Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft

Jiang Houqing; Hou Yu; Guo Yongxing

doi:10.16578/j.issn.1004.2539.2023.11.010

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Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft

Design· Calculation | 更新时间：2023-12-01

- Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft
- Journal of Mechanical Transmission Vol. 47, Issue 11, Pages: 65-72(2023)
- 作者机构：
  
  1.武汉科技大学冶金装备及其控制教育部重点实验室，湖北武汉 430081
  2.武汉科技大学机械传动与制造工程湖北省重点实验室，湖北武汉 430065
  3.武汉科技大学精密制造研究院，湖北武汉 430081
- 作者简介：
- 基金信息：
- DOI：10.16578/j.issn.1004.2539.2023.11.010
  CLC：
- Published：15 November 2023，
  
  Received：27 August 2022，
  
  Revised：17 September 2022，
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江厚清,侯宇,郭永兴.单驱动多模式扑翼飞行器设计及耦合动力学研究[J].机械传动,2023,47(11):65-72.

Jiang Houqing,Hou Yu,Guo Yongxing.Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft[J].Journal of Mechanical Transmission,2023,47(11):65-72.
江厚清,侯宇,郭永兴.单驱动多模式扑翼飞行器设计及耦合动力学研究[J].机械传动,2023,47(11):65-72. DOI： 10.16578/j.issn.1004.2539.2023.11.010.

Jiang Houqing,Hou Yu,Guo Yongxing.Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft[J].Journal of Mechanical Transmission,2023,47(11):65-72. DOI： 10.16578/j.issn.1004.2539.2023.11.010.

摘要

针对目前扑翼飞行器扑翼运动模式单一，飞行灵活性和稳定性不高的问题，设计了一款基于空间连杆机构的单驱动多模式扑翼飞行器。建立了扑翼飞行器运动学模型，通过软件Matlab与Adams联合仿真对驱动机构进行分析，对比得出了扑翼飞行器的运动特性；建立了单驱动多模式扑翼飞行器气动力学模型，将求得的周期变化的迎风阻力施加在机翼上，分析了扑翼飞行器的动力学特性；通过联合机构运动学和气动力学耦合分析，得出扑翼飞行器的耦合动力学特性。为未来扑翼飞行器的飞行控制与性能提升提供了研究基础。

Abstract

Aiming at the problems of single flapping wing movement mode and low flight flexibility and stability of flapping-wing aircraft

a single-drive multi-mode flapping-wing aircraft based on the space linkage mechanism is designed. The kinematic model of the flapping-wing aircraft is established

and the driving mechanism is analyzed by Matlab and Adams co-simulation

and the kinematic characteristics of the flapping-wing aircraft is obtained by comparison. The aerodynamic model of a single-drive multi-mode flapping-wing aircraft is established. The windward resistance with periodic variation is applied to the wing

and the dynamic characteristics of the flapping-wing aircraft are analyzed. Through the kinematic and aerodynamic coupling analysis of the combined mechanism

the coupling dynamic characteristics of the flapping-wing aircraft are obtained

which provides a research basis for the flight control and performance improvement of the flapping-wing aircraft in the future.

关键词

扑翼飞行器多飞行模式空间机构运动分析耦合动力学分析

Keywords

Flapping-wing aircraftMultiple flight modeSpace mechanismMotion analysisCoupling dynamic analysis

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