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Automatic propeller stopping control system and method of unmanned aerial vehicle and unmanned aerial vehicle

A control method, UAV technology, applied in attitude control, aircraft power transmission, power plant on aircraft, etc., can solve problems such as difficulty and coordination problems

Pending Publication Date: 2021-09-07
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, two-person operation requires additional human assistance and may present coordination issues
It is too difficult and dangerous for a single person to operate. When the drone is too heavy or too large, it cannot be grasped with one hand

Method used

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  • Automatic propeller stopping control system and method of unmanned aerial vehicle and unmanned aerial vehicle
  • Automatic propeller stopping control system and method of unmanned aerial vehicle and unmanned aerial vehicle
  • Automatic propeller stopping control system and method of unmanned aerial vehicle and unmanned aerial vehicle

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Embodiment Construction

[0030] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0031] see figure 1 , is a drone 100 provided in an embodiment of the present invention. Such as figure 2 As shown, the drone 100 includes a control system 20 and a power device 30 . The control system 20 is used for controlling the power unit 30 to automatically stop rotating when an abnormality of the UAV 100 is detected, thereby controlling the UAV 100 to stop propellers. In this embodiment, the control system 20 includes at least one sensor device 21 and a ...

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Abstract

The invention provides an automatic propeller stopping control system and method for an unmanned aerial vehicle, which are applied to the unmanned aerial vehicle. The control system comprises a sensor device and a flight control device electrically connected with the sensor device. The sensor device is used for detecting at least one of flight parameters and flight attitudes of the unmanned aerial vehicle. And the flight control device is used for analyzing at least one of the flight parameters and the flight attitude detected by the sensor device, and generating a control signal for controlling a power device of the unmanned aerial vehicle to stop rotating when an analysis result of the at least one of the flight parameters and the flight attitude is abnormal. The control system can trigger the unmanned aerial vehicle to stop propellers according to the abnormal flight parameters and / or the abnormal flight attitude of the unmanned aerial vehicle in the flight and recovery process of the unmanned aerial vehicle, and the situation that the unmanned aerial vehicle transversely moves in the falling process and even falls in an accelerated mode after being overturned is avoided.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an automatic propeller stop control system and control method of an unmanned aerial vehicle and an unmanned aerial vehicle. Background technique [0002] Current UAVs include fixed-wing UAVs and rotary-wing UAVs with rotors that can take off and land vertically. For rotor UAVs, the propellers are generally driven by corresponding motors to rotate, thereby generating different magnitudes of pulling force to make the UAV take off, fly or land. [0003] UAVs need to maintain a stable attitude when flying in the air. When the UAV's attitude is out of balance due to collision with obstacles, excessive wind speed or mechanical failure, it will cause the UAV to lose control. At this time, if the UAV is within the visible range, experienced pilots can judge whether the UAV cannot return to a safe flight state by observing the UAV's attitude, flight speed, and flight hei...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G05D1/10
CPCB64D35/00B64D45/00
Inventor 霍达君周群威杨豪白高平
Owner SZ DJI TECH CO LTD
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