The invention belongs to the technical field of aviation aircrafts, and discloses a multi-rotor integrated aircraft and a flight control method.The multi-rotor integrated aircraft is composed of an aircraft body, integrated wings, a flight control system and a power system; vertical take-off and landing, low-speed flight and hovering of the aircraft can be achieved like a multi-rotor aircraft, the aircraft can also fly like a fixed wing, multi-rotor flight and fixed wing flight state conversion is completed by controlling the elevation angle of the integrated wing, the endurance is improved by additionally arranging the large foldable fixed wing, and the economic performance of the aircraft is improved. The vector thruster is additionally arranged to improve the maneuvering performance of the aircraft, the integrated wings are designed to be of a foldable structure, storage and transportation are facilitated, and the aircraft can be controlled to do lifting, left-right steering, front-back translation, left-right translation and other motions under the condition that a single integrated wing is not provided with a power adapter through the design that a rudder is additionally arranged on each integrated wing.
本发明属于航空飞行器技术领域,公开了一种多旋翼集成飞行器与飞行控制方法,飞行器由机体、集成机翼、飞控系统、动力系统组成,在机体上至少设置两组纵列式集成机翼,既可以像多旋翼飞行器一样解决飞行器垂直起降、低速飞行与空中悬停,也可以像固定翼一样飞行,通过对集成机翼的仰角控制完成多旋翼飞行与固定翼飞行状态转换,通过加装大型可折叠固定翼提高续航力提高其经济性能,加装矢量推进器改善其操纵性能,把集成机翼设计成可折叠结构,方便于储存与运输,通过在每个集成机翼上增加方向舵的设计在单个集成机翼没有功率适配器的情况下也可控制飞行器进行升降、左右转向、前后、左右平移等运动。
Multi-rotor integrated aircraft and flight control method
一种多旋翼集成飞行器与飞行控制方法
2024-09-20
Patent
Electronic Resource
Chinese
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