A human shadow rocket launch safety detection and ignition control system and method

By designing an integrated human shadow rocket launch safety detection and ignition control system, and using microcontroller units to jointly control resistance detection and ignition control, the problems of high complexity and low detection efficiency of traditional systems are solved, high-precision detection and rapid ignition control are achieved, and the safety and reliability of rocket launch are improved.

CN119178353BActive Publication Date: 2025-03-25CHENGDU ZHENGYANG BOCHUANG ELECTRONIC TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202411686423.3
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-11-25
Publication Date
2025-03-25
Estimated Expiration
2044-11-25

AI Technical Summary

Technical Problem

The traditional human shadow rocket launch safety detection and launch control system has problems such as high complexity, high failure rate, high maintenance cost, low degree of automation, low detection efficiency and accuracy, and lacks real-time and dynamic monitoring methods, which poses great safety hazards.

Method used

A safety detection and ignition control system for launching a figure rocket is designed, using rocket resistance detection unit, ignition control unit, microcontroller unit and common cable. Through the coordinated control of the resistance detection unit and ignition control unit by the microcontroller unit, high-precision detection of rocket resistance and seamless switching of fast boost ignition control under a single line and interface are achieved.

Benefits of technology

It improves the safety and reliability of rocket launches, simplifies system design, reduces failure rate, improves overall work efficiency, and ensures the reliability and safety of the ignition system.

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Abstract

The present invention relates to the technical field of rocket launch safety detection and ignition control, and in particular to a human shadow rocket launch safety detection and ignition control system and method, including a rocket resistance detection unit, an ignition control unit, a microcontroller unit, a common cable, and a detection / ignition two-in-one interface. The microcontroller unit is responsible for processing resistance detection data and controlling the boost ignition process. The microcontroller unit includes a plurality of control ports, and the effective switching of the reference signal source is achieved by controlling the signal relay of the detection switching circuit. The switched reference source signal is connected to the common cable, and the ignition contact of the human shadow rocket is connected through the detection / ignition two-in-one interface to form a rocket resistance sampling loop, thereby detecting the resistance of the human shadow rocket. The present application has the effect of improving the safety and reliability of rocket launches and improving overall work efficiency.
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