Study on the Master Inertial Navigation System Reference Data Delay Processing Method in Transfer Alignment

XIA Jia-he;QIN Yong-yuan;ZHAO Chang-shan

Acta Armamentarii ›› 2009, Vol. 30 ›› Issue (3) : 342-345. DOI: 10.3969/j.issn.1000-1093.2009.03.017
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Study on the Master Inertial Navigation System Reference Data Delay Processing Method in Transfer Alignment

  • XIA Jia-he, QIN Yong-yuan, ZHAO Chang-shan
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Abstract

A method for processing the problem resulting from master inertial navigation system (MINS) data delay in transfer alignment was presented. When the slave inertial navigation system (SINS) got the MTNS reference data, the data was processed by Kalman filtering and the time origin was unified to the moment corresponding to the MINS data; the current error estimation of the SINS was obtained by time update. Simulation results show that the transfer alignment performance is im?proved by compensating data delay; in the fast and high accuracy alignment it is necessary to take the MINS reference data delay into account.

Key words

control and navigation technology of aerocraft / transfer alignment / data delay / Kalman filter / time update

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XIA Jia-he, QIN Yong-yuan, ZHAO Chang-shan. Study on the Master Inertial Navigation System Reference Data Delay Processing Method in Transfer Alignment. Acta Armamentarii. 2009, 30(3): 342-345 https://doi.org/10.3969/j.issn.1000-1093.2009.03.017

References

[I] Bar-ItzhacJs I Y,Vitek Y. The enigma of false bias detection in a strap down system during transfer alignment [J ] ? Journal of Guid?ance, 1985,8(2): 175-180.
[2] You-Chol Lim, Joon Lyou. An error compensation method for transier alignment[C] //Proceedings of IELE Lxxiference on Elec?trical and Electronic Technology. Singapore: IEEE, 2001 : 850 -855.
[3] 扈光锋,王艳东,范跃祖.传递对准中測量延迟的补偿方法 [J3 ?中国惯性技术学报,2005,13(1):10 — 14.
HU Guang-feng, WANG Yan-dong, FAN Yue-zu. Compensation method for measurement delay in transfer alignment [ J ]. Journal of Chinese Inertial Technology, 2005,13(1) : 10-14. (in Chi?nese)
[4] 魏志刚.空空导弹系統信息延迟时间的测试及分析[J].航空 兵器,2005,(5):7-9.
WEI Zhi-gang. Test and analysis of iniormation transmit delay in air-to-air missile system[J]. Aero Weaponry, 2005,(5) :7 - 9. (in Chinese)
[5] Azor R, Bar-Itzhack I Y, Deutschmann J K, et al. Angular-rate estimation using delayed quaternion measurements [ J ]. Journal of Guidance, Control, and Dynamics, 2001, 24(3) :436 - 443.
[6] Larsen T D, Anderson N A, Ravn 0. Incorporation of time de?layed measurements in a discrete-time Kalman filter [C]//Pro?ceedings of the 37th IEEE Conference on Decision & Control Tampa. Florida: IEEE, 1998: 3972-3977.

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