期刊文献+

高精度加速度计重力场标定试验方法 被引量:13

Calibration test method of high-precision accelerometer in gravitational field
下载PDF
导出
摘要 为标定高精度(10-6)的加速度计,提出了一种在双轴转台上进行正交双加速度计标定的试验方案,建立了正交双加速度计的g2观测模型;分析了正交双加速度计的模型系数相关性,在此基础上基于D-最优试验设计方法,针对加速度计多位置试验中模型方程的特殊形式,利用信息矩阵推导出了该试验计划的解析解。仿真试验和实测数据的估计结果均表明:双表试验辨识结果的标准差较小,参数的估计精度较高,优于传统的单表试验方法,双表试验能提高高精度加速度计的标定精度。 A method of calibrating the dual orthogonal accelerometers(DOA) on a two-axis turning table was proposed to calibrate the high-precision accelerometer. A square-of-g observation model was built for the DOA and the correlation of the DOA model coefficients was analyzed. Based on the D- optimal experiment design, according to the special form of the model equation in the multi-position test of the accelerometers, an analytical solution of the experiment design was derived using the information matrix of equation. The simulation and experiment demonstrated that the standard deviation of the DOA method is less than, and its identification accuracy is better than that of the single accelerometer. So, the DOA method can enhance the calibration accuracy of the high-precision accelerometer.
出处 《吉林大学学报(工学版)》 EI CAS CSCD 北大核心 2010年第1期287-292,共6页 Journal of Jilin University:Engineering and Technology Edition
基金 '973'国家安全重大基础研究项目(973-61334)
关键词 仪器仪表技术 加速度计 标定试验 模型辨识 正交双加速度计法 D-最优 重力场标定试验 technology of instrument and meter calibration test accelerometer model identification dual orthogonal accelerometers(DOA) method D optimal plan calibration test in gravity field
  • 相关文献

参考文献9

  • 1张春京,原俊安,李凡东,王雷,任多立.从加速度计测试技术研究看惯性仪表测试技术发展趋势[J].航天控制,2005,23(2):78-84. 被引量:19
  • 2Gyro and Accelerometer Panel of the IEEE Aerospace and Electronic System Society. IEEE standard specification format guide and test procedure for linear, single-axis, nongyroscopic accelerometers[S]. New York= The Institute of Electrical and Electronics Engineers, 1998.
  • 3Yogesh B G, Selden B C. Parametric modeling of a microaccelerometer: comparing I- and D-optimal design of experiments for finite-element analysis [ J]. Journal of Microelectromechanical Systems, 1998,7 (2) : 274-282.
  • 4Begot S, Voisin E, Hiebel P. D-optimal experimental design applied to a linear rnagnetostatie inverse problem [J]. IEEE Transactions on Magnetics, 2002,38(2) : 1065-1068.
  • 5富立,刘文丽.D-最优试验设计在动力调谐陀螺测试中的应用[J].航空学报,2008,29(2):467-471. 被引量:12
  • 6Moreira P A F P, Guedes S, Iunes P J, et al, D-optimal design of fission track annealing experiments [J], Nuclear Instruments and Methods in Physics Research: Section B, 2005,240(4): 881-887.
  • 7Gyro and Accelerometer Panel of the IEEE Aero space and Electronic System Society. IEEE recommended practice for inertial sensor test equipment, instrumentation, data acquisition, and analysis[S]. New York: The Institute of Electrical and Electronics Engineers, 2005.
  • 8Magnus M. Optimal experimental design for identification of viscoelastic materials[J]. IEEE Transactions on Control Systems Technology, 2004,12 (4) : 578-582.
  • 9Qiao Y H, Liu Y, Su B K. Study on PIGA test method on centrifuge[C] // International Conference on Computation Intelligence and Security, Harbin, 2007:42-47.

二级参考文献15

  • 1邹达明,谢李李.关于动力调谐陀螺8位置法漂移测试的研究[J].应用科技,2004,31(8):44-46. 被引量:2
  • 2祁家毅,任顺清,王常虹.用三轴转台辨识陀螺仪误差模型系数时的速率试验设计[J].宇航学报,2006,27(3):565-570. 被引量:11
  • 3荣伟彬,陈涛,陈立国,孙立宁.挠性陀螺十字铰链模型的建立与分析[J].光学精密工程,2006,14(5):864-869. 被引量:4
  • 4乔永辉,刘雨,苏宝库,曾鸣.陀螺加速度计误差模型系数离心机测试方法研究[J].宇航学报,2007,28(4):854-859. 被引量:17
  • 5Tom Reed. Consultant Milli Sensor Systems & Actuators,Inc. (MSSA,Inc.) ,Future Guidance,Navigation & Control Issues[ C ]. 17th Biennial Guidance Test Symposium Holloman Air Force Base,New Mexico 1995:42 -60.
  • 6Fredric Nadeau. The CIGFT Connection:A StoW of Precision Testing at the Central Inertial Guidance Test Facility [ C ]. Institute of Navigation, Annual Meeting, 51 st,Colorado Springs, CO, June 5 - 7, 1995, Proceedings( A96-1400102-32 ) , Alexandria, VA, Institute of Navigation. 1995:283 - 292.
  • 7Captain Roger Evans. Use of a High Performance Aircraft and GPS to Evaluate the Accuracy of the Peacekeeper Inertial Measurement Unit [ C ]. 16th Biennial Guidance Test Symposium. Holloman Air Force Base,New Mexico, October 5 - 7,1993 : 169 - 182.
  • 8M. V. Chichinadze, V. N. Ilyin, A. V. Novgorodski, N.Barbour. Accelerometer Designs and Fields of Application[ C ]. 3th Saint Petersburg International Conference on Integrated Navigation Systems, 1996 : 115 - 125.
  • 9John Boutelle, Dr. ShingP. Kau, Charles J. Marino. ICBM Reentry Vehicle Navigation System Development at Honeywell [ R ]. 0-7803-4330-1/98/IEEE 1998:294 - 301.
  • 10Dr. ShingP. Kau, John Boutelle, Larry Lawdermih. Accelerometer Input Axis Angular Acceleration Sensitivity[ R ]. 0-7803-5872-4/00/IEEE 2000:449 - 456.

共引文献27

同被引文献103

引证文献13

二级引证文献34

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