A Multifunctional HIL Testbed for Multirotor VTOL UAV Actuator
Application driven multirotor UAV design becomes an emerging challenge as missions’ needs require improved performance. In this paper, a multifunctional identification and control testbed for UAV actuators is introduced. Brushless controllers, motors and propeller pairs need to be chosen precisely to achieve optimal performance. Accurate identification of intrinsic parameters of those actuators and their comparison allow the engineer to decide between choosing existing parts or designing their own. Furthermore, we introduce a real-time MATLAB interface that allows to reduce implementation time when developing brushless motors control algorithms.
Corentin Chéron Aaron Dennis Vardan Semerjyan YangQuan Chen
Center for Self-Organizing and Intelligent Systems, Department of Electrical and Computer Engineering, Utah State University.
国际会议
青岛
英文
44-48
2010-07-15(万方平台首次上网日期,不代表论文的发表时间)