首页> 外国专利> A non-contact type attitude measurement system for three axis simulator

A non-contact type attitude measurement system for three axis simulator

机译:用于三轴模拟器的非接触式姿态测量系统

摘要

The present invention is non-contact 3-axis simulator for the precise measurement of the position of the 3-axis attitude control rocket simulator relates to a position measuring system. The present invention includes the coordinate plate are laser pointer is displayed; Camera to measure the image of the laser pointer indicated above; And wherein in use the image information obtained by the camera position and attitude of the object of the conventional non-contact type comprising a computer for calculating the position measuring system, the object is in the air unit and the air form the ball bearing, the rotation axis on the air bearing ball connected to the simulator, and the pitch axis consists of three laser pointers are fixed rest simulators installed, John shaft, and air bearing system that is rotated in the roll axis, three-axis, the coordinate axis of rotation and the outer plate is the air bearing ball in the air bearing system match to be installed in the same direction and the color is painted in two different colors so as to facilitate the measurement coordinates when obtaining image information by the camera, the camera is mounted outside the air bearing system forming the three laser pointer on the coordinate plate measuring the image of a triangle, and wherein the computer is a pitch angle of the simulator in the obtained image is measured by the camera, yaw angle, but calculating the roll angle, pitch angle and the coordinates of the triangle formula , yaw angle and the coordinates of the triangle equation , the roll angle and the coordinates of the triangle equation The present invention is moved on the coordinate plate in the same motion as a laser pointer are also air bearing system with the air bearing system air bearing system is moved by the air cushion. The camera transmits the images to a computer to detect, process the image to be stored inside the computer calculates the current position and attitude of the simulator.
机译:本发明是一种用于精确测量3轴姿态控制火箭模拟器位置的非接触式3轴模拟器,涉及一种位置测量系统。本发明包括坐标板被激光指示器显示;相机测量上面指示的激光指示器的图像;并且其中,在使用中,通过包括具有用于计算位置测量系统的计算机的常规非接触型物体的照相机位置和姿态所获得的图像信息,该物体位于空气单元中并且空气由滚珠轴承构成,旋转轴上的空气轴承球连接到模拟器,并且俯仰轴由三个激光指示器组成,安装有固定的休息模拟器,约翰轴和空气轴承系统在滚动轴,三轴,坐标轴上旋转旋转,并且外板是与空气轴承系统中的空气轴承球匹配并以相同方向安装的,并且将颜色涂成两种不同的颜色,以便在通过摄像机获取图像信息时方便测量坐标,安装在空气轴承系统的外部,在坐标板上形成三个激光指示器,测量三角形的图像,其中计算机是模拟物体的俯仰角用照相机测量获得的图像中的指示器的偏航角,但是计算侧倾角,俯仰角和三角形公式的坐标,偏航角和三角形方程的坐标,侧倾角和三角形方程的坐标本发明在坐标板上以与激光指示器相同的运动运动,空气轴承系统也与空气轴承系统一起,空气轴承系统通过气垫运动。相机将图像传输到计算机进行检测,处理要存储在计算机内部的图像,计算出模拟器的当前位置和姿态。

著录项

  • 公开/公告号KR100617602B1

    专利类型

  • 公开/公告日2006-09-01

    原文格式PDF

  • 申请/专利权人

    申请/专利号KR20040108883

  • 发明设计人 전상운;최형돈;정호락;김지훈;

    申请日2004-12-20

  • 分类号G01C21/00;G01C21/20;

  • 国家 KR

  • 入库时间 2022-08-21 21:23:07

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