期刊文献+

炮载惯导高精度准动态零速修正方法 被引量:2

High precision dynamic zero velocity update for gun-board SINS
下载PDF
导出
摘要 针对现有零速修正方法效率低下的问题,以某型自行火炮为研究对象,利用加速度信息推导出了匀速直线运动时载体两个方向的姿态及角速度,并详细介绍了推导过程。为提高零速修正的精度和实时性,以所得姿态为基准,将其加入到滤波观测量中,使得原有速度匹配改为速度加姿态匹配,提出了高精度动态零速修正方法。仿真结果表明,利用加速度信息能有效获得当前载体姿态,验证了该方法的正确性。在跑车实验之前,利用有限冲激响应(finite impulse response,FIR)数字滤波器处理加速度计输出信息,实验结果表明,所提新方法能大幅提高零速修正的精度和实时性,东向位置误差在10m以内,北向位置误差在20m以内,实现了在连续行车条件下的高精度导航和误差标定。 Taking certain type self-propelled gun as the target of study,two directions of attitude and angular velocity are derived using the acceleration information when the carrier in a uniform straight line motion,and the derivation process are introduced in detail.In order to improve the zero velocity update precision and realtime performance,the attitude is taken as a benchmark,and is added to the filter in the observation.The original velocity matching is changed to velocity and attitude matching.The high precision dynamic zero velocity update method is put forward.The simulation results show that using acceleration information can effectively get the current carrier attitude,verifying the correctness of the method.Before sports car test,the accelerometer output information is processed using the finite impulse response(FIR)digital filter.The experiment results show that the accuracy and real-time performance of zero velocity update is greatly increased by using the proposed method,limiting the east position error within 10 m,and north position error within 20 m.High precision navigation and error calibration are realized under the condition of continuous driving.
作者 王志伟 狄长春 杨功流 石志勇 杨玉良 王风杰 WANG Zhiwei;DI Changchun;YANG Gongliu;SHI Zhiyong;YANG Yuliang;WANG Fengie(Department of Artillery Engineering , Army Engineering University , Shijiazhuang 050003 , China;School of InsirumenUion Science and OpLo-elecLronics Engineering , Beihang University , Beijing 100191 , China;Unit 63870 of the PLA , Huayin 714200 , China)
出处 《系统工程与电子技术》 EI CSCD 北大核心 2017年第12期2782-2789,共8页 Systems Engineering and Electronics
基金 国防预研基金资助课题
关键词 晃动补偿 捷联惯导 零速修正 有限冲激响应数字滤波 shaking compensation strapdown inertial navigation system(SINS) zero velocity update finite impulse response(FIR)digital filter
  • 相关文献

参考文献8

二级参考文献42

  • 1秦永元,严恭敏,顾冬晴,郑吉兵.摇摆基座上基于信息的捷联惯导粗对准研究[J].西北工业大学学报,2005,23(5):681-684. 被引量:131
  • 2严恭敏,秦永元,杨波.车载航位推算系统误差补偿技术研究[J].西北工业大学学报,2006,24(1):26-30. 被引量:41
  • 3[1]Chatfield A B.Fundamentals of High Accuracy Inertial Navigation[M].AIAA,1997. 被引量:1
  • 4[2]Britting K R.Inertial Navigation Systems Analysis[M].New York:Wiley-interscience,1971. 被引量:1
  • 5[3]Lian J,Wu Y,Wu W,et al.A Novel Strapdown INS Alignment Method for Swaying Vehicles[C]//13th International Conference on Integrated Navigation System,Saint Petersburg,Russia,2006. 被引量:1
  • 6[4]Giovanni C S,Levinson E.Performance of a Ring Laser Strapdown Marine Gyrocompass[C]//ION 37th Annual Meeting Proceedings,Annapolis,Maryland,USA,1981. 被引量:1
  • 7[5]Wan D,Huang Y,Ren T.Study on New Kalman Filter Mechanization for Initial Alignment of INS in Random Rocking Vehicles[C]//Stuttgart,West Germany,1989. 被引量:1
  • 8[6]El-sheimy N,Nassar S,et al.Wavelet De-noising for IMU Alignment[J].IEEE/AES Magazine,2004,19. 被引量:1
  • 9[7]Zhang C,Tian W,Jin Z h.A Novel Method Improving the Alignment Accuracy of a Strapdown Inertial Navigation System on a Stationary Base[J].Measurement Science and Technology,2004,15:765. 被引量:1
  • 10[8]Gaiffe T,Cottreau Y,Faussot N,et al.Highly Compact Fiber Optic Gyrocompass for Applications at Depths up to 3,000 Meters[C]//IEEE/Underwater Technology,Proceedings of the International Symposium,2000. 被引量:1

共引文献92

同被引文献8

引证文献2

二级引证文献6

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