Wing-deformation-based control mechanism of hummingbird-imitation flapping-wing unmanned aerial vehicle

A technology of unmanned aerial vehicle and control mechanism, which is applied in the direction of aircraft, aircraft control, aircraft parts, etc., can solve the problems of lack of control mechanism, inability to achieve full attitude control, and inability to generate a large enough torque control angle to achieve the effect of light weight

Pending Publication Date: 2020-01-03
NANKAI UNIV
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  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

[0005] A large part of existing research and inventions cannot realize the full attitude control of the three degrees of freedom of pitch, roll and y

Method used

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  • Wing-deformation-based control mechanism of hummingbird-imitation flapping-wing unmanned aerial vehicle
  • Wing-deformation-based control mechanism of hummingbird-imitation flapping-wing unmanned aerial vehicle
  • Wing-deformation-based control mechanism of hummingbird-imitation flapping-wing unmanned aerial vehicle

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Embodiment Construction

[0027] The following content is a specific implementation manner of the present invention, but this manner does not limit the present invention itself in any form. It is worth pointing out that within the framework of the core content of the present invention, improvements to the partial details or specific implementation of the present invention still belong to the scope of protection of this patent.

[0028] The present invention will be described in more detail below in conjunction with the accompanying drawings.

[0029] Such as figure 1 and figure 2 Shown based on the control mechanism of the imitation hummingbird flapping wing UAV based on wing deformation, the control mechanism includes a rotating steering gear base 11 (see the specific structure Figure 7 ) and the rotating steering gear 10 fixed on it, this part is connected with the flapping wing driving mechanism through 4 cylindrical holes at the bottom, a rotating steering gear rocker arm 9 is respectively fixe...

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Abstract

The invention discloses a wing-deformation-based control mechanism of a hummingbird-imitation flapping-wing unmanned aerial vehicle. The control mechanism comprises linear steering engines, a rotary steering engine, a linear steering engine base, a rotary steering engine base, wing joints, steering engine pull rods, semi-cylindrical fasteners, rotary steering engine rocker arms, wing root carbon rods, a wing joint main shaft carbon rod, a rotary steering engine control carbon rod and other parts, wherein the main body parts are obtained through a 3D printing processing mode by using resin or nylon materials, and the mass is very light; the two linear steering engines and the one rotary steering engine are utilized, so that the full-attitude control of the 3 degrees of freedom of pitch, roll and yaw is achieved; and on the basis of realizing full-attitude control, the large pitch, roll and yaw control angle is generated through the structural optimization design, so that the very important significance for controlling the attitude of a prototype in the hovering flight state is achieved, and a foundation for the subsequent design of a lightweight and compact flapping-wing prototype is provided.

Description

technical field [0001] The invention relates to a control mechanism of a bionic aircraft, which belongs to the technical field of unmanned aerial vehicles or the field of robots. Background technique [0002] In recent years, with the vigorous development of bionic research and the increasing demand for UAVs in domestic and foreign markets, research on flapping-wing unmanned aerial vehicles has attracted more and more attention. Compared with common fixed-wing and rotary-wing aircraft, the flapping-wing unmanned aerial vehicle has significant advantages such as high efficiency, light weight, strong maneuverability, and low energy consumption, and has a wide range of application prospects, especially in the military field. host. [0003] In the design of the flapping-wing unmanned aerial vehicle, the design of the control mechanism is a very important part. In the design of the control mechanism, there are mainly two control methods: the control method based on changing the...

Claims

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Application Information

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IPC IPC(8): B64C33/00B64C9/00
CPCB64C33/00B64C9/00
Inventor 方勇纯李友朋钱辰
Owner NANKAI UNIV
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