Longitudinal Attitude Control Device and method for Flapping Wing MAV

摘要

The present invention controls posture of a wing flapping flight vehicle. The present invention includes: a mounting unit on which a weight body is mounted; and a variable board to which the mounting unit is connected, wherein the variable board is arranged in a length direction of the wing flapping flight vehicle and is deformed upwards or downwards in a longitudinal direction of the wing flapping flight vehicle by a wire, thereby being capable of posture control and capable of preventing decrease of operating force by decreasing friction even with a simpler structure than a conventional one by the structure changing the center of gravity of the wing flapping flight vehicle by movement of the mounting unit.