<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>In order to better understand the flight performance and kinematics performance of flapping wing aircraft designed and developed based on the principle of bionics, a space crank rocker mechanism was tried to carry out the virtual prototype design of the bionic aircraft in space motion, and on this basis, its movement characteristics were analyzed. Analyzing the flight mechanisms and scale laws of common flying organisms yields various physical estimation parameters that affect flight characteristics. Flight patterns and motion patterns are analyzed based on the design principles of seabirds, and structural designs and mathematical models are established. Secondly, carry out the design of its flapping and transmission structures, and based on this, carry out the overall structural design and establish a three-dimensional model. Here, the kinematics analysis of its flapping amplitude and angular velocity value is carried out by combining its mechanism motion diagram, and the kinematics simulation results are compared with the theoretical results, which proves the correctness of the theoretical analysis and the feasibility of the design structure.</p>
</abstract>

In order to better understand the flight performance and kinematics performance of flapping wing aircraft designed and developed based on the principle of bionics, a space crank rocker mechanism was tried to carry out the virtual prototype design of the bionic aircraft in space motion, and on this basis, its movement characteristics were analyzed. Analyzing the flight mechanisms and scale laws of common flying organisms yields various physical estimation parameters that affect flight characteristics. Flight patterns and motion patterns are analyzed based on the design principles of seabirds, and structural designs and mathematical models are established. Secondly, carry out the design of its flapping and transmission structures, and based on this, carry out the overall structural design and establish a three-dimensional model. Here, the kinematics analysis of its flapping amplitude and angular velocity value is carried out by combining its mechanism motion diagram, and the kinematics simulation results are compared with the theoretical results, which proves the correctness of the theoretical analysis and the feasibility of the design structure.

Design and motion analysis of a space crank rocker biomimetic aircraft

College of Mechanical and Intelligent Manufacturing, Central South University of Forestry and Technology

Applied Mathematics and Nonlinear Sciences

This work is licensed under the Creative Commons Attribution 4.0 International License.

{"article-title":"Design and motion analysis of a space crank rocker biomimetic aircraft"}

In order to better understand the flight performance and kinematics performance of flapping wing aircraft designed and developed based on the principle of...

Design and motion analysis of a space crank rocker biomimetic aircraft

Online veröffentlicht: 02. Juli 2024

Seitenbereich: -

Eingereicht: 28. Feb. 2024

Akzeptiert: 23. Mai 2024

DOI: https://doi.org/10.2478/amns-2024-1539

Schlüsselwörter
Flight scale law, Flapping structure, Kinematics model, Parameter estimation, Motion simulation

© 2024 Shuai Yan et al., published by Sciendo

This work is licensed under the Creative Commons Attribution 4.0 International License.

Design and motion analysis of a space crank rocker biomimetic aircraft

Online veröffentlicht: 02. Juli 2024

Seitenbereich: -

Eingereicht: 28. Feb. 2024

Akzeptiert: 23. Mai 2024

DOI: https://doi.org/10.2478/amns-2024-1539

SchlüsselwörterFlight scale law, Flapping structure, Kinematics model, Parameter estimation, Motion simulation

© 2024 Shuai Yan et al., published by Sciendo

This work is licensed under the Creative Commons Attribution 4.0 International License.

Schlüsselwörter
Flight scale law, Flapping structure, Kinematics model, Parameter estimation, Motion simulation