The invention discloses a multi-section flap control system for a double-wing unmanned aerial vehicle, and relates to the technical field of aircraft flight control. The system comprises an upper flap set, a lower flap set, a control unit, a control unit, a plurality of flap driving units and a detection unit, the flap sets are arranged on four wings of the unmanned aerial vehicle, flap pieces in the flap sets are independently controlled through a flight control calculation unit and the flap driving units, and therefore accurate control over the unmanned aerial vehicle can be achieved; and the aerodynamic efficiency of the unmanned aerial vehicle is improved.
本发明公开了一种用于双翼无人机的多段式襟翼控制系统,涉及航空器飞行控制技术领域;该系统包括上襟翼组、下襟翼组、操控单元、操控单元、多个襟翼驱动单元和检测单元,通过在无人机的四片机翼上设置襟翼组,并通过飞控计算单元和多个襟翼驱动单元对襟翼组中的襟翼片单独控制,从而能够实现对无人机的精确控制,提高无人飞机的气动效率。
Multi-section flap control system for double-wing unmanned aerial vehicle
一种用于双翼无人机的多段式襟翼控制系统
2023-03-03
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2022
|European Patent Office | 2023
|European Patent Office | 2022
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