The invention discloses a hovering type bionic double-flapping-wing aircraft and a control method thereof, relates to the technical field of bionic double-flapping-wing aircrafts, and aims to solve the problem that the existing aircraft is likely to be more easily interfered by extraneous interference such as airflow and wind power due to the motion property of a double-wing structure, so that the hovering type bionic double-flapping-wing aircraft is more likely to be damaged. According to the invention, a shifting rack, a driving gear and an adjusting brace are arranged and are matched with a first fixed seat, so that when the aircraft flies, a relatively balanced posture is difficult to keep during flight, so that not only is a large load brought to parts of the aircraft, but also relatively poor stability during flight is caused. The shifting rack, the driving gear and the adjusting brace are arranged and are matched with the first fixed seat; according to the bionic double-flapping-wing aircraft, the shape of the wings can be changed to obtain larger lift force, in addition, maneuverability can be better improved, the simulation effect is better, the bionic double-flapping-wing aircraft can be more stable during flight, the structural design of the bionic double-flapping-wing aircraft can flexibly adapt to different flight scenes and task requirements, and the bionic double-flapping-wing aircraft has high adaptability and application potential.
本发明公开了一种可悬停式仿生双扑翼飞行器及其控制方法,涉及仿生双扑翼飞行器技术领域,现如今飞行器会存在一个较大的弊端,由于双翼结构的运动性质,飞行器可能更容易受到气流、风力等外界干扰,因此在飞行难以保持相对平衡的姿态,这样不仅会对飞行机的零部件带来较大的负荷,还会导致飞行中稳定性相对较差,本发明通过设置拨动齿条、驱动齿轮以及调节拉条并与第一固定座进行配合,使得飞行器在飞行时,可以通过改变翅膀的形状来获得更大的升力,另外在机动性上也能得到更好的提升,拟真效果更好,可以在飞行时更加的稳定,且仿生双扑翼飞行器的结构设计可以灵活适应不同的飞行场景和任务需求,具备较强的适应性和应用潜力。
Hovering type bionic double-flapping-wing aircraft and control method thereof
一种可悬停式仿生双扑翼飞行器及其控制方法
2023-11-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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