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Missile launching position and aiming shaft included angle deviation detection device and method

A technology for missile launch and deviation detection, which is applied in the direction of measuring devices, optical devices, angle/taper measurement, etc., can solve the problems that affect the detection accuracy and certain requirements for detection distance, achieve good test results, simple structure, and improve work efficiency effect

Pending Publication Date: 2019-11-26
CHANGCHUN SHIKAI TECH IND CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem that the detection distance in the prior art has a certain requirement and affects the detection accuracy, the present invention proposes a device and a detection method for detecting the angle deviation between the launch position of the missile and the aiming axis

Method used

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  • Missile launching position and aiming shaft included angle deviation detection device and method
  • Missile launching position and aiming shaft included angle deviation detection device and method
  • Missile launching position and aiming shaft included angle deviation detection device and method

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Embodiment Construction

[0021] Such as figure 1 As shown, the device for detecting the angle deviation between the launch position of the missile and the aiming axis includes three parts: a guide rail 1 , a collimator 2 and two parallel optical axis detectors 3 .

[0022] Such as figure 2 As shown, the guide rail 1 includes a board 1-1 and a support frame 1-2, and the support frame 1-2 is fixed on the board 1-1 by two M5 screws.

[0023] Such as image 3 As shown, the collimator 2 includes an objective lens 2-1, a reticle 2-2, a housing 2-3 and a bracket 2-4. The objective lens 2-1 and the reticle 2-2 are arranged in the casing 2-3, and the reticle 2-2 is arranged at the focal plane of the objective lens 2-1. The upper end of the support 2-4 is fixed on the housing 2-3, and the lower end is fixed on the plugboard 1-1.

[0024] The inserting board 1-1 is a wedge-shaped structure with an angle α between the bottom reference plane and the upper plane. The α angle is the same as the missile launch ...

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Abstract

A missile launching position and aiming shaft included angle deviation detection device and method belong to the technical field of optical integrated detection. In order to solve a problem in the prior art, a support frame is fixed at one end of a plugboard. An objective lens and a reticle are arranged in a shell, and the reticle is arranged on a focal plane of the objective lens. An upper end ofthe support frame is fixed on the shell, and a lower end is fixed on the plugboard. A hand wheel pressing ring is connected to one end of a flange plate which is fixed in the support frame. The otherend of the flange plate is connected to a main shell. A light through hole in a side surface of the upper portion of the main shell is aligned with an inner hole of the flange plate. A roof prism isarranged in the main shell and fixed to a roof prism base. An axial end surface of the roof prism is pressed through a roof prism pressing ring, and a roof prism base pressing ring is pressed at an upper end of the roof prism base. A right-angle prism is arranged in a right-angle prism frame and is integrally fixed with a right-angle prism pressing ring through a right-angle prism space ring, anda whole body is arranged in the lower end of the main shell. The light through hole of the right-angle prism frame is aligned with the light through hole of the main shell.

Description

technical field [0001] The invention relates to a device and a detection method capable of detecting the angle deviation between a missile launch position and an aiming axis, and belongs to the technical field of optical integrated detection. Background technique [0002] The angle deviation of the missile launch position relative to the aiming axis of the missile weapon system directly affects the initial position of the missile axis and aiming when the missile is launched. If the two satisfy the theoretical angle position, the missile can be located within the range of the missile control field, which is conducive to the timely and effective tracking and guidance of the missile by the launch guidance device, which is an important factor affecting the missile hit rate. [0003] The angle between the launch position of the missile weapon system relative to the aiming axis directly affects the initial position of the missile axis and the aiming when the missile is launched. F...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B5/24G01B11/26F42B35/02
CPCG01B11/26G01B5/24F42B35/02
Inventor 王杰王继奎李娜李彦沈长亮徐椿明彭刚张兴迪
Owner CHANGCHUN SHIKAI TECH IND CO LTD