The embodiment of the invention discloses an eight-flapping-effect hovering flapping-wing aircraft and a flight control method thereof.The flapping-wing aircraft comprises a fuselage, ailerons, a cross-shaped empennage, a wing root rod, two aileron driving mechanisms, two flapping mechanisms and four pairs of wings, and the ailerons, the flapping mechanisms and the aileron driving mechanisms are arranged on the fuselage; the cross-shaped empennage is arranged at the tail part of the fuselage, two pairs of wings are respectively arranged on two sides of the fuselage through wing root rods, and the two groups of flapping mechanisms respectively drive the wings on two sides to do reciprocating flapping motion; each aileron is composed of a fixed control surface and two rotating control surfaces arranged on the two sides of the fixed control surface correspondingly, and the two aileron driving mechanisms drive the two rotating control surfaces to deflect front and back correspondingly. The flapping-wing aircraft is simple and efficient in overall structure and easy to control, and lifting, hovering, pitching, rolling and yawing movement of the flapping-wing aircraft capable of hovering with the eight-beat effect can be achieved by controlling the rotating speed of the motors and deflection of the steering engines.
本发明实施例公开了一种八拍合效应的可悬停扑翼飞行器及其飞行控制方法,所述扑翼飞行器包括机身、副翼、十字型尾翼、翼根杆、2组副翼驱动机构、2组扑动机构、四对机翼,所述副翼、扑动机构、副翼驱动机构设于机身上,十字型尾翼设于机身尾部,机身两侧通过翼根杆各设有2对机翼,2组扑动机构分别驱动两侧的机翼做往复扑翼运动;副翼由固定舵面和2个分别设于固定舵面两侧的转动舵面组成,2组副翼驱动机构分别驱动2个转动舵面做前后偏转运动。本发明的整体结构简单高效,容易控制,通过控制电机的转速以及舵机的偏转即可实现八拍合效应的可悬停扑翼飞行器的升降、悬停、俯仰、滚转和偏航运动。
Eight-beat-effect hovering ornithopter and flight control method thereof
八拍合效应的可悬停扑翼飞行器及其飞行控制方法
27.08.2024
Patent
Elektronische Ressource
Chinesisch
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