Calibration system and calibration method suitable for on-missile inertial assembly of small-sized guided missile

A technology for calibrating systems and missiles, which is applied in the direction of measuring devices and instruments, can solve the problems that restrict the mass application of small guided missiles, the difficulty of missile maintenance, and the complicated implementation process, and achieve high test efficiency, low maintenance difficulty, and measurement accuracy high effect

Active Publication Date: 2019-08-30
西安航天三沃机电设备有限责任公司
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  • Summary
  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

This calibration method is difficult to implement, the implementation process is complicated, and there are unavoidable safety hazards in the process of missile disassembly
The above problems make missile maintenance difficult and restrict the mass application of small guided missiles

Method used

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  • Calibration system and calibration method suitable for on-missile inertial assembly of small-sized guided missile
  • Calibration system and calibration method suitable for on-missile inertial assembly of small-sized guided missile
  • Calibration system and calibration method suitable for on-missile inertial assembly of small-sized guided missile

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Embodiment Construction

[0024] In order to make the objects, features and advantages of the present invention more comprehensible, specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0025] Such as figure 1 , figure 2 with image 3 As shown, a calibration system suitable for inertial components on small guided missiles, including a test platform, joint robot, fixture, remote control cabinet, a set of video monitoring system, a set of host computer for man-machine communication,

[0026] Wherein the test platform 5 and the joint robot 9 are fixed on the base plate 6, the front and rear ends of the measurement platform 5 are provided with a V-shaped support 4, and a limit mechanism 10 is arranged behind the rear end V-shaped support 4; the camera bracket 1 is connected with the measurement platform 5 Fixed, the monitoring camera 2 is installed on the camera bracket 1; a clamp 7 is installed at the front end of the arm of th...

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Abstract

The invention discloses a calibration system and a calibration method suitable for an on-missile inertial assembly of a small-sized guided missile. The calibration system comprises a joint robot, a clamp, a test platform, a remote control cabinet and the like, wherein the joint robot can clamp and fix a tested missile through the special clamp, and the remote control cabinet controls the joint robot to grab the tested missile to reach different positions and postures; at the same time, the joint robot is provided with an angle reference, and test and calibration of the on-missile inertial assembly are realized through comparison between the angle reference and output of the inertial assembly. The calibration system of the invention has the beneficial effects that: test and calibration of the on-missile inertial assembly can be completed under the whole missile condition, a stable, reliable, safe and convenient platform for test and calibration of the on-missile inertial assembly is provided, and the problem that a calibration process of the on-missile inertial assembly is complex at present is solved.

Description

technical field [0001] The invention relates to the technical field of special test equipment, in particular to a calibration system suitable for calibrating inertial components on small guided missiles. Background technique [0002] With the transformation of the world's military and the wide application of high and new technologies, the operational form and concept of modern warfare are changing, and the concept of war benefits based on "effects-based warfare" is gradually accepted by countries all over the world. Small-sized guided missiles have the advantages of small size, light weight, low combat implementation cost, and high hit accuracy. They are widely used in today's local wars, especially the anti-terrorist war, and have become the key development direction of relevant domestic scientific research units in recent years. [0003] Limited by factors such as cost and volume, most of the inertial components on the small guided missiles at this stage use MEMS inertial ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C25/00
CPCG01C25/005Y02P90/02
Inventor 王梦楠何志杰邙强郇光周陈伟袁莉崔天祥陈志刚
Owner 西安航天三沃机电设备有限责任公司
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