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Bionic ornithopter and control method thereof

A flapping aircraft and a control method technology, applied in the field of bionic robots, can solve the problems of flight maneuverability and stability that need to be improved, and achieve the effect of improving maneuverability and stability

Active Publication Date: 2021-01-29
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, the flight maneuverability and stability of the current bionic flapping-wing aircraft need to be improved

Method used

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  • Bionic ornithopter and control method thereof
  • Bionic ornithopter and control method thereof
  • Bionic ornithopter and control method thereof

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Embodiment Construction

[0041] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0042] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0043] figure 1 The structural diagram of the bionic flapping-wing aircraft provided by the embodiment of the present invention. see figure 1 , the bionic flapping-wing aircraft of the present embodiment is a bi...

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Abstract

The invention discloses a bionic ornithopter and a control method thereof. The chest structure in the bionic ornithopter comprises a chest main carbon fiber rod, a first driving steering engine and asecond driving steering engine, wherein a first driving steering engine and a second driving steering engine are arranged at the top end of the chest main carbon fiber rod; the first driving steeringengine is connected with the left wing; the second driving steering engine is connected with the right wing; a belly structure comprises a belly carbon fiber rod and a third driving steering engine; the third driving steering engine is arranged at the tail end of the chest main carbon fiber rod; a top end of the belly carbon fiber rod is fixed with a third driving steering engine; a micro-controlsystem is arranged at a tail end of the belly carbon fiber rod; the micro-control system is used for controlling the first driving steering engine, the second driving steering engine and the third driving steering engine so as to drive the left wing and the right wing to do cosine law playing motion and drive the belly carbon fiber rod to do swing motion with the same frequency and opposite phaseas the cosine law playing motion. The bionic ornithopter is advantaged in that maneuverability and stability of flight can be improved.

Description

technical field [0001] The invention relates to the field of bionic robots, in particular to a bionic flapping-wing aircraft and a control method thereof. Background technique [0002] The flapping-wing aircraft has its unique advantages, and has broad application prospects in the fields of national defense and civilian use. The research on the flapping-wing aircraft has become a hot spot in the field of aviation research. In the early days, due to the limitations of people's understanding of the flapping wing flight method and the limitation of the technological level at that time, the true veil of this flight method was not unveiled. People in ancient times tried to use various materials to make wings, hoping to fly with birds by relying entirely on human physical strength. Leonardo da Vinci of the European Renaissance designed a human-powered orthopter. However, attempts to achieve flight by simply vibrating wings using human power have failed. Afterwards, people focus...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 王少萍张益鑫黄文皓李少石何思源王兴坚
Owner BEIHANG UNIV
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