Patrol aircraft safety control system

Abstract

The invention relates to a patrol aircraft safety control system, which comprises a ground control device, an emergency air bag device, an aircraft and a main control chip and a slave control chip for controlling the aircraft, wherein the aircraft is provided with an image acquisition unit, a flight control unit, a wireless transmitting and receiving device and a memory electrically connected with the main control chip respectively; the ground control device comprises a wireless transmitting and receiving module, an aircraft remote control module and a flight path module; the aircraft is also provided with a speed sensor, a GPS positioning device, a six-axis inertial sensor and an ultrasonic sensor electrically connected with the input end of the slave control chip, and the output end of the slave control chip is electrically connected with a rotor control device, a speed reducing protection device, and a gas generating device. The aircraft can perform patrol automatically according to the made flight path, the aircraft reduces the speed once fault happens, the air bag can be ejected in time, and the process is safe and reliable.

Description

technical field [0001] The invention belongs to the field of aircraft safety control, in particular to a patrol aircraft safety control system. Background technique [0002] Inspection methods can be divided into manual inspection, manned helicopter inspection and aircraft inspection. Although manual inspection is the most commonly used inspection method, it has always had shortcomings such as slow efficiency and constraints of climate and geographical environment. Aircraft inspection is being widely researched and applied. , especially the high-efficiency feature of aircraft inspection, has more and more application value. At present, the inspection tasks for aerial vehicles are basically controlled by the ground personnel remotely and manually, which cannot be automatically operated, the efficiency is low, and it is difficult to apply to the real-time monitoring system. At the same time, the safety status of the aircraft in flight cannot be monitored. Once a failure occurs...

AI Technical Summary

Problems solved by technology

[0002] Inspection methods can be divided into manual inspection, manned helicopter inspection and aircraft inspection. Although manual inspection is the most commonly used inspection method, it has always had shortcomings such as slow efficiency and constraints of climate and geographical environment. Aircraft inspection is being widely researched and applied. , especially the high-efficiency feature of aircraft inspection, has more and more application value

At present, the inspection tasks for aerial vehicles are basically controlled by the ground personnel remotely and manually, which cannot be automatically operated, the efficiency is low, and it is difficult to apply to the real-time monitoring system. At the same time, the safety status of the aircraft in flight cannot be monitored. Once a failure occurs, It will inevitably lead to damage to the aircraft itself and damage to the equipment loaded on it, which will cause economic losses. At the same time, after the aircraft falls from a high altitude, it may also cause damage to personnel and other equipment on the ground.

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