摘要
针对共轴双旋翼无人机操纵系统气动性复杂、各飞行运动耦合性强、建立数学模型及三维模型难度较大的问题,对共轴双旋翼无人机模型进行了结构设计和模拟装配,对倾斜盘的倾斜角度与旋翼受力和运动状态的关系进行了动力学仿真分析,分析结果表明可控方向共轴双旋翼可以完成相应的飞行姿态。
Because the aerodynamics of the control system of coaxial twin-rotor UAV is complex and the coupling of each flight motion is strong,it is difficult to establish a mathematical model and a three-dimensional model.In view of the above problems,the structure design and simulation assembly of the coaxial twin-rotor UAV model are carried out,and the dynamic simulation analysis of the relationship between the rotor force and motion state by the tilt angle of the tilting disc is carried out.The analysis results that that the controllable coaxial twin-rotor can complete the corresponding flight attitude.
作者
吕宝亮
史春景
郝永平
徐九龙
刘成奇
LV Bao-liang;SHI Chun-jing;HAO Yong-ping;XU Jiu-long;LIU Cheng-qi(School of Mechanical Engineering,Shenyang Ligong University,Shenyang 110000,China;Hua An Industry Group Co.,Ltd.,Qiqihar 161000,China)
出处
《机械工程与自动化》
2021年第6期57-59,共3页
Mechanical Engineering & Automation
