Figure rocket launching safety locker based on MCU microprocessor control

Abstract

The invention provides a figure rocket launching safety locker based on MCU microprocessor control. The figure rocket launching safety locker comprises a controller, and an operation module, a launching control module, a communication module and a power supply module which are connected with the controller, and a shell for placing hardware equipment. The controller is an MCU microprocessor and isin communication connection with eahc module through UART. The controller is in two-way communication connection with the operation module, the launching control module and the communication module; the power supply module supplies power to all other modules in a one-way manner; the launching control module comprises a digital delay tube rocket launch controller and a capacitor discharge type rocket launch controller. The ignition voltage is not greater than 80v; a safety locking function is integrated on a traditional rocket launching device, so that rocket launching by non-operators can be prevented, information such as launchers and launching conditions can be recorded and uploaded to a server, unified management is facilitated, and the launching authority of the device can be releasedin time through a remote instruction.

Description

technical field [0001] The invention relates to the field of aviation control equipment, in particular to a safety locker for launching a shadow rocket based on the control of an MCU microprocessor. Background technique [0002] With the continuous development of weather modification (hereinafter referred to as shadow) business, the number of shadow operation equipment and ammunition usage continues to increase, and there is always great pressure on safety management and control. The ability to actively prevent and control shadow safety risks needs to be improved. In order to implement the China Meteorological Administration's "Weather Modification "Cultivating Clouds" Action Plan (2020-2022)", people can actively prevent and control the safety risks of ground operations, and complete the meteorological small-scale construction project "Weather Modification Safety Technology Improvement Demonstration Project" with high quality Construction, the Emergency Disaster Mitigation ...

AI Technical Summary

Problems solved by technology

[0004] 1. The ignition voltage is too high (600V);

[0005] 2. There are no functions such as security lock (unlock with authorized password), satellite positioning, launch information collection and storage and upload server, communication and management with the command platform, and reserved communication interface;

[0006] 3. Illegal use by non-operators;

[0007] 4. Does not support the detection and launch of digital rockets, and cannot achieve backward compatibility

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