期刊文献+

A D-optimal Multi-position Calibration Method for Dynamically Tuned Gyroscopes 被引量:5

A D-optimal Multi-position Calibration Method for Dynamically Tuned Gyroscopes
原文传递
导出
摘要 This paper presents a novel experimental design to greatly improve the calibration accuracy of the acceleration-insensitive bias and the acceleration-sensitive bias of the dynamically tuned gyroscopes(DTGs).In order to reduce experimental cost,the D-optimal criteria with constraints are constructed.The turntable positions and the number of test points are chosen to build D-optimal experimental designs.The D-optimal experimental designs are tested by multi-position calibration experiment for tactical-grade DTGs.Test results show that,with the same cost,the fit uncertainty is reduced by about 50% by using the D-optimal 8-position experimental procedure,compared to using a defacto standard experimental procedure in ANSI/IEEE Std 813-1988.Furthermore,the new experimental procedure almost achieves optimal accuracy with only 12-position which is half the cost of the widely adopted 24-position experimental procedure for achieving optimal accuracy. This paper presents a novel experimental design to greatly improve the calibration accuracy of the acceleration-insensitive bias and the acceleration-sensitive bias of the dynamically tuned gyroscopes(DTGs).In order to reduce experimental cost,the D-optimal criteria with constraints are constructed.The turntable positions and the number of test points are chosen to build D-optimal experimental designs.The D-optimal experimental designs are tested by multi-position calibration experiment for tactical-grade DTGs.Test results show that,with the same cost,the fit uncertainty is reduced by about 50% by using the D-optimal 8-position experimental procedure,compared to using a defacto standard experimental procedure in ANSI/IEEE Std 813-1988.Furthermore,the new experimental procedure almost achieves optimal accuracy with only 12-position which is half the cost of the widely adopted 24-position experimental procedure for achieving optimal accuracy.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第2期210-218,共9页 中国航空学报(英文版)
基金 National Natural Science Foundation of China (61071014) National Basic Research Program of China(2009CB72400201)
关键词 optimization methods CALIBRATION GYROSCOPES error compensation design for testability optimization methods calibration gyroscopes error compensation design for testability
  • 相关文献

参考文献21

  • 1Merhav S. Aerospace sensor systems and applications. New York: Springer-Verlag, 1996.
  • 2Chatfield A B. Fundamentals of high accuracy inertial navigation. Reston: American Institute of Aeronautics and Astronautics, 1997.
  • 3Grewal M S, Henderson V D, Miyasako R S. Application of Kalman filtering to the calibration and align- ment of inertial navigation systems. IEEE Transactions on Automatic Control 1991; 36(1): 3-13.
  • 4Bekkeng J K. Calibration of a novel MEMS inertial reference unit. IEEE Transactions on Instrumentation and Measurement 2009; 58(6): 1967-1974.
  • 5Pittelkau M E. Calibration and attitude determination with redundant inertial measurement units. Journal of Guidance, Control, and Dynamics 2005; 28(4): 743-752.
  • 6Titterton D H, Weston J L. Strapdown inertial navigation technology. 2nd ed. Reston: American Institute of Aeronautics and Astronautics, 2004.
  • 7Syed Z F, Aggarwal P, Goodall C, et al. A new multi-position calibration method for MEMS inertial navigation systems. Measurement Science and Technology 2007; 18(7): 1897-1907.
  • 8American National Standards Institute. IEEE specification format guide and test procedure for two-degree-of-freedom dynamically tuned gyros. ANSI/IEEE Std 813-1988, 1989.
  • 9Cho S Y, Park C G.Calibration of a redundant IMU. AIAA-2004-5123, 2004.
  • 10Zhang H L, Wu Y X, Wu M P, et al. A multi-position calibration algorithm for inertial measurement units. AIAA-2008-7437, 2008.

同被引文献31

  • 1卿立,李海强.一种中低精度捷联惯测装置的不开箱标定方法研究[J].中国惯性技术学报,2004,12(4):16-19. 被引量:11
  • 2ARTESE G,TRECROCI A.Calibration of a low cost MEMS INS sensor for an integrated navigation system[C].The 21st ISPRS, 2008 : 877-882.
  • 3AYDEMIR G A ,SARANLL A.Characterization and calibra- tion of MEMS inertial sensors for state and parameter esti- mation applications[J].Measurement, 2012,45(5) : 1210-1225.
  • 4SCHOPP P, KLINGBEIL L, PETERS C, et al.Sensor fusion algorithm and calibration for a gyroscope-free IMU[J].Pro- cedia Chemistry, 2009,1 ( 1 ) : 1323-1326.
  • 5FU L, YANG X, WANG L L.A novel calibration procedure for dynamically tuned gyroscope designed by D-optimal approach [ J ]. Measurement, 2013,46 (9) : 3173- 3180.
  • 6LI C, ZHANG S F, CAO Y. One new onboard calibration scheme for gimbaled IMU [ J]. Measurement, 2013,46 (8) : 2359 - 2375.
  • 7LIU T, REN Q, WANG B, et al. An optimization method for self-calibration method of dual-axis rotational inertial navigation system [ C]// The Proceeding of the 32nd Chi- nese Control Conference, 2013: 5198- 5203.
  • 8FENG L, WANG B, DENG Z H, et al. On-line self-cali- bration for inertial platform system with a sin gle totally free axis [ C]//IEEE The 9th Asian Control Conference, 2013 : 1-6.
  • 9SEONG-HONG P W, FARID G. A triaxial accelerometer calibration method using a mathematical model [ C ] // IEEE Transcation on Instruction and Measurement, 2010, 59 ( 8 ) : 2044 - 2053.
  • 10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

引证文献5

二级引证文献11

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