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Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method

A security monitoring system, ignition controller technology, applied in the direction of the gun control system, weapon accessories, offensive equipment, etc., can solve the problem of inability to automatically collect operation information and upload operation information in real time, artificial weather modification operations cannot be unified management, Uncontrolled weather operations and other issues, to achieve the effect of simple installation, easy maintenance, and high degree of modularization

Active Publication Date: 2011-10-19
陕西中天火箭技术股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to overcome the problems that artificial weather modification operations of rockets and antiaircraft guns are not controlled, and cannot automatically collect operation information and upload operation information in real time, resulting in the inability to conduct unified management of artificial weather modification operations and difficult monitoring of operation safety, the present invention proposes a rocket, The antiaircraft artillery operation control and safety monitoring system and operation monitoring method are aimed at controlling the launch of rockets or antiaircraft artillery while automatically collecting information including launch pitch, azimuth, launch rocket or shell information, latitude and longitude coordinates of operating points, operating time, and operating bombs. Operation information such as quantity, operation channel number, ignition line resistance, etc., and upload the operation information to the management center for unified monitoring of operation safety

Method used

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  • Rocket and antiaircraft gun operation control and safety monitoring system and operation monitoring method

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Embodiment 1

[0032] This embodiment provides a rocket operation control and safety monitoring system and an operation monitoring method. refer to figure 1 , the rocket operation control and safety monitoring system in this embodiment includes a plurality of operation point acquisition control units 1 and a weather modification operation center management platform, namely the upper computer 2; the upper computer 2 and the operation point acquisition control unit 1 Data transmission between mobile communication GPRS;

[0033] refer to figure 2 , wherein one operating point acquisition control unit 1 is composed of an ignition controller 101, an information relay controller 102, a collector 103, a pitch and azimuth angle reader 104, a rocket or shell identification device 105, an electronic identity tag 106, a launcher, The rocket is composed; the rocket is installed on the launcher; the electronic identity tag 106 is installed on the rocket, the pitch and azimuth reader 104, and the rocke...

Embodiment 2

[0052] This embodiment provides an antiaircraft artillery operation control and safety monitoring system and operation monitoring method. refer to figure 1 , the antiaircraft gun operation control and safety monitoring system in this embodiment includes a plurality of operating point acquisition control units 1 and a host computer 2; the upper computer 2 and the operating point acquisition control unit 1 communicate through 3G;

[0053] refer to figure 2, one of the operating point acquisition control unit 1 is composed of an ignition controller 101, an information transfer controller 102, a collector 103, a pitch and azimuth reader 104, a shell identification device, an electronic identity tag 106, an antiaircraft gun, and a shell; The shell is installed on the anti-aircraft gun; the electronic identity tag 106 is fixed on the shell, and the pitch, azimuth reader 104 and the shell ID identifier are fixed on the anti-aircraft gun; the collector 103 reads the pitch , the inf...

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Abstract

The invention discloses a rocket and antiaircraft gun operation control and safety monitoring system and an operation monitoring method. The system comprises a plurality of operation point acquisition and control units 1 and an artificially-influenced weather operation central management platform, namely an upper computer 2, wherein data is transmitted between the upper computer 2 and the operation point acquisition and control units 1 through mobile communication and the Internet. The operation monitoring method comprises the following steps of: controlling the launching of a rocket or an antiaircraft gun; automatically acquiring operation information such as a launching pitch angle, a launching azimuth angle, rocket or antiaircraft gun launching information, longitude and latitude coordinates of operation points, operation time, operation ammunition using amount, operation channel numbers, ignition circuit resistance and the like; and uploading the operation information to a management center to monitor operation safety in a unified mode. By the system and the method, the problem of inaccurate information caused by manually recording and transmitting the operation information through personnel in the prior art is solved, and an effective tool is provided for a manager to accurately and timely master the information and scientifically perform artificially-influenced weather command and management.

Description

Technical field: [0001] The invention relates to the use of wireless communication, information collection and electronic identification technology to control the operation of rockets and anti-aircraft guns and monitor the process. While controlling the launch of rockets or anti-aircraft guns, the operation information of the launching process is automatically collected, and the information is wirelessly transmitted to the management team. The center is used for operation safety management, specifically rocket and antiaircraft gun operation control and safety monitoring systems and operation monitoring methods. Background technique: [0002] At present, the widely carried out artificial weather modification operation is completed by launching rockets or shells, launching rockets or shells through ignition controllers, launching pitch and azimuth angles by adjusting rocket launchers or antiaircraft gun barrels, rockets or shells, launchers or antiaircraft guns And the ignitio...

Claims

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Application Information

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IPC IPC(8): F41G5/02
Inventor 陈轶敏薛蔚罗永乐王心根张凯高新建姚梦涛王黎苏选强王金华王丹梁琼
Owner 陕西中天火箭技术股份有限公司
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