首页> 外国专利> METHOD AND EQUIPMENT FOR SETTING INITIAL COORDINATE VALUES OF INERTIA DETECTING MEANS OF MOVING BODY

METHOD AND EQUIPMENT FOR SETTING INITIAL COORDINATE VALUES OF INERTIA DETECTING MEANS OF MOVING BODY

机译:设定运动物体惯性检测装置初始坐标值的方法和设备

摘要

PURPOSE: To set initial coordinate values of navigation of an inertia detecting means of a moving body by a method wherein motion of shaking, rotation or the like is given to a moving body from a moving parent body, the motion is detected by the inertia detecting means of the moving body and the moving parent body and a detected value of the moving body is corrected with the detected value of the moving parent body used as a reference. ;CONSTITUTION: Acceleration is given to an inertial navigation system (MINS) 18 of a missile by shaking or rotating a missile launcher 10 intentionally, and this acceleration is detected by an accelerometer which the MINS 18 has. An inertial navigation system (SINS) 12 is installed in the vicinity of the center of shaking or rotation of the launcher and it can measure the acceleration of the launcher precisely. Based on a detected value of the SINS 12, accordingly, an acceleration vector at the time of roll to be detected at the position of the MINS 18 can be obtained by computation precisely from the relative positional relationship between the SINS 12 and the MINS 18. Three orthogonal coordinate axes of acceleration vectors of the SINS 12 and the MINS 18 thus obtained are compared and a difference value of each coordinate axis is set correctively in the MINS 18 as a corrective value for the MINS 18 and stored therein as an initial coordinate value. Using as references the coordinate values thus obtained, the missile 16 can fly to a target point correctly from a warship 10.;COPYRIGHT: (C)1994,JPO&Japio
机译:目的:通过一种方法来设置移动物体的惯性检测装置的导航的初始坐标值,该方法是从移动的母体向移动物体施加摇动,旋转等运动,通过惯性检测来检测运动利用移动体和移动母体的检测手段,以移动母体的检测值作为基准来校正移动体的检测值。组成:通过有意地摇动或旋转导弹发射器10,对导弹的惯性导航系统(MINS)18进行加速,并且该加速度由MINS 18所具有的加速度计检测。惯性导航系统(SINS)12安装在发射器的摇动或旋转中心附近,它可以精确地测量发射器的加速度。因此,基于SINS 12的检测值,可以通过精确地从SINS 12与MINS 18之间的相对位置关系进行计算,来获得在MINS 18的位置处要检测的侧倾时的加速度矢量。比较由此获得的SINS 12和MINS 18的加速度矢量的三个正交坐标轴,并且在MINS 18中校正地设置每个坐标轴的差值作为MINS 18的校正值,并且将其存储为初始坐标值。 。使用这样获得的坐标值作为参考,导弹16可以从军舰10正确地飞行到目标点。版权所有:(C)1994,JPO&Japio

著录项

  • 公开/公告号JPH0611354A

    专利类型

  • 公开/公告日1994-01-21

    原文格式PDF

  • 申请/专利权人 MITSUBISHI PRECISION CO LTD;

    申请/专利号JP19920170764

  • 发明设计人 TAKAGI HIROSHI;MATSUMOTO SHINSUKE;

    申请日1992-06-29

  • 分类号G01C21/16;G01C25/00;

  • 国家 JP

  • 入库时间 2022-08-22 04:53:05

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