Manned flapping -wing aircraft

The utility model discloses a manned flapping -wing aircraft, include: install in the mount pad at human back, install respectively two sensors on human left hand and the right hand, install on the mount pad and bilateral symmetry's two wing subassemblies and locate the mount pad in the controller, the wing subassembly includes: cross bogie, flapping wing, bearing pressure arm component, first motor, second motor, first telescopic link and second telescopic link, controller respectively with sensor, first motor and the 2nd motor electrically connected, flexible action is realized to the first telescopic link of a motor drive, flexible action is realized to the 2nd motor drive second telescopic link. The utility model discloses a sensor detects the direction of motion and the dynamics of arm, and the controller control motor is according to corresponding proportion work, the flexible volume of telescopic link in the control wing subassembly to driving the direction of motion of the synchronous arm of flapping