期刊文献+

半球谐振子动力学方程的建立及固有频率的计算 被引量:10

Establishment of dynamics equation of HRG resonator and calculation of natural frequency
下载PDF
导出
摘要 为了建立半球谐振陀螺仪谐振子的动力学方程,由基希霍夫-李雅夫假设分析了半球谐振子上任一点的应变及应力,然后在谐振子上取一薄壳单元,对其进行受力分析,并考虑了三轴角速率和角加速度的情况下引起的惯性力,建立了薄壳单元的平衡方程及薄壳的边缘运动方程,利用解微分方程的布勃诺夫-加廖尔金法建立了谐振子的动力学方程,最后根据动力学方程求出了谐振子的固有频率.通过与各种计算固有频率的方法的计算值以及实测值的比较,证明了本文推导的半球谐振子动力学方程和固有频率的正确性。 In order to establish dynamics equation of resonator in HRG,the strains and stresses of an arbitrary point in the hemispherical thin shell were deduced under Kirchhoff-Lyav hypothesis.The force and torque equilibrium equations of the thin shell element selected from the resonator were gained on the basis of the calculated strains and stresses,then the border motion equations of the HRG were obtained in consideration of the subjected 3-D angular rate and the 3-D angular acceleration.Finally the dynamics equations of resonator were established by Bubonov-Galerkin method which is common used for solving differential equations,thus the natural frequency is computed by the established dynamics equations.By contrast with other methods of calculating natural frequency and the measured frequency values of practical HRG,the correctness of the established dynamics equations and the method of frequency calculation are proved.
出处 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 2010年第11期1702-1706,共5页 Journal of Harbin Institute of Technology
基金 国防预研项目(51309050601)
关键词 半球谐振陀螺 固有频率 动力学 hemispherical resonator gyro natural frequency dynamics
  • 相关文献

参考文献3

二级参考文献4

  • 1Lin Gaufeng,1979年
  • 2Lynch D D. Hemispherical resonator gyros [J]. TOS Technical Journal , 1995 ,3(1).
  • 3Lynch D D. Coriolis vibratory gyros[C]//Stuttgart ,Germany: Symposium Technology ,1998.
  • 4Anthony Matthews , Santa Barbbara. Vibratory rotation sensor with scanning tunneling transducer readout[p]. USP. 5712427 , Jan , 27 , 1998.

共引文献44

同被引文献56

  • 1伊国兴,谢阳光,王常虹,祁子阳.加速度对半球谐振陀螺振动检测系统影响分析[J].中国惯性技术学报,2013,21(5):676-681. 被引量:3
  • 2沈博昌,伊国兴,任顺清,王常虹,方针.半球谐振陀螺仪谐振子振动特性的有限元分析[J].中国惯性技术学报,2004,12(6):56-60. 被引量:11
  • 3樊尚春,刘广玉,王振均.半球谐振陀螺的理论与实验研究[J].测控技术,1994,13(1):29-33. 被引量:11
  • 4樊尚春,刘广玉.半球谐振陀螺振子耦合振动的有限元分析[J].仪器仪表学报,1995,16(3):281-287. 被引量:6
  • 5Emily L B, Allan Y L. In-flight characterization of Cassini inertial reference units[C]//AIAA Guidance, Navigation and Control Conference and Exhibit, 20-23 August 2007. Hilton Head, South Carolina, AIAA 2007-6340.
  • 6B.A.MaTBeea,B.H.YlvtnaTnnroB, A.B.A.aexiH.HpoegTnpo8 aHrie.Boauoaoro rBeporeJrrnoro rrapocKona[M]. t3,aaxea1,erao MFTY mei-iriH.3.13ayMai-la, 1998: 1-43.
  • 7Emily L B, Allan Y L. In-flight characterization of Cassini inertial reference units[C]//AIAA Guidance, Navigation and Control Conference and Exhibit, 20 - 23 August 2007 Hilton Head, South Carolina, AIAA 2007-6340.
  • 8Jiayi Q, Xue C, Shunqing R, Changhong W. Dynamic error mechanism analysis of HRG[C]//ISSCAA2008. Shenzhen, 2008-12.
  • 9Zhbanov Y K. Vibration of a hemispherical shell gyro excited by an electrostatic field[J]. Mechanics of Solids, 2008, 43(3): 328-332.
  • 10Zhbanov Y K, Zhuravlev V P. Effect of movability of the resonator center on the operation of a hemispherical resonator gyro[J]. Mechanics of Solids, 2007, 44(3): 851-859.

引证文献10

二级引证文献56

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部