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An Image-Based High-Precision Barrel Angle Measuring Device

A measuring device and high-precision technology, applied in the direction of measuring devices, optical devices, instruments, etc., to achieve the effects of short measurement time, solving measurement problems, and strong environmental adaptability

Active Publication Date: 2019-12-24
BEIJING CHANGCHENG INST OF METROLOGY & MEASUREMENT AVIATION IND CORP OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is: in order to solve the problem of quickly and accurately measuring the initial angle of the navigation device, the present invention proposes an image-based high-precision cylinder bullet angle measuring device

Method used

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  • An Image-Based High-Precision Barrel Angle Measuring Device
  • An Image-Based High-Precision Barrel Angle Measuring Device
  • An Image-Based High-Precision Barrel Angle Measuring Device

Examples

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Embodiment Construction

[0015] Below in conjunction with accompanying drawing and implementation example the present invention is further described: the terminal reference drawing-out device of this device is installed on the bomb locking device of missile body, and the bomb locking device is fixedly installed on the afterbody of missile body. Due to the error caused by processing and assembly, the angle between the guide buttons on both sides of the body tail and the centerline of the two positioning pins on the lock will deviate from the design value. To solve this problem, a three-coordinate measuring machine can be used to measure each The included angle of the bullet, the introduced offset angle α 1 The position of the guide button of the projectile can be determined by measuring the position of the positioning pin on the upper tail of the spring lock. The guide button of the projectile is equipped with a pin hole. The small photogrammetry code disc is installed on the guide button reference lead...

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Abstract

The invention provides an image-based high-precision cylinder and bullet angle measuring device. A tail end reference leading-out device is installed on a bullet locking device at the tail end of a bullet body of the device, and used for leading out non-measurable reference on the two bullet bodies after a guide button is assembled. A bullet cylinder reference leading-out device is installed on the end face of a double-helix guide rail at the front end of the bullet cylinder, and is tightly attached to the inner side face of the double-helix guide rail through double pins installed on the bullet cylinder reference leading-out device, so that the bullet cylinder reference which is not visible in the bullet cylinder is led out. A single CCD is sequentially focused on the bullet cylinder reference leading-out device and the tail end reference leading-out device through a zoom lens, so as to obtain large and small photography measurement coded disc images. Coding line identifying angles onthe large and small photography measurement coded discs, point angle and point coordinates are extracted. Distortion elimination process is carried out, the rotation matrix before and after rotationof an angle point target through an optimal fitting method, and the initial angle of a missile directional navigation device can be accurately obtained.

Description

[0001] Technical field [0002] The invention is an image-based high-precision cylinder projectile angle measuring device, which belongs to the field of geometric quantity detection in the production of weapons and equipment, and can directly measure the rotation angle of a projectile body along a threaded track in a launch tube with a helical track. Background technique [0003] The projectile launch track with a helix can only be used after being placed for a long time, which requires the inertial navigation component to have an extremely low zero deflection rate. Affected by zero bias factors, the accuracy of long-term directional navigation devices such as fiber optic gyroscopes is not satisfactory. Before the weapon leaves the factory, from the perspective of the system, under the condition that the accuracy of the directional navigation device is certain, by reasonably establishing the error model of the accelerometer and gyroscope, and designing an effective filter, the...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01B11/26
CPCG01B11/26
Inventor 孙安斌马骊群甘晓川曹铁泽王继虎李洋高廷邹志樊晶晶
Owner BEIJING CHANGCHENG INST OF METROLOGY & MEASUREMENT AVIATION IND CORP OF CHINA
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