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A control method for a UAV capable of vertical take-off and landing

A technology of vertical take-off and landing and control method, which is applied in the direction of vertical take-off and landing aircraft, aircraft control, unmanned aircraft, etc. The effect of convenient take-off and landing, saving driving energy consumption

Active Publication Date: 2021-06-15
BEIJING UNIV OF CIVIL ENG & ARCHITECTURE
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Limited by the development of battery technology, the battery life of multi-rotor drones, high altitude, and long-distance performance are not good.
Traditional fixed-wing aircraft have the characteristics of heavy load and long endurance, but they have strict requirements for take-off conditions, and often require a long distance for taxiing
[0004] Existing fixed-wing aircraft that can take off and land vertically have single functions and insufficient battery life
However, fixed-wing UAVs have relatively large take-off and landing restrictions, are difficult to apply in a wide range, and cannot quickly carry various equipment, and the cost of use is high.

Method used

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  • A control method for a UAV capable of vertical take-off and landing
  • A control method for a UAV capable of vertical take-off and landing
  • A control method for a UAV capable of vertical take-off and landing

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Embodiment Construction

[0042] In order to make the purpose and technical solutions of the embodiments of the present invention more clear, the technical solutions of the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings of the embodiments of the present invention. Apparently, the described embodiments are some, not all, embodiments of the present invention. Based on the described embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0043] Those skilled in the art can understand that, unless otherwise defined, all terms (including technical terms and scientific terms) used herein have the same meaning as commonly understood by those of ordinary skill in the art to which this invention belongs. It should also be understood that terms such as those defined in commonly used dictionaries shoul...

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Abstract

A control method for an unmanned aerial vehicle capable of vertical take-off and landing. The invention controls the drone to operate in the vertical take-off and landing mode when it takes off and lands, and takes off or lands through the vertical take-off and landing system; The set fixed-wing propulsion device outputs driving force to drive the UAV to fly, saving driving energy consumption. The UAV control method provided by the present invention has lower energy consumption required for flight, and due to the setting of the vertical take-off and landing system, it can conveniently take off and land in a small space.

Description

technical field [0001] The invention relates to the field of flight equipment, in particular to a method for controlling an unmanned aerial vehicle capable of vertical take-off and landing. Background technique [0002] With the application of multi-rotor UAVs more and more widely, UAVs have begun to be well known. At the same time, unmanned aerial vehicles have begun to emerge in the civilian and commercial fields. But now all kinds of drones have their own advantages, and the advantages are different and have a single function. [0003] For example, multi-rotor drones, which are widely used at present, have the functions of vertical take-off and landing, hovering in the air, strong flexibility, and can complete flight tasks in a short distance range. Limited by the development of battery technology, the current multi-rotor UAVs have poor battery life, high altitude, and high long-distance performance. Traditional fixed-wing aircraft have the characteristics of heavy loa...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C27/26B64C27/28B64C29/00B64C19/00
CPCB64C27/26B64C27/28B64C29/00B64C19/00B64U10/25B64U30/10B64U2201/00B64U30/20B64U50/19B64U10/10B64U2101/00
Inventor 姚德臣孙强张骄武向鹏杨建伟刘恒畅寇子明
Owner BEIJING UNIV OF CIVIL ENG & ARCHITECTURE