The invention relates to the technical field of micro aircraft, in particular to four-flapping wing aircraft and a control method thereof. The four-flapping wing aircraft comprises a fixed bracket, afuselage, flapping mechanisms, flapping wings, a flight control system and an empennage, wherein the fixed bracket and the empennage are respectively arranged on the front end and the back end of thefuselage; four groups of flapping mechanisms are arranged on the fixed bracket in a circumferential direction; four groups of flapping wings are respectively connected with the four groups of flappingmechanisms, and the flapping mechanisms are used for driving the flapping wings connected with the flapping mechanisms to flap; and the flight control system is arranged on the fuselage and is used for controlling the four groups of flapping mechanisms, so that the attitude control over the four-flapping wing aircraft is realized. According to the four-flapping wing aircraft, the four groups of flapping mechanisms are coupled through airflow, the lifting force generating efficiency is high, the provided total lifting force is large, the flight endurance time can be extended, and the maneuverability and flexibility of the aircraft are enhanced.
本发明涉及微型飞行器技术领域,特别涉及一种四扑翼飞行器及其控制方法。四扑翼飞行器包括固定支架、机身、扑动机构、扑翼、飞控系统及尾翼,其中固定支架和尾翼分别设置于机身的前、后端;扑动机构为四组,并且沿周向设置于固定支架上;扑翼为四组,并且分别与四组扑动机构连接,扑动机构用于驱动与其连接的扑翼进行扑动动作;飞控系统设置于机身上,用于控制四组扑动机构,从而实现四扑翼飞行器的姿态控制。本发明的四套扑动机构互相有气流耦合,升力的产生效率高,可提供的总升力大,有助于提高飞行续航时间,增强飞行器的机动性与灵活性。
Four-flapping wing aircraft and control method thereof
一种四扑翼飞行器及其控制方法
2020-12-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Four-flapping-wing aircraft and attitude control system thereof
European Patent Office | 2025
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