Simulation Analysis of Electromechanical Coupling for Unmanned Aerial Vehicle Cabin Door System  

作　　者：Bangjian Wang Xiaohang Hu Hong Nie Bangjian Wang;Xiaohang Hu;Hong Nie(College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China)

机构地区：[1]College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

出　　处：《World Journal of Engineering and Technology》2023年第4期1012-1018,共7页世界工程和技术（英文）

摘　　要：In order to study the dynamic response of the unmanned aerial vehicle cabin door opening and closing system under impact load conditions, considering the flexible treatment of mechanical components, and the system’s motion with different stiffness of energy-absorbing components, a rigid-flexible coupling model of the cabin door actuation system was established in LMS. Virtual. Motion. In Amesim, a control model of the motor was created. Through the Motion-Amesim co-simulation module, the dynamic module of the system was combined with the motor control module to complete the electromechanical coupling simulation and analyze the results. .In order to study the dynamic response of the unmanned aerial vehicle cabin door opening and closing system under impact load conditions, considering the flexible treatment of mechanical components, and the system’s motion with different stiffness of energy-absorbing components, a rigid-flexible coupling model of the cabin door actuation system was established in LMS. Virtual. Motion. In Amesim, a control model of the motor was created. Through the Motion-Amesim co-simulation module, the dynamic module of the system was combined with the motor control module to complete the electromechanical coupling simulation and analyze the results. .

关 键 词：Unmanned Aircraft Cabin Door Electromechanical Coupling Virtual Prototype Dynamic Characteristics 

分 类 号：G63[文化科学—教育学]