Patent ID: 6659839
Filing Date: 2003-12-09
Classification: A63H

Abstract:
A flight control system capable of reproducing a flight attitude of a corresponding real aircraft, the flight control system comprisinga base, a model aircraft, a vertical motion means mounted on the base for enabling the model aircraft to ascend or descend in order to reproduce changes in position from a state in which the aircraft is set at a lower position so as to copy the attitude of the corresponding real aircraft during a halt to a state in which the aircraft is set at a higher position so as to copy the attitude of the corresponding real aircraft during flight, an attitude control means mounted in the model aircraft for enabling the model aircraft to be inclined in longitudinal and lateral directions in order to reproduce longitudinal and lateral motions of the corresponding real aircraft, the attitude control means being provided at a tip portion of the vertical motion means so that an operation performed by the vertical motion means can be coordinated with an operation performed by the attitude control means, and an external control section being remotely connected to at least one of said vertical motion means and said attitude control means via wired or wireless communication lines.