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HYBRID INERTIAL NAVIGATION SYSTEM AND METHOD FOR DETERMINING INERTIAL NAVIGATION PARAMETERS BASED ON A KINEMATIC MODEL

机译:基于运动学模型的混合惯性导航系统及惯性导航参数的确定方法

摘要

The invention concerns a method for improving determination of inertial navigation parameters (1) of a carrier (1) moving along modelizable kinematic movement components, the method including the following steps: (a) selecting, taking into account a kinematic model (13) of the carrier (1), at least one movement component whereby integration (11) of the inertial measurements (20) is assumed to give a predetermined value, (b) integrating (11) the inertial measurements (20) in accordance with the selected component(s), (c) determining (14) based on the component(s) a variation between the integration (11) obtained at step (b) and the predetermined value of step (a), (d) estimating on the basis of the variation(s) thus obtained a global inertial error resulting from inertial errors associated with said modelizable components, and values to be updated of variable parameters of the kinematic model (13), (e) correcting said inertial navigation based on the thus determined global inertial error. The invention also concerns an inertial navigation system for implementing said method.
机译:本发明涉及一种用于改进对沿着可建模运动学运动分量运动的载体(1)的惯性导航参数(1)的确定的方法,该方法包括以下步骤:(a)考虑到运动模型(13)来选择载体(1),至少一个运动分量,从而假定惯性测量值(20)的积分(11)给出一个预定值,(b)根据所选分量对惯性测量值(20)进行积分(11) (s),(c)根据组件确定(14)步骤(b)中获得的积分(11)与步骤(a),(d)的预定值之间的变化,并基于因此,所述变化获得了由与所述可建模的组件相关联的惯性误差引起的全局惯性误差,以及运动模型(13)的可变参数的待更新值,(e)基于由此确定的整体来校正所述惯性导航惯性误差河本发明还涉及用于实施所述方法的惯性导航系统。

著录项

  • 公开/公告号IL183755B

    专利类型

  • 公开/公告日2012-11-29

    原文格式PDF

  • 申请/专利权人 SAGEM DEFENSE SECURITE;

    申请/专利号IL183755

  • 发明设计人

    申请日2007-06-07

  • 分类号G01Cnull/null;

  • 国家 IL

  • 入库时间 2022-08-21 16:41:37

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