仿生无人系统动力学模型验证数据

“仿生无人系统动力学模型验证数据”主要面向仿生扑翼无人系统动力学建模与智能控制研究需求建设，基于MATLAB R2023b平台在Lenovo Legion R9000k计算环境中通过理论建模与数值仿真方法产生。数据主要记录了仿生无人机在扑动控制、柔性形变与振动抑制等典型场景下的动力学仿真结果，涵盖单柔性翼振动控制、刚柔耦合双连杆机翼动力学及三维柔性翼高精度形变跟踪等内容。数据包括12组数值文件（.mat格式）与8组仿真结果图（.jpg格式），详细反映了弯曲/扭转位移、扑动角度与振动响应等关键观测值，数据量约3.7MB。该数据集为“建立扑翼飞行通用数学模型”任务提供核心验证支撑，对推动仿生无人系统结构设计与控制策略研究具有重要意义。

This dataset is constructed for the research demands of dynamic modeling and intelligent control of bionic flapping-wing unmanned systems. It is generated through theoretical modeling and numerical simulation on the Lenovo Legion R9000k computing environment using the MATLAB R2023b platform. The data primarily documents the dynamic simulation results of bionic unmanned aerial vehicles (UAVs) under typical scenarios such as flapping control, flexible deformation and vibration suppression, covering single flexible wing vibration control, rigid-flexible coupled dual-link wing dynamics, high-precision deformation tracking of 3D flexible wings, and other relevant contents. The dataset includes 12 numerical files in .mat format and 8 simulation result images in .jpg format, which thoroughly reflect key observed metrics including bending/torsional displacement, flapping angle and vibration response, with a total data size of approximately 3.7 MB. This dataset provides core validation support for the task of "establishing a general mathematical model for flapping flight", and is of great significance for advancing the research on structural design and control strategies of bionic unmanned systems.