多自由度仿生扑翼飞行机器人结构设计与分析

Design and Analysis of Multi-Degree of Freedom Bionic Flapping Wing Flight Robot Structure

旨在设计一种能够飞行的大型仿生扑翼飞行机器人,以海鸥作为设计原型进行飞行方式和运动规律分析,建立结构设计和数学模型,实现多自由度仿生扑翼飞行。对设计结构进行运动学分析,使仿生飞行结构更加合理且符合基本气动性能。通过建立三维模型,将其运动学仿真结果与理论结果进行对照分析,证明了理论分析的正确性和设计结构的合理性。

The purpose of this paper is to design a large bionic flapping wing flying robot that can fly.The seagull was used as a design prototype to analyze the flight mode and motion laws.Through structural design and mathematical model establishment,multi-degree of freedom bionic flapping-wing flight was realized.The kinematic analysis of the design structure makes the bionic flight structure more reasonable and meets the basic aerodynamic performance.By establishing a three-dimensional model and comparing its kinematics simulation results with theoretical results,the correctness of the theoretical analysis and the rationality of the designed structure are proved.