首页> 外国专利> HEADING INCONSISTENCY MITIGATION FOR INERTIAL NAVIGATION USING LOW-PERFORMANCE INERTIAL MEASUREMENT UNITS WITH RELATIVE AIDING

HEADING INCONSISTENCY MITIGATION FOR INERTIAL NAVIGATION USING LOW-PERFORMANCE INERTIAL MEASUREMENT UNITS WITH RELATIVE AIDING

机译:使用相对辅助的低性能惯性测量单元进行惯性导航的航向不一致性缓解

摘要

A method of mitigating filter inconsistency of a heading estimate in an inertial navigation system is provided. The method includes inputting inertial measurements from at least one low-performance inertial measurement unit (IMU) in the inertial navigation system; inputting an initial-heading from at least one heading-information source; inputting an initial-heading uncertainty level associated with an error in the inputted initial-heading; initializing an initial-heading estimate with the inputted initial-heading; initializing an initial-heading uncertainty estimate with the inputted initial-heading uncertainty level; initializing an accumulated heading-change estimate to zero at a startup of the at least one low-performance IMU; and initializing an accumulated heading-change uncertainty estimate with an initial accumulated heading-change uncertainty level that is a value less than the inputted initial-heading uncertainty level; and periodically updating the accumulated heading-change estimate with the inertial measurements input from the at least one low-performance IMU.
机译:提供了一种减轻惯性导航系统中的航向估计的滤波器不一致的方法。该方法包括从惯性导航系统中的至少一个低性能惯性测量单元(IMU)输入惯性测量;以及从至少一个航向信息源输入初始航向;输入与所输入的初始航向中的误差有关的初始航向不确定度;用输入的初始标题初始化初始标题估计;用输入的初始航向不确定性水平初始化初始航向不确定性估计;在至少一个低性能IMU启动时将累积的航向变化估计初始化为零;并以小于输入的初始航向不确定性水平的值的初始累积航向变化不确定性水平来初始化累积航向变化不确定性估计;以及利用从至少一个低性能IMU输入的惯性测量值来周期性地更新累积的航向变化估计。

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