FLAPPING-WING SYSTEM HAVING A PITCHING MOMENT GENERATOR FOR LONGITUDINAL ATTITUDE CONTROL

摘要

The present invention relates to a flapping flight vehicle having a pitching moment generation device for longitudinal altitude control. The flapping flight vehicle comprises: a frame (110) forming the fuselage of the flapping flight vehicle; a driving module (120) fixed on the frame (110) to generate rotation driving force; a slider (130) arranged on the frame (110) to be vertically slid by the rotation driving force of the driving module (120); a pair of wing fixing holders (140) symmetrically arranged in both sides of the frame to fix wings; a pair of link members (150) having one end connected to the wing fixing holders (140) to be rotated and the other end connected to the sliders (130) to be rotated; and a tilting angle adjustment member (160) connected to the pair of wing fixing holders (140) to be rotated, and hinge-assembled to the frame (110) to adjust the tilting angle range of the wing fixing holders (140). The present invention can control altitude by easily adjusting the flapping angle range of the flapping flight vehicle without a complex mechanical composition.