基于最优解析的陀螺现场免转台标校方法

杨管金子;李建辰;黄海;国琳娜

兵工学报 ›› 2020, Vol. 41 ›› Issue (3) : 577-584.

兵工学报 ›› 2020, Vol. 41 ›› Issue (3) : 577-584. DOI: 10.3969/j.issn.1000-1093.2020.03.019
论文

基于最优解析的陀螺现场免转台标校方法

  • 杨管金子1,2, 李建辰1,2, 黄海1, 国琳娜1,2
作者信息 +

Non-turntable Field-calibration Method for Gyroscope Based on Optimal Analysis

  • YANG Guanjinzi1,2, LI Jianchen1,2, HUANG Hai1, GUO Linna1,2
Author information +
文章历史 +

摘要

作为载体姿态测量的重要惯性器件,陀螺在使用过程中由于长时间运输及存放等因素会产生误差漂移,造成对运动参数测量精度的降低,由此带来陀螺器件在使用前误差再标校的需求。根据现场无高精度转台设备支持的工作条件及中等精度陀螺指标需求,提出一种基于最优解析的陀螺现场标校方法。通过建立陀螺输出与地球自转角速率及加速度计输出间的映射关系式,将标校问题转换为最优解析问题;同时采用改进遗传算法,达到现场简易操作、不依赖转台等辅助设备、缩短标校时间、提高标校精度的目的。开展数学及半实物仿真实验,验证了所提方法的有效性,结果显示该方法能够有效地获得满足中等精度陀螺的标校结果,具有现场实用价值。

Abstract

Gyro is served as an important inertial device for vehicle attitude measurement. The error drift of gyroscope is due to long transportation and storage,which leads to the reduction in the measurement accuracy of motion parameters, thus needing to calibrate the gyroscope before use. A non-turntable field-calibration method for medium accuracy gyroscope based on optimal analysis is proposed in accordance with the working conditions without high precision turntable equipment in the field and the requirement of the indexes of medium accuracy gyroscope. The calibration problem is transformed into an optimal analytical problem by establishing the mapping relationship between the gyro output and the earth rotation rate as well as the accelerometer output. The method, combined with the improved genetic algorithm, is used to achieve the goal of simplifying the operation steps, doing not rely on turntable and other auxiliary equipment, shortening the calibration time and improving the calibration accuracy. The validity of the method is verified by mathematical and hardware-in-the-loop simulation experiments. The results show that the method can be used effectively to achieve the accuracy of medium-accuracy gyroscope calibration. Key

关键词

陀螺 / 现场标校 / 免转台 / 最优解析 / 改进遗传算法

Key words

gyroscope / fieldcalibration / turntable / optimalanalysis / improvedgeneticalgorithm

引用本文

导出引用
杨管金子, 李建辰, 黄海, 国琳娜. 基于最优解析的陀螺现场免转台标校方法. 兵工学报. 2020, 41(3): 577-584 https://doi.org/10.3969/j.issn.1000-1093.2020.03.019
YANG Guanjinzi, LI Jianchen, HUANG Hai, GUO Linna. Non-turntable Field-calibration Method for Gyroscope Based on Optimal Analysis. Acta Armamentarii. 2020, 41(3): 577-584 https://doi.org/10.3969/j.issn.1000-1093.2020.03.019

基金

国家重点实验室稳定支持基金项目(JCKY2019207CD02)

