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Flight control method, device and aircraft

A flight control and aircraft technology, applied in the field of communications, can solve the problems of inability to effectively avoid obstacles, and the aircraft cannot pass through, so as to achieve the effect of obstacle avoidance

Pending Publication Date: 2018-01-26
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] During the flight, the aircraft can identify obstacles by means of radar or ultrasonic waves. For example, when the aircraft faces application scenarios such as windows or trees, the aircraft emits ultrasonic waves through the ultrasonic device and receives ultrasonic waves reflected by window frames or tree branches. Then the aircraft will Windows or woods are identified as obstacles, and then the aircraft is controlled to keep hovering, so that the aircraft cannot pass through windows or woods and other application scenarios, and obstacle avoidance cannot be effectively realized

Method used

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  • Flight control method, device and aircraft
  • Flight control method, device and aircraft
  • Flight control method, device and aircraft

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Embodiment Construction

[0045] The following will clearly and completely describe the technical solutions in the embodiments of the present disclosure with reference to the accompanying drawings in the embodiments of the present disclosure. Apparently, the described embodiments are only some of the embodiments of the present disclosure, not all of them. Based on the embodiments in the present disclosure, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present disclosure.

[0046] The embodiment of the present disclosure provides a flight control method, please refer to figure 1 , figure 1 It is a schematic flowchart of a flight control method provided in an embodiment of the present disclosure. As shown in the figure, the flight control method in the embodiment of the present disclosure may at least include:

[0047] S101. Determine a reference object in the flight environment where the aircraft is located.

[0...

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Abstract

Provided are a flight control method, a device and an aircraft. The flight control method is applied to the aircraft. The method includes the steps of: determining a reference object (S101) in a flight environment where the aircraft is located; acquiring a distance (S102) between the aircraft and the reference object; obtaining a flight strategy (S103) corresponding to the distance according to the pre-established corresponding relation between the distance, which is between the aircraft and the reference object, and the flight strategy; controlling the aircraft to fly (S104) based on the flight strategy; and realizing effective obstacle avoidance by using the flight control method, the apparatus and the aircraft.

Description

[0001] The disclosure of this patent document contains material that is protected by copyright. This copyright belongs to the copyright owner. The copyright owner has no objection to the reproduction by anyone of the patent document or the patent disclosure as it exists in the official records and files of the Patent and Trademark Office. technical field [0002] The present disclosure relates to the technical field of communication, and in particular to a flight control method, device and aircraft. Background technique [0003] During the flight, the aircraft can identify obstacles by means of radar or ultrasonic waves. For example, when the aircraft faces application scenarios such as windows or trees, the aircraft emits ultrasonic waves through the ultrasonic device and receives ultrasonic waves reflected by window frames or tree branches. Then the aircraft will Windows or woods are recognized as obstacles, and then the aircraft is controlled to keep hovering, so that th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
CPCG05D1/101G08G5/0021G08G5/0078G08G5/045B64U2101/30B64U2201/20B64U20/87G05D1/106
Inventor 周游谢鹏杜劼熹
Owner SZ DJI TECH CO LTD
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