期刊文献+

捷联惯性测量装置全温度标定方法 被引量:7

Calibrating method for strap-down inertial measurement unit at all environmental temperature
下载PDF
导出
摘要 为了提高捷联惯性测量装置(SIMU)的测量精度,在使用前必须对其进行标定,以确定SIMU的参数及性能指标。为此研究了一种SIMU的全温度标定方法,利用专用的测试设备对SIMU进行全温度标定试验。给出了SIMU的静态模型方程,详细介绍了模型方程中各参数的标定方法及具体的误差补偿计算方法,最后给出了SIMU综合性能指标的计算。经过多发SIMU的标定实验,结果表明:该标定方法有效地提高了SIMU的实际实用精度。 The Strap-down Inertial Measurement Unit(SIMU)must be calibrated before putting into use to improve its measurement precision and obtain its parameters and performance specifications. A method for calibrating SIMU at all environmental temperature was studied, a special test equipment was used for the calibrating test at all environmental temperature. Static model equations of SIMU were provided, the od of all parameters in the model equations and the calculating calibrating methmethod about error compensation were described in detail. The calculation of the SIMU's synthesis performance specifications was also presented. Lots of SIMUs have been calibrated. The experiment results showed that the applied precision of SIMU was improved effectively by this calibrating method.
出处 《电光与控制》 北大核心 2007年第6期127-130,143,共5页 Electronics Optics & Control
关键词 捷联惯性测量装置 标定 模型方程 误差补偿 strap-down inertial measurement unit calibration model equations error compensation
  • 相关文献

参考文献4

  • 1胡恒章.陀螺仪漂移测试原理及其实验技术[M].北京:国防工业出版社,1992.
  • 2陆元九.惯性器件[M].北京:宇航出版社,1993.
  • 3董景新,赵常德,曹志锦,等.微惯性仪表[M].北京:清华大学出版社,2003.167—168.
  • 4徐清雷,韩冰,邓正隆.激光陀螺捷联惯性组合的全温度标定方法[J].中国惯性技术学报,2004,12(6):4-7. 被引量:11

二级参考文献2

  • 1Malthan H. Test of a Honeywell GG1342 ring laser gyro [A]. Symposium on Gyro Technology[C]. Duesseldorf, West Ger:Deutsche Gesellschaft fuer Ortung und Navigation, 1982.
  • 2范胜林,孙永荣,袁信.捷联系统陀螺静态漂移参数标定[J].中国惯性技术学报,2000,8(1):42-46. 被引量:22

共引文献31

同被引文献45

  • 1严恭敏,秦永元.激光捷联惯组的双轴位置转台标定仿真[J].中国惯性技术学报,2007,15(1):123-127. 被引量:34
  • 2黄德鸣 程禄.惯性导航系统[M].哈尔滨:哈尔滨工程大学出版社,1999..
  • 3严恭敏,李四海,秦永元.惯性仪器测试与数据分析[M].北京:国防工业出版社,2012:157-178.
  • 4Skog I, H Ndel P. Calibration of a MEMS inertial measurement unit [C].//XVII IMEKO World Congress, 2006.
  • 5Fong W, Ong S, Nee A. Methods for in-field user calibration of an iner- tial measurement unit without external equipment [J]. Measurement Science and Technology, 2008, 19(8): 085202(1 lpp).
  • 6Syed Z, Aggarwal P, Goodall C, et al.A new multi-position calibration method for MEMS inertial navigation systems [J]. Measurement Sci- ence and Technology, 2007, 18(7): 1897-1907.
  • 7Shen S.C., Chen C.J., Huang H.J..A new calibration method for low cost MEMS inertial sensor module [J]. Journal of Marine Science and Technology, 2010,18(6): 819- 824.
  • 8J.C. L6tters, J. Schipper, P.H. Veltink, et al. Procedure for in-use cali- bration of triaxial accelerometers in medical applications [J]. Sensors and Actuators A: Physical, 1998, 61 ( 1):221-228.
  • 9黄德呜,程禄.惯性导航系统[M].哈尔滨工程大学出版社,1999,1-2.
  • 10ANSI/IEEE std813-1988,IEEE Specification Format Guide and Test Procedure for Two-Degree-of-Freedom Dynamically Turned Gyros[S]. American National Standards Institute, Approved May 4,1989.

引证文献7

二级引证文献13

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