To provide an aircraft that is automatically restored from an overturned posture to an upright one.

The aircraft includes an automatically restored frame configuration 140 having a protrusion 158 extending upward from an automatically restored center vertical axis. A propulsion system can be installed in a center void 146 in the frame configuration to generate floating power. A power supply 176 is installed in the center void 146 in the automatically restored frame and connected to at least one of rotors 172, 173 in an operated state so as to supply power to the rotor to be rotatable. Moreover, an electronic device 178 for receiving a remote control command is installed in the center void in the automatically restored frame so that it is communicatively interconnected to the power supply so as to allow an aircraft to take off, aviate and land using remote control.