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Method of determination of the parameters of the inertial navigation of a carrier and the inertial navigation.

机译:确定载体的惯性导航和惯性导航的参数的方法。

摘要

Method of determining the parameters of the inertial navigation of a carrier, comprising the steps of: - embodiment of the inertial measurements (s1) of movement of the carrier, the measurements which may include inertial errors, - estimation (s2) of a state comprising the parameters of the inertial navigation and the inertial errors, the method being characterized in that it comprises the following steps implemented when the wearer moves on a substantially planar surface, an uncertainty on the flatness is limited by an upper limit (δ) known: - comparison (s3) of a parameter of navigation according to the vertical component with a predetermined auxiliary data item (y), - determination (s4) of a lack of precision (r) associated with said auxiliary data item (y) as a function of the upper limit (δ) which is known, and resetting) - (s5 of the state as a function of the comparison (s3) and the inaccuracy (r).
机译:确定载体的惯性导航的参数的方法,包括以下步骤:-载体运动的惯性测量(s1)的实施方式,所述测量可以包括惯性误差,-状态的估计(s2),包括:惯性导航的参数和惯性误差,该方法的特征在于,该方法包括以下步骤:当佩戴者在基本平坦的表面上移动时,平坦度的不确定性受到已知的上限(δ)的限制:-根据垂直分量将导航参数与预定的辅助数据项(y)进行比较(s3),-确定(s4)与所述辅助数据项(y)相关联的精度(r)不足,取决于已知的上限(δ)并进行重置)-(状态的s5作为比较(s3)和不准确性(r)的函数。

著录项

  • 公开/公告号FR2944867B1

    专利类型

  • 公开/公告日2011-04-22

    原文格式PDF

  • 申请/专利权人 SAGEM DEFENSE SECURITE;

    申请/专利号FR20090052680

  • 发明设计人 SIMON GAVILLET;

    申请日2009-04-24

  • 分类号G01C21/16;G01C25/00;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:57

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