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Four-rotor aircraft and control system thereof

A technology for a quadrotor aircraft and a control system, which is applied in the field of aircraft and can solve the problems of slow attitude adjustment and poor crosswind resistance.

Inactive Publication Date: 2016-10-12
周小勇
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Quadrotor aircraft has the advantages of vertical take-off and landing, hovering in the air, etc., and is widely used. However, the existing quadrotor aircraft changes the flying attitude of the aircraft in the air by adjusting the speed of the four rotors. It has poor crosswind resistance and slow attitude adjustment. and other defects

Method used

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  • Four-rotor aircraft and control system thereof
  • Four-rotor aircraft and control system thereof
  • Four-rotor aircraft and control system thereof

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Embodiment 1

[0034] Such as figure 1 As shown, the present embodiment provides a quadrotor aircraft, which includes a frame 1, a first shaft 11, a second shaft 21, a third shaft 31, a fourth shaft 41, a first rotor 12, a second rotor 22, The third rotor 32, the fourth rotor 42, the first rotor shaft 13, the second rotor shaft 23, the third rotor shaft 33 and the fourth rotor shaft 43; the first shaft 11, the second shaft 21, the third shaft 31 and one end of the fourth shaft 41 are installed on the frame 1 respectively, and the first shaft 11, the second shaft 21, the third shaft 31 and the fourth shaft 41 are all on the same horizontal plane; wherein, the The third axis 31 is in the extension direction of the first axis 11, the second axis 21 is in the extension direction of the fourth axis 41, and the first axis 11 is perpendicular to the second axis ; The first rotor shaft 13 is perpendicular to the horizontal plane and installed on the other end of the first shaft 11, the second rotor...

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PUM

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Abstract

The invention relates to a four-rotor aircraft and a control system thereof. The four-rotor aircraft comprises a rack, a first shaft, a second shaft, a third shaft, a fourth shaft, a first rotor, a second rotor, a third rotor, a fourth rotor, a first rotor shaft, a second rotor shaft, a third rotor shaft and a fourth rotor shaft. The first rotor shaft deflects in the axial direction of the first shaft, the second rotor shaft deflects in the axial direction of the second shaft, the third rotor shaft deflects in the direction of the third shaft, and the fourth rotor shaft deflects in the axial direction of the fourth shaft. The flying direction of the aircraft can be changed by adjusting the deflecting angles of the rotor shafts, and therefore the flying direction of the aircraft can be controlled conveniently.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a quadrotor aircraft and a control system thereof. Background technique [0002] Quadrotor aircraft has the advantages of vertical take-off and landing, hovering in the air, etc., and is widely used. However, the existing quadrotor aircraft changes the flying attitude of the aircraft in the air by adjusting the speed of the four rotors. It has poor crosswind resistance and slow attitude adjustment. and other defects. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide a four-rotor aircraft with strong crosswind resistance and sensitive flight direction adjustment. [0004] The technical solution of the present invention to solve the above-mentioned technical problems is as follows: a quadrotor aircraft, which includes a frame, a first shaft, a second shaft, a third shaft, a fourth shaft, a first rotor, a second rotor, a third rot...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C9/06B64C9/08
CPCB64C9/06B64C9/08
Inventor 周小勇
Owner 周小勇
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