期刊文献+

基于转动的光纤陀螺捷联系统初始对准研究 被引量:6

Study on Initial Alignment of Fiber Optic Gyro SINS Based on Rotation
下载PDF
导出
摘要 基于某型低精度光纤陀螺捷联系统,分别采用经典罗经对准、两位置卡尔曼滤波及连续旋转卡尔曼滤波三种方法进行了初始对准实验研究。结果表明,经典罗经对准方法由于未对零偏进行处理,导致其精度不高。两位置卡尔曼滤波方法可以对惯性器件的零偏进行估计并补偿,一定程度上提高了精度。连续旋转卡尔曼滤波方法通过调制抑制陀螺零偏误差影响,相比前两种对准方法,精度显著提高,该文进行了理论分析。 Based on one fiber optic gyro SINS, three initial alignment methods including classical gyrocompass, two-position Kalman filter and continuous-rotation Kalman filter are experimentally studied. The result shows that the alignment accuracy of classical gyrocompass method is low due to the non-compensated bias of IMU. Two-position Kalman filter can estimate and compensate the biases of gyros and accelerometers, and thus the accuracy is improved. Continuous rotation Kalman filter can modulate and restrain the bias, which greatly improves the alignment accuracy compared with above two methods. Additionally, theoretical analysis is given in this paper.
出处 《压电与声光》 CSCD 北大核心 2007年第5期519-522,共4页 Piezoelectrics & Acoustooptics
关键词 捷联惯性导航 初始对准 卡尔曼滤波 光纤陀螺 strapdown inertial navigation initial alignment Kalman filter fiber optic gyro
  • 相关文献

参考文献4

二级参考文献7

  • 1赵忠.惯性平台测漂对准的一种新方案[J].西北工业大学学报,1995,13(3):432-436. 被引量:2
  • 2袁信,导航系统,1993年,135页
  • 3蒋正新,矩阵理论及其应用,1988年,116页
  • 4王锦瑜.激光陀螺速率偏频技术研究[D].西安:西北工业大学,2000.
  • 5Buschelberger H J,Handrich E,H Malthan H,et al.Laser gyros in system applications with rate-bias technique[A].Symposium Gyro Technology[C].Stuttgart Germany,1987.
  • 6Mathews A,Wetter H.Cost efficient high accuracy inertial navigation[J].Navigation,1989,36(2):157-172.
  • 7Kuryatov V N,Cheremisenov G V,Panasenko V N,et al.Marine INS based on the laser gyroscope KM-11[A].Symposium Gyro Technology[C].Stuttgart Germany,2002.

共引文献90

同被引文献44

引证文献6

二级引证文献31

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