Electromechanical Co-simulation for UAV’s Mission Payload
摘要
The aim of this study is to assist the debugging of servo motion control system and the designing of product structure while developing electric-optic turret of the current UAV’s mission payload. We researched on the electromechanical co-simulation technology for the electric-optic turret stabilized platform by constructing a multi-body dynamic model for the structure, Considering the disturbance of UAV, and designing an inertial servo control system using the speed-loop control to achieve inertial stability. The study implemented the electromechanical co-simulation analysis of the integration of mechanism and the servo control system.