Abstract: The present invention provides a remote control system of an aircraft 1 that includes a camera 2 mounted on the aircraft 1, a monitor 4 visible from an operator 3 remote from the aircraft 1, a remote controller 5 operated by the operator 3, an acceleration sensor 6 mounted on the aircraft 1 to detect upward/downward, left/right and forward/backward accelerations, sensitive pads 7 configured to be attached to each portion of the operator 3, and a controller 8 that generates a vibration or an electrical stimulus on each of the sensitive pads 7 while a magnitude of the vibration or the electrical stimulus is changed based on an output value of the acceleration sensor 6 to make the operator 3 feel a direction and a magnitude of the acceleration generated on the aircraft 1.

Abstract: The present invention provides a remote control system of an aircraft 1 that includes a camera 2 mounted on the aircraft 1, a monitor 4 visible from an operator 3 remote from the aircraft 1, a remote controller 5 operated by the operator 3, an acceleration sensor 6 mounted on the aircraft 1 to detect upward/downward, left/right and forward/backward accelerations, sensitive pads 7 configured to be attached to each portion of the operator 3, and a controller 8 that generates a vibration or an electrical stimulus on each of the sensitive pads 7 while a magnitude of the vibration or the electrical stimulus is changed based on an output value of the acceleration sensor 6 to make the operator 3 feel a direction and a magnitude of the acceleration generated on the aircraft 1.