首页> 外文会议>Saint Petersburg International Conference on Integrated Navigation Systems >PARAMETRIC IDENTIFICATION OF INTEGRATED NAVIGATION SYSTEMS IN REAL TIME AND FROM FLIGHT DATA
【24h】

PARAMETRIC IDENTIFICATION OF INTEGRATED NAVIGATION SYSTEMS IN REAL TIME AND FROM FLIGHT DATA

机译:实时和飞行数据中集成导航系统的参数识别

获取原文

摘要

Problems that arise during use of integrated navigation systems (INS) are considered. The proposed solutions permit us to take into account any changes in dynamic and accuracy characteristics of sensors by means of the appropriate coefficients of the models of errors. Under actual conditions of INS operation, the determination of current values of the parameters of the models of sensors and of an estimation filter rely on identification procedures. The results of full-scale experiments are given, which corroborate the expediency of parametric identification of the models of INS errors in real time and from flight data.
机译:考虑了在使用综合导航系统(INS)期间出现的问题。拟议的解决方案允许我们通过适当的错误系数来考虑传感器的动态和准确性特性的任何变化。在INS操作的实际条件下,确定传感器模型和估计滤波器的参数的当前值依赖于识别程序。给出了满量程实验的结果,其实时和从飞行数据中实际和从飞行数据中的INS错误模型的加速度。

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号