VERTICAL TAKEOFF AND LANDING AIRCRAFT USING HYBRID ELECTRIC PROPULSION SYSTEM AND CONTROL METHOD THEREFOR

A vertical takeoff and landing aircraft using a hybrid electric propulsion system and a control method therefor according to an embodiment of the present invention can: perform control such that, during vertical takeoff and landing of an aircraft (1), a generator (20), a power management device (4), and a battery management system (60) simultaneously provide power to a motor (80); and perform control such that, during a cruise flight or transition flight of the aircraft (1), the thrust of a second propeller (82) is increased and a battery (62) of the battery management system (60) is charged with redundant power generated by the generator (20). 根据本发明实施例的使用混合电力推进系统的垂直起降航空器及其控制方法，当飞行体(1)进行垂直起降时，可以控制发电机(20)、电力管理装置(40)及电池管理系统(60)同时向发动机(80)提供电源，当上述飞行体(1)进行巡航飞行或过渡飞行时，可以控制增强第2螺旋桨(82)的推力，且控制由上述发电机(20)生产的富余电力充入上述电池管理系统(60)的电池(62)。