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Power system configuration method, device, unmanned aerial vehicle, server and user terminal

A configuration method and power system technology, applied in the field of unmanned aerial vehicles, can solve problems such as flight safety of unmanned aerial vehicles, thin atmosphere density, power system efficiency decline, etc.

Active Publication Date: 2021-07-20
SZ DJI TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For example, an unmanned aerial vehicle is equipped with a power system. When flying at location A, the efficiency of the power system is relatively high. If the unmanned aerial vehicle is replaced to fly at location B, the atmospheric density of location B is thinner than that of location A, and the propeller efficiency In order to provide enough lift, the propeller needs to increase the speed. The problems caused by increasing the speed include: the efficiency of the power system decreases, the controllability of the UAV decreases, and even the flight safety of the UAV

Method used

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  • Power system configuration method, device, unmanned aerial vehicle, server and user terminal
  • Power system configuration method, device, unmanned aerial vehicle, server and user terminal
  • Power system configuration method, device, unmanned aerial vehicle, server and user terminal

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Embodiment Construction

[0101] The technical solutions in the embodiments of the present invention will be clearly described below in conjunction with 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 making creative efforts belong to the protection scope of the present invention.

[0102] It should be noted that when a component is said to be "fixed" to another component, it can be directly on the other component or there can also be an intervening component. When a component is said to be "connected" to another component, it may be directly connected to the other component or there may be intervening components at the same time.

[0103] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood...

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Abstract

A method for configuring a power system, the method comprising: acquiring information about the environment where an unmanned aerial vehicle (100) is located; When the unmanned aerial vehicle is flying in the corresponding environment, the efficiency of the power system of the unmanned aerial vehicle (100) is relatively high, so as to avoid the power failure of the unmanned aerial vehicle (100) due to the mismatch between the power suit installed on the unmanned aerial vehicle (100) and the environment in which it is located. Decreased system efficiency and even flight safety issues. At the same time, a flight control device, an unmanned aerial vehicle, a server and a user terminal are respectively disclosed.

Description

technical field [0001] Embodiments of the present invention relate to the field of unmanned aerial vehicles, and in particular, relate to a power system configuration method and device, an unmanned aerial vehicle, a server, and a user terminal. Background technique [0002] The power system of the unmanned aerial vehicle in the prior art includes a motor, an electronic governor, and a propeller. The electronic governor controls the speed of the motor according to the throttle signal sent by the flight controller, and the motor drives the propeller to rotate. [0003] The efficiency of the power system is related to the parameters of the propeller, motor, and electronic governor, and also to the combination of the propeller, motor, and electronic governor. In addition, when the power system of the UAV is fixed, the efficiency of the power system will be affected by The influence of the environment where the UAV is located, such as atmospheric pressure, atmospheric density, at...

Claims

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Application Information

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IPC IPC(8): B64C13/16G05D1/10
CPCB64C13/16G05D1/102G05D1/10
Inventor 林灿龙商志猛
Owner SZ DJI TECH CO LTD
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