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
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[0031] Example 1:
[0032] This embodiment provides a rocket operation control and safety monitoring system and operation monitoring method. Refer to figure 1 The rocket operation control and safety monitoring system in this embodiment includes multiple 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 through mobile communication GPRS;
[0033] Refer to figure 2 , One of the work point acquisition control unit 1 consists of ignition controller 101, information transfer controller 102, collector 103, pitch and azimuth reader 104, rocket or shell identification device 105, electronic identification tag 106, launcher, Rocket composition; the rocket is installed on the launcher; the electronic identification tag 106 is installed on the rocket, the pitch and azimuth reader 104, and the rocket or shell identifica
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[0051] Example 2:
[0052] This embodiment provides an anti-aircraft artillery operation control and safety monitoring system and operation monitoring method. Refer to figure 1 , The anti-aircraft artillery operation control and safety monitoring system in this embodiment includes multiple operation point acquisition control units 1 and a host computer 2; the upper computer 2 and the operation point acquisition control unit 1 communicate through 3G;
[0053] Refer to figure 2 , One of the working point acquisition control unit 1 is composed of ignition controller 101, information transfer controller 102, collector 103, pitch and azimuth reader 104, shell identification device, electronic identification tag 106, antiaircraft artillery, and shells; The artillery shell is installed on the artillery; the electronic identity tag 106 is fixed on the artillery shell; the pitch and azimuth reader 104 and the artillery shell identification device are fixed on the artillery; the collector 103
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