The invention discloses a micro flapping-wing air vehicle with a controllable wing flapping plane and a flight control method of the micro flapping-wing air vehicle. The device comprises two sets of transmission mechanisms, two flexible wings, two sets of control mechanisms, a connecting support and a battery. The transmission mechanism converts rotation of the rotating shaft of the motor into reciprocating flapping of the driving rod. And the bistable flexible wings are driven by a driving rod of the transmission mechanism to do reciprocating flapping to generate gas power. The control mechanism changes the direction of aerodynamic force resultant force generated by the bistable flexible wings by changing the flapping plane. The connecting support is used for installing the transmission mechanism, the control mechanism and the battery. The battery is used for providing electric energy for the motor. According to the invention, by changing the flapping plane and the rotating speed of the motor, the micro flapping-wing air vehicle can quickly generate the control torque meeting the flight control requirement, and the design difficulty of an air vehicle control system is reduced.
本发明公开了一种翼扑动平面可控的微型扑翼飞行器及其飞行控制方法。该装置包含两套传动机构、两个柔性翼、两套控制机构、连接支架和电池。所述传动机构将电机转轴的转动转化为驱动杆的往复扑动。所述双稳态柔性翼在传动机构的驱动杆的驱动下往复扑动产生气动力。所述控制机构通过改变扑动平面的方式改变双稳态柔性翼产生气动力合力的方向。所述连接支架用于安装传动机构、控制机构和电池。所述电池用于向电机提供电能。本发明通过改变扑动平面和电机转速的方式,使微型扑翼飞行器能够快速产生满足飞行控制需要的控制力矩,降低了飞行器控制系统的设计难度。
Micro flapping-wing air vehicle with controllable wing flapping plane and flight control method of micro flapping-wing air vehicle
一种翼扑动平面可控的微型扑翼飞行器及其飞行控制方法
2024-03-26
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
Europäisches Patentamt | 2020
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