首页> 外国专利> A NAVIGATION SYSTEM UTILIZING YAW RATE CONSTRAINT DURING INERTIAL DEAD RECKONING

A NAVIGATION SYSTEM UTILIZING YAW RATE CONSTRAINT DURING INERTIAL DEAD RECKONING

机译:惯性航迹推算过程中利用横摆率约束的导航系统

摘要

A system operating in a dead reckoning mode accumulates relative yaw measurements, i.e., measurements of rotation about a z-axis, made by one or more over mechanization update intervals and produces dead reckoning mechanization update values. The system accumulates the values over a turn rate accumulation period, calculates a yaw rate and determines if the yaw rate exceeds a turn rate threshold. If so, the system directs an INS filter to perform a zero yaw rate update at the start of a next mechanization update interval, to correct for the z-axis drift errors of the gyroscopes based on the sensed rotation in the relative yaw measurements over the previous mechanization update interval. The system then sets the z-axis drift errors to zero. If the system determines that the yaw rate exceeds the turn rate threshold, the zero yaw rate update is not performed at the start of the next mechanization update interval.
机译:在航位推算模式下运行的系统累积由一个或多个机械更新间隔进行的相对偏航测量值,即绕z轴的旋转测量,并产生航位推算机械更新值。系统在转弯速率累积时段内累积值,计算偏航速率,并确定偏航速率是否超过转弯速率阈值。如果是这样,系统将指示INS滤波器在下一个机械化更新间隔开始时执行零偏航角速度更新,以基于在相对偏航测量中感测到的旋转来校正陀螺仪的z轴漂移误差。先前的机械化更新间隔。然后,系统将z轴漂移误差设置为零。如果系统确定偏航率超过转弯率阈值,则在下一个机械化更新间隔开始时不执行零偏航率更新。

著录项

  • 公开/公告号EP3385671A1

    专利类型

  • 公开/公告日2018-10-10

    原文格式PDF

  • 申请/专利权人 NOVATEL INC.;

    申请/专利号EP20180150408

  • 发明设计人 BOBYE MICHAEL;

    申请日2018-01-05

  • 分类号G01C21/16;G01S5;

  • 国家 EP

  • 入库时间 2022-08-21 13:15:19

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