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This paper studies the system design of micro flapping wing air vehicle, and describes the mechanical design and controller design of micro flapping wing air vehicle. X-airfoil is selected to design the wing of air vehicle. The combination of cork and carbon fiber is used to design air vehicle body. The system for the aerodynamic testing of micro flapping wings air vehicle is designed to verify the thrust and lift obtained from the system applied for the micro flapping wings air vehicle. The indicators of flight are given by flight test.