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TRAILING EDGE CHANGE MECHANISM AS AN ATTITUDE CONTROL MECHANISM OF FLAPPING WING AERIAL VEHICLES
TRAILING EDGE CHANGE MECHANISM AS AN ATTITUDE CONTROL MECHANISM OF FLAPPING WING AERIAL VEHICLES
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机译：跟踪边缘变化机制作为扑翼飞行器的姿态控制机制
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摘要
The present invention relates to a control mechanism of a wing end part to control an insect pose mimicking a type of flapping flight fuselage, which comprises: a left-wing and right-wing TE holder in order to fix both wing ends of the flapping flight respectively; and to control tilt operating both wing ends rotatable in the flapping flight fuselage; an actuator module provided in the flapping flight fuselage; and a link element to transmit the operation force generated by the actuator module to the right wing and the left wing TE holder. Therefore, the present invention can control a stable flight pose by manipulating the tilt operating of both wing ends of the flight to generate rolling, pitching, yawing, or arbitrary moment which are necessary to control the flight pose.
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