Flexible rocket projectile guidance cabin physical quantity testing system

A test system and guidance cabin technology, which is applied in the direction of ammunition testing, ammunition, measuring devices, etc., can solve the problems of centroid measuring equipment and centroid measuring methods that do not meet the needs of factory development and waste of resources, and achieve convenient and fast printing and simple operation. Convenient and cost-effective effect

Active Publication Date: 2021-05-04
NORTH NAVIGATION CONTROL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The technical problem to be solved by the present invention is how to provide a flexible rocket guidance cabin physical quantity testing system to solve the problems that the existing centroid measurement equipment and centroid measurement method do not meet the development needs of the factory, resulting in waste of resources, etc.

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  • Flexible rocket projectile guidance cabin physical quantity testing system
  • Flexible rocket projectile guidance cabin physical quantity testing system
  • Flexible rocket projectile guidance cabin physical quantity testing system

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Embodiment Construction

[0050] In order to make the purpose, content and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0051] The flexible rocket guidance cabin physical quantity automatic test system can measure the center of mass, height and weight of three types of rocket guidance cabin products, such as penetrating bombs, cluster bombs, killing bombs, and cloud bombs.

[0052] Through the design of software control and mechanical mechanism, the automatic measurement, calculation and information output of products are realized. Just place the product in the corresponding position, the measurement process does not require manual operation and recording, and the equipment can automatically determine the measurement results. Generate test information packets, realize seamless connection with information systems, effectively solve end-to...

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Abstract

The invention relates to a flexible rocket projectile guidance cabin physical quantity testing system, and belongs to the field of automatic testing. Through cooperative control of software and a mechanical structure, a front supporting mechanism can be automatically replaced according to the model of a tested product. Through cooperation of the mechanical structure and software control, the system can realize automatic selection of the front supporting mechanism according to the model of a tested product. A rotation alignment mechanism is controlled by a limiting sensor, and the mechanical structure design of the front supporting mechanism, a rear supporting mechanism and a limiting mechanism is combined, so that the product axis and a supporting table top are always kept horizontal in the testing process, and the testing precision is ensured. The system can realize simultaneous automatic testing of three physical quantities of mass center, weight and height of a plurality of rocket projectile guidance cabin products. According to the invention, the product carrying is reduced, the test time is shortened, and higher economic benefits are generated.

Description

technical field [0001] The invention belongs to the technical field of automatic testing, and in particular relates to a physical quantity testing system of a flexible rocket guidance cabin. Background technique [0002] The center of mass is an inherent characteristic of missiles. High-precision mass and center of mass positions can reduce the difficulty of missile control during flight, and are an important guarantee for improving the success rate and hit rate of missile flight tests. As an important subsystem of the rocket weapon system, the guidance module must not only meet the electrical performance requirements, but also ensure the accuracy of the processing and assembly of the guidance module. Therefore, the detection and analysis of the quality and center of mass parameters of the guidance cabin is an important link in the development and production of the guidance cabin. [0003] Most of the existing guidance cabin mass center of mass measurement systems are dedic...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01D21/02F42B35/00
CPCG01D21/02F42B35/00
Inventor 王武周寅车新宇李猛田文静于飞杨勇崔萌萌
Owner NORTH NAVIGATION CONTROL TECH
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