首页> 外国专利> Configurable inertial navigation system with dual extended kalman filter modes

Configurable inertial navigation system with dual extended kalman filter modes

机译:具有双重扩展卡尔曼滤波模式的可配置惯性导航系统

摘要

A system and method for more accurately and robustly estimating navigation state of a vehicle by adaptively processing signals from an inertial sensor assembly and other sensors. A navigation system receives signals from two or more sensors to evaluate and correct the attitude estimated by an Extended Kalman Filter (EKF). The navigation system selects sensor signals from the other sensor assemblies and processes the selected sensor signals in conjunction with estimates from the inertial navigation module to obtain more accurate estimates of the attitude. The parameters and conditions for using certain sensor signals may be adjusted based on the characteristics and configuration of the vehicle.
机译:一种通过自适应地处理来自惯性传感器组件和其他传感器的信号来更准确,更可靠地估计车辆导航状态的系统和方法。导航系统从两个或多个传感器接收信号,以评估和校正扩展卡尔曼滤波器(EKF)估计的姿态。导航系统从其他传感器组件中选择传感器信号,并与来自惯性导航模块的估计值结合处理选定的传感器信号,以获得更准确的姿态估计值。可以基于车辆的特性和配置来调整用于使用某些传感器信号的参数和条件。

著录项

  • 公开/公告号US8065074B1

    专利类型

  • 公开/公告日2011-11-22

    原文格式PDF

  • 申请/专利权人 DARREN S. LICCARDO;

    申请/专利号US20080206566

  • 发明设计人 DARREN S. LICCARDO;

    申请日2008-09-08

  • 分类号G01C21/00;

  • 国家 US

  • 入库时间 2022-08-21 17:26:08

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