. Precision Eng., 2012, 20(9): 1991-1998.(in Chinese)

韩邦成,袁倩.大型磁悬浮CMG转子的组合优化策略[J].宇航学报, 2012, 33(2): 275-280.

HAN B CH, YUAN Q. The combinatorial optimization strategy for large-sized magnetic suspension rotor in CMG system [J]. Journal of Astronautics, 2012, 33(2): 275-280. ( in Chinese)

叶全红,李红,韩邦成.基于iSIGHT的磁悬浮反作用飞轮优化设计[J].宇航学报, 2007, 28(6): 1619-1623.

YE Q H, LI H, HAN B CH. Optimization design of magnetic bearing reaction wheel rotor using iSIGHT software [J]. Journal of Astronautics, 2007, 28(6):1619-1623. ( in Chinese)

MANDI M. An optimal two-dimensional eometry of flywheel for kinetic energy storage [J]. Int. J. of Thermal & Environmental Engineering, 2011, 3(2): 67-72.

SUNG K, SEONG J, SANA U, et al.. Design optimization and fabrication of a hybrid composite flywheel rotor [J]. Composite Structures, 2012, 94(11): 3290-3299.

王辉,武俊峰,吴一辉.轮缘驱动式姿控飞轮电机设计[J].工程设计学报,2012, 19(3): 225-230.

WANG H, WU J F, WU Y H. Design of rim-driven attitude control flywheel motor [J]. Chinese Journal of Engineering Design, 2012, 19(3): 225-230. ( in Chinese)

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Related Author

WANG Hui

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WU Yi-hui

LI Yin

WU Yi-hui

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Related Institution

Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences

Contionental Avtomotive corporation(Lianyungang) Co. Ltd. Changchun Branch

Electrical Engineering and Automation College, Anhui University

Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China

State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

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