Abstract: A control device includes :a resultant thrust magnitude calculation unit that calculates a magnitude of a resultant thrust of a vertical thrust and a horizontal thrust, based on a magnitude of a thrust indicated by a signal output from a thrust adjustment lever; a resultant thrust angle setting unit that sets a resultant thrust angle in accordance with a speed of an aircraft; a component calculation unit that calculates a vertical component and a horizontal component of the resultant thrust; and a rotor control unit that controls a vertical rotor device to provide the vertical thrust having the vertical component and controls a horizontal rotor device to provide the horizontal thrust having the horizontal component.

Abstract: A rotor control device includes: a vertical rotor control unit that controls each VTOL rotor based on a first allocation command value; a horizontal rotor control unit that controls each cruise rotor based on a second allocation command value; and an allocation command value calculation unit that sets, as the first allocation command value, a difference between a command value of a yaw moment and the second allocation command value, that sets the magnitude of the second allocation command value to 0 when the command value of the yaw moment is less than a threshold, and that sets the magnitude of the second allocation command value to a value greater than 0 when the command value of the yaw moment is equal to or greater than the threshold.

Abstract: A rotor control device for performing attitude control of a fuselage of an aircraft includes a VTOL rotor control unit for controlling each rotor based on a roll moment command value, a pitch moment command value, and a yaw moment command value. When the magnitude of the roll moment command value or the magnitude of the pitch moment command value is equal to or greater than a threshold, the VTOL rotor control unit controls each rotor without using the yaw moment command value.

Abstract: A fuel adapter includes: an adapter main body, an outer panel-side seal part, and an inner panel-side seal part. The adapter main body is formed of a rigid plastic. The outer panel-side seal part and the inner panel-side seal part are formed of a flexible plastic to be elastically deformable. The inner panel-side seal part is capable of being subject to a deflection deformation that absorbs a variation of a relative position between the outer panel and the inner panel.