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1. 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
2. 中国科学院 研究生院 北京,100039
收稿日期:2005-04-22,
修回日期:2005-11-18,
网络出版日期:2006-02-20,
纸质出版日期:2006-02-20
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刘治华, 白 越, 黎海文, 等. 单轴飞轮储能与姿态控制系统误差分析[J]. 光学精密工程, 2006,14(1):127-132.
LIU Zhi-hua, BAI Yue, LI Hai-wen, et al. Analysis on errors of single axis energy storage/attitude control system with double flywheels[J]. Optics and precision engineering, 2006, 14(1): 127-132.
介绍了单轴飞轮储能及姿态控制一体化系统的总体构成和工作原理
研究并推导了系统的数学模型
分析了系统误差产生的原因
建立了转台角度位置误差与转子安装不同轴误差、转子偏心误差、飞轮速度测量与控制误差之间的误差关系式
并进行了误差合成。结合实际实验系统算出了各项误差
并对比和分析了各项误差。结果表明:影响系统位置精度的主要因素有飞轮安装不同轴误差、转动惯量误差和飞轮速度测量与控制误差等
其中飞轮转动惯量误差和飞轮安装不同轴误差是不可控量;而飞轮的转速测量与控制误差是可控量。最后提出了提高飞轮储能与姿态控制系统精度的主要方法
可以通过提高位置测量传感器和速度测量传感器的分辨率
采用先进的控制算法来降低飞轮的转速测量与控制误差。
The general structure and working principle of the single axis energy storage/attitude control system were introduced. The mathematical model of the system was studied and put forward; the cause of errors was analyzed; the equations of platform angular error and flywheel install error
the platform angle error and flywheel eccentricity error
the platform angle error and error of flywheel speed measurement and control were also analyzed
respectively; then every piece of errors were compounded. The actual errors were computed combined with the actual experimental system
and each error was compared and analyzed. The results show that the primary factors are the flywheel install error
flywheel eccentricity error
speed measurement error and control error etc. The install error and eccentricity error are uncontrolled factors
while the flywheel speed measurement error and control error are controllable factors. In conclusion
the primary method that can improve the attitude control precision is presented; the speed measurement error and control error of flywheels can be reduced by improving the resolutions of position sensor and speed sensor
as well as adopting advanced control algorithm.
. 杨宁, 王昊, 田蔚风, 等 高精度飞轮控制系统方案分析研究[J]. 航天控制, 2004, 22(3): 50-53. YAGN N, WANG H, TIAN W F, et al. Analysis and research on the proposal of the high precision flywheel control system.[J]. Aerospace Control, 2004, 22(3):50-53.(in Chinese)
. 夏永江, 张云, 牛睿. 卫星储能/姿控一体化飞轮构型及其误差分析[J]. 上海航天, 22(1): 19-23. XIA Y J, ZHANG Y, NIU R. Analysis on configuration and errors of integrated power and attitude control flywheel in satallite.[J]. Aerospace Shanghai, 22(1): 19-23.(in Chinese)
. 贾宏光, 赵华兵, 白越,等. 单轴储能及姿态控制一体化系统研究[J]. 光学 精密工程, 2004, 12(5): 504-509. JIA H G, ZHAO H B, BAI Y, et al. Single axis double flywheels integrated power and attitude control system[J]. Optics and Precision Engineering, 2004, 12(5): 504-509.(in Chinese)
. 韩邦成. 单轴飞轮储能/姿态控制系统的仿真及其实验研究 . 中国科学院长春光学精密机械与物理研究所, 2004. HAN B CH. Simulation and experiment of single axis attitude control and energy storage system with two flywheels . Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, 2004.
. KENNY B,KASCAK P. DC bus regulation with a flywheel energy storage system . NASA/TM-2002-211897, NASA Glenn Research Center.
. KASCAK P E,JANSEN R H,KENNY B,et al.Single axis attitude control and DC bus regulation with two flywheels . IECEC 2002-20078.
. 刘巧伶. 理论力学[M]. 长春: 吉林科学技术出版社, 1997. LIU Q L. Theoretical mechanics [M]. Changchun: Jilin Science and Technology Press 1997.(in Chinese)
. 费业泰. 误差理论与数据处理[M]. 北京: 机械工业出版社, 2004. FEI Y T. Error theory and data process [M]. Beijing: China Machine Press 2004.(in Chinese)
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