期刊文献+

加速度计误差系数对拟合残差的影响及试验分析 被引量:1

accelerometer error coefficient's Impact on fitting residual and its experimental analysis
在线阅读 下载PDF
导出
摘要 为了提高加速度计的测试精度,针对加速度计在重力场的试验,分析了加速度计误差模型中误差系数对辨识拟合残差的影响。通过石英挠性加速度计的三十六位置翻滚试验,利用最小二乘参数估计后,根据残差曲线的规律性形状确定了加速度计误差模型中存在零偏不对称项和标度因数不对称项,从而进一步完善误差模型。试验结果表明,被测加速度计的零偏不对称项和标度因数不对称项对辨识结果影响很大,加入到误差模型中拟合残差标准差从原来的1.1×10-5g提高到7×10-6g左右,精度明显得到改善。 To increase the measuring precision of accelerometer,the impact of accelerometer error coefficient on the discrimination of fitting residual is analyzed based on the accelerometer's gravitational field experiment,and it is pointed out that the error coefficient could be determined by the shape of fitting residual.By the quartz flexible accelerometer 36-position tumbling experiment,it is found that there are bias asymmetry and factor asymmetry in accelerometer error model after making the least squares parameter identification,and they can be used to perfect the error model.The experimental results show that,after adding error coefficient in the model,the residual is reduced from 1.1×10-5 g to 7×10-6 g and the identification accuracy is significantly improved.
出处 《中国惯性技术学报》 EI CSCD 北大核心 2010年第6期761-765,共5页 Journal of Chinese Inertial Technology
基金 总装备部"十一五"预研项目(51309050702)
关键词 加速度计 重力场试验 误差系数 拟合残差 accelerometer experiment in the gravitational field error coefficient fitting residual
  • 相关文献

参考文献12

二级参考文献29

  • 1杨亚非,吴广玉,任顺清.提高加速度计标定精度的方法[J].中国惯性技术学报,1998,6(4):99-103. 被引量:7
  • 2徐凤霞,夏刚,曾鸣,苏宝库.用三轴转台减小陀螺加速度表输入失调角的试验研究[J].中国惯性技术学报,2005,13(4):70-73. 被引量:4
  • 3朱家友,李华容,卜继军,彭志高.加速度计八位置标定测试系统的开发[J].压电与声光,2007,29(2):170-172. 被引量:5
  • 4何铁春 周世勤.惯性导航加速度计[M].北京:国防工业出版社,1983..
  • 5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
  • 6Tom 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.
  • 7Fredric 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.
  • 8Captain 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.
  • 9M. 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.
  • 10John 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.

共引文献81

同被引文献8

  • 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
  • 2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
  • 3AEDTC-TP-92-38, 6585th Test Group. Honeywell Advanced Technology Advanced Inertial Measurement Unit Laboratory and Sled Test[R], Guidance Test Division, Holloman AFB, New Mexico 88330-5000, 1992: 10-21.
  • 4Colombatti G, Aboudana A, Ferria F, Angrillia E Huygens probe entry dynamic model and accelerometer data analysis[J]. Planetary and Space, 2008, 56(5): 601-612.
  • 5Anthony S Hu. Improved space-time reference systems for use on rocket sled track[R]. Air Force Special Wespon Center. 1972:2-41.
  • 6IEEE Std 1293-1998, IEEE Standard Specification Format Guide and Test Procedure for Linear, Single-Axis, Nongyoscopic Accelerometers[S]. IEEE Aerospace and Electronic System Society, 1988.
  • 7Akira U, Mike O, Kohji S, et al. Calibration of three-axis accelerometers using a three-dimensional vibration generator and three laser interferometers[J]. Sensors and Actuators, A: Physical, 2004, 114(1): 93-101.
  • 8陈东生,魏宗康,房建成.验证石英加速度计误差模型的火箭橇试验[J].中国惯性技术学报,2009,17(2):236-239. 被引量:15

引证文献1

二级引证文献9

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