Longitudinal Attitude Control Device and method for Flapping Wing MAV

摘要

The present invention is to control the attitude of the wing vehicle, comprising a mounting portion on which the weight is mounted and a variable plate connected to the mounting portion, the variable plate is disposed in the longitudinal direction of the wing aircraft and longitudinally upward of the wing vehicle by the wire Alternatively, the posture control of the wing aircraft can be controlled in a simpler configuration than the conventional one by changing the center of gravity of the wing aircraft by the movement of the mounting portion and reducing the friction to reduce the operating force. Device method.