发明名称 RESONANCE MOTOR DIRECT DRIVE FLAPPING WING MICRO AIR VEHICLE SYSTEM
摘要 Presented herein are an actuation system and a flapping wing micro aerial vehicle system. In one embodiment, for energy efficiency and to achieve a resonant system, the flapping wing is directly driven using conventional DC motors coupled with torsion springs. Using a transmission gear, the motor is designed to operating at an efficient speed, but generates an overall reciprocal motion to the wing. Closed loop control is applied to achieve tracking of the desired wing motion kinematics, the frequency of which is tuned to match the resonant frequency of the system. We also show that wing kinematic control can be achieved by tracking trajectories with different amplitude and bias, therefore creating flight control forces and torques.
申请公布号 US2016159477(A1) 申请公布日期 2016.06.09
申请号 US201514707877 申请日期 2015.05.08
申请人 PURDUE RESEARCH FOUNDATION 发明人 Deng Xinyan;Zhang Jian
分类号 B64C33/02 主分类号 B64C33/02
代理机构 代理人
主权项 1. An actuation system, comprising: a direct current motor; a motor encoder, the motor encoder providing position feedback for the motor; and a torsional spring, the torsional spring is coupled to the direct current motor.
地址 West Lafayette IN US