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

作　　者：李颖 朱志松[1] LI Ying;ZHU Zhisong(School of Mechanical Engineering,Nantong University,Nantong 226019,China)

机构地区：[1]南通大学机械工程学院,南通226019

出　　处：《现代制造工程》2025年第4期53-60,35,共9页Modern Manufacturing Engineering

基　　金：教育部产学合作协同育人项目(220906517065911)。

摘　　要：针对当前扑翼飞行器生产调试效率低、缺乏有效监控方式等问题,研究并设计了扑翼飞行器数字孪生交互系统。首先,分析了扑翼飞行器数字孪生交互系统五维模型架构,并在此基础上设计了虚拟仿真系统、监测系统及控制系统;然后,虚拟仿真系统基于Webots虚拟仿真平台构建物理实体的孪生体模型并进行飞行姿态、飞行动作的仿真调试,从而提高现场调试效率,监测系统及控制系统均通过上位机控制系统实现孪生体模型和物理实体之间数据的虚实实时双向闭环交互,从而实现扑翼飞行器飞行过程的可视化监控;最后,通过姿态可视化试验和飞行试验验证了扑翼飞行器数字孪生交互系统的有效性和可行性。扑翼飞行器数字孪生交互系统为进一步丰富扑翼飞行器数字孪生系统功能提供了新方案。To address the issues of low production and debugging efficiency and the lack of effective monitoring methods for flapping-wing aircraft, a digital twin interaction system for flapping-wing aircraft was researched and designed. First, the five-dimensional model architecture of the digital twin interaction system was analyzed, based on which the virtual simulation system, monitoring 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 debugging 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 

分 类 号：TP391.9[自动化与计算机技术—计算机应用技术]