参考文献



[1]高伟,叶攀,许伟通.捷联惯导系统现场标定方法[J].计算机测量与控制,2016,24(7):301-303.
GAO W,YE P,XU W T.Field calibration method for strapdown inertial navigation system[J].Computer Measurement & Control,2016,24(7):301-303.(in Chinese)
[2]ALEXANDERK,IGOR S,NINA V.IMU calibration on a low grade turntable: embedded estimation of the instrument displacement from the axis of rotation[J]. Advance in Space Research,2014,48(5): 850-856.
[3]杨管金子,李建辰,黄海,等.基于遗传算法的加速度计免转台标定方法[J].中国惯性技术学报,2017,25(1):119-123.
YANG G J Z,LI J C,HUANG H,et al. Non-turntable calibration method for accelerometer based on genetic algorithm[J].Journal of Chinese Inertial Technology,2017,25(1):119-123.(in Chinese)
[4]崔敏,马铁华,张萌,等.无陀螺惯性测量系统的标定及误差补偿研究[J].电子测量与仪器学报,2009,23(9):23-26.
CUI M,MA T H,ZHANG M,et al. Research on calibration and error compensation for GFSINS[J].Journal of Electronic Measurement and Instrument,2009,23(9): 23-26.(in Chinese)
[5]FONG W T,ONG S K,NEE A Y C. Methods for in-field user calibration of an inertial measurement unit without external equipment[J].Measurement Science and Technology,2008,19(8): 085202.
[6]CHANG G B,XU J N,LI A,et al.Error analysis and simulation of the dual-axis rotation-dwell auto-compensating strapdown inertial navigation system [C]∥Proceedings of International Conference on Measuring Technology and Mechatronics Automation.Changsha, China:Changsha University of Science & Technology, Central South University,2010.
[7]WANG Y X,WU J,XU T,et al. Verification of rotation modulation effects on inertial navigation system based on MEMS sensors[J].Journal of Navigation,2013,66(5):751-772.
[8]WANG L,WANG W,ZHANG Q,et al.Self-calibration method based on navigation in high-precision inertial navigation system with fiber optic gyro[J].Optical Engineering,2014,53(6): 064103.
[9]LI K,GAO P,WANG L,et al. Analysis and improvement of attitude output accuracy in rotation inertial navigation system[J].Mathematical Problems in Engineering,2015,2015(1):1-10.

[10]MORGANA A,ELMILIGI H,EL_KHARASHI M W,et al.Multi-objective optimization for networks-on-chip architectures using genetic algorithm[C]∥Proceedings of 2010 IEEE International Symposium on Circuits and Systems.Piscataway,NJ,US: IEEE,2010:3725-3728.
[11]张樨,李杰,侯利朋,等.半捷联惯导系统轴向角度安装误差分析与补偿[J].兵工学报,2015,36(7):1222-1227.
ZHANG X,LI J,HOU L P,et al. Analysis and compensation of installation axial angle errors of semi-strapdown IMS[J].Acta Armamentarii,2015,36(7):1222-1227.(in Chinese)
[12]金涛,周泽渊,陈晓洪.基于伪并行遗传算法的消防管网受损电定位方法[J].海军工程大学学报,2016,28(3): 40-44.
JIN T,ZHOU Z Y,CHEN X H.Leakage localization method based on pseudo-parallel genetic algorithm for fire fighting system [J]. Journal of Naval University of Engineering,2016,28(3): 40-44.(in Chinese)
[13]宫志华,段鹏伟,刘洋,等.多样本遗传算法在武器外弹道组网试验中的应用[J].兵工学报,2019,40(7): 1503-1510.
GONG Z H,DUAN P W,LIU Y,et al. Application of multi-sample genetic algorithm in weapon exterior ballistics networking test[J].Acta Armamentarii,2019,40(7):1503-1510.(in Chinese)
[14]PAWARS N,BICHKAR R S.Genetic algorithm with variable length chromosomes for network intrusion detection[J].International Journal of Automation and Computing,2015,12(3):337-342.
[15]张步忠,程玉胜,王一宾.求解N皇后问题的片上多核并行混合遗传算法[J].计算机工程,2015,41(7):199-203.
ZHANG B Z,CHENG Y S,WANG Y B.On-chip multi-core parallel hybrid genetic algorithm for solving N-queens problem[J]. Computer Engineering,2015,41(7): 199-203.(in Chinese)





第41卷
第3期2020年3月兵工学报ACTA
ARMAMENTARIIVol.41No.3Mar.2020

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