Vertical take-off and landing aircraft

The invention provides a vertical take-off and landing aircraft. The plurality of VTOL rotors (20) are divided into a plurality of groups, each VTOL rotor is included in any one of the groups, the controller (44) is capable of performing stop control for stopping the rotational operation of each VTOL rotor during flight, and when the stop control of the plurality of VTOL rotors is released, the controller (44) sequentially performs release of the stop control in groups. Accordingly, it is possible to suppress a change in the ride comfort of the VTOL aircraft at a stage of shifting from the cruise process to the landing process. 本发明提供一种垂直起降航空器。多个VTOL旋翼(20)被分为多个组，每个VTOL旋翼都包含在任意一个组中，控制器(44)能够在飞行过程中进行使每个VTOL旋翼的旋转动作停止的停止控制，当解除多个VTOL旋翼的停止控制时，控制器(44)以组为单位依次进行停止控制的解除。据此，能够抑制在从巡航工序向降落工序转移的阶段VTOL飞机乘坐舒适度的变化。