摘要
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.
作者
王超
屈方杰
黄恒敬
仲军
WANG Chao;QU Fangjie;HUANG Hengjing;ZHONG Jun(Hohai University,College of Mechanical and Electrical Engineering,Nanjing 213000,China)
出处
《宇航总体技术》
2020年第1期39-46,62,共9页
Astronautical Systems Engineering Technology
基金
装备预研教育部联合基金(6141A02033616).
关键词
仿生扑翼飞行机器人
海鸥
运动学
三维建模
计算机仿真
Bionic flapping wing flying robot
Seagull
Kinematics
Three-dimensional modeling
Computer simulation
