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扑翼飞行器数字孪生交互系统的研究与实现

李颖 朱志松

现代制造工程Issue(4):53-60,35,9.
现代制造工程Issue(4):53-60,35,9.DOI:10.16731/j.cnki.1671-3133.2025.04.006

扑翼飞行器数字孪生交互系统的研究与实现

Research and implementation of a digital twin system for flapping-wing aircraft

李颖 1朱志松1

作者信息

  • 1. 南通大学机械工程学院,南通 226019
  • 折叠

摘要

Abstract

To address the issues of low production and debugging efficiency and the lack of effective monitoring methods for flap-ping-wing aircraft,a digital twin interaction system for flapping-wing aircraft was researched and designed.First,the five-dimen-sional model architecture of the digital twin interaction system was analyzed,based on which the virtual simulation system,moni-toring system,and control system were designed.The virtual simulation system constructed a twin model of the physical entity on the Webots simulation platform and carried out simulation of flight attitudes and flight maneuvers,thereby improving on-site de-bugging efficiency.The monitoring and control systems enabled real-time bidirectional colsed-loop data interaction between the twin model and the physical entity through the upper computer control system,achieving visual monitoring of the flapping-wing aircraft during flight.Finally,the effectiveness and feasibility of the digital twin interaction system were verified through attitude visualization tests and flight tests.This digital twin interaction system provides a new approach to further enhancing the functions of digital twin systems for flapping-wing aircraft.

关键词

数字孪生/扑翼飞行器/虚实映射/Webots平台/虚拟调试

Key words

digital twin/flapping-wing aircraft/virtual-to-real mapping/Webots platform/virtual debugging

分类

计算机与自动化

引用本文复制引用

李颖,朱志松..扑翼飞行器数字孪生交互系统的研究与实现[J].现代制造工程,2025,(4):53-60,35,9.

基金项目

教育部产学合作协同育人项目(220906517065911) (220906517065911)

现代制造工程

OA北大核心

1671-3133

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