发明名称 ELECTRO-MECHANICAL ACTUATOR OF UNMANNED AERIAL VEHICLE AND CONTROL METHOD THEREOF
摘要 <p>The present invention relates to an electric driving device of an unmanned aerial vehicle, and a method to control the same. According to the present invention, the electric driving device installed in an unmanned aerial vehicle to transmit power generated in a first motor and a second motor to the output terminal through one common gear in order to move a control surface of an unmanned aerial vehicle comprises: a communication unit to receive a control signal related to flight; a detecting unit to detect a state of the first and second motors, and to generate state information on the first and second motors; a first controlling unit to control at least one between the first and second motors based on the state information of the first and second motors and the control signal; a second controlling unit to receive the control signal from the communication unit, and receive the state information on the first and second motors from the detecting unit; and a trigger signal generating unit to generate a trigger signal when a malfunction is generated in the first controlling unit. When the trigger signal is generated, the first controlling unit stops control of at least one, and the second controlling unit controls at least one based on the state information of the first and second motors and the control signal while receiving the same in order to continuously control at least one.</p>
申请公布号 KR101494780(B1) 申请公布日期 2015.02.23
申请号 KR20140167724 申请日期 2014.11.27
申请人 发明人
分类号 B64C13/20;B64C13/50 主分类号 B64C13/20
代理机构 代理人
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