Method and device for controlling a drone

A UAV, opportunity technology, applied in control/regulation system, non-electric variable control, 3D position/channel control and other directions, can solve problems such as UAV self-crash, UAV crash, UAV safety hidden danger, etc.

Active Publication Date: 2021-09-07
BEIJING SANKUAI ONLINE TECH CO LTD +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

When these situations occur, the UAV will not only face the situation of self-crash, but also may collide with other flying UAVs under the influence of factors such as wind force and its own speed during the falling process. The chain reaction of a total of three drones crashing
In other words, when the UAV itself falls, it will bring great safety hazards to other UAVs, and this will also bring great cost pressure to the business performed by UAVs. Reduced efficiency of business execution
At the same time, the crash of multiple drones will also bring considerable safety hazards to pedestrians or vehicles on the road.

Method used

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  • Method and device for controlling a drone
  • Method and device for controlling a drone

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Embodiment Construction

[0055] In order to make the purpose, technical solution and advantages of this specification clearer, the technical solution of this specification will be clearly and completely described below in conjunction with specific embodiments of this specification and corresponding drawings. Apparently, the described embodiments are only some of the embodiments in this specification, not all of them. Based on the embodiments in this specification, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this specification.

[0056] The technical solutions provided by each embodiment of this specification will be described in detail below in conjunction with the accompanying drawings.

[0057] figure 1 It is a schematic flow diagram of a method for controlling a drone in this specification, including the following steps:

[0058] S101: Determine the interference UAV and the state data of the interference UAV, ...

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Abstract

This specification discloses a UAV control method and device, which can determine the interference UAV and the state data of the UAV, wherein the UAV needs to be controlled by a parachute installed on the UAV. Automatic forced landing. Then, according to the state data, the flight interference area corresponding to the interference drone can be determined, and according to the flight interference area, it can be determined whether the interference drone will cause interference to the driving of the target drone. The human-opportunity will interfere with the driving of the target UAV. According to the flight interference area, the route of the target UAV can be re-planned, the target route can be obtained, and the target UAV can be driven according to the target route, so as to ensure the safety of the target UAV. Drive safely, reduce the cost of business execution based on the target UAV, and improve the efficiency of business execution based on the target UAV.

Description

technical field [0001] This specification relates to the field of unmanned driving, in particular to a method and device for controlling a drone. Background technique [0002] With the development of unmanned driving technology, drones can gradually be applied to various fields. For example. UAVs can be used for aerial photography, and for example, UAVs can be used for food delivery. Another example is high-altitude fire fighting by drones. It can be seen that the application of drones in various fields provides great convenience for people's daily life and improves the efficiency of business execution. [0003] In practical applications, drones may encounter situations such as motor failure, lightning strikes, and signal failures that cannot control their own flight during flight. When these situations occur, the UAV will not only face the situation of self-crash, but also may collide with other flying UAVs under the influence of factors such as wind force and its own s...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 张继伟张邦彦眭泽智黄金鑫寻其锋
Owner BEIJING SANKUAI ONLINE TECH CO LTD
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