The invention discloses an aircraft control surface deflection angle control method and device and a storage medium, and the method comprises the steps: obtaining a flight state parameter and a control surface control variable of an aircraft in a preset control mode, and obtaining an aileron control surface deflection angle of the aircraft when the flight state parameter and the control surface control variable meet a preset first condition; when the aileron control surface deflection angle meets a preset second condition, a sideslip angle instruction is generated at the sideslip angle rate, and a limit value is calculated according to the corrected airspeed value; and generating a direction control surface instruction and an aileron control surface instruction based on the sideslip angle instruction, and controlling an aileron control surface deflection angle according to the direction control surface instruction and the aileron control surface instruction. According to the technical scheme, the technical problem that in the prior art, an aircraft driver needs to adjust the control surface deflection angle can be solved, the flight cruise resistance can be reduced, and under the condition that the same maneuvering characteristics and structure safety are met, the control burden of the driver is effectively relieved, and the aircraft cruise performance is improved.

    本发明公开了一种飞行器舵面偏转角控制方法、装置及存储介质,方法包括:在预设的控制模式下,获取飞行器的飞行状态参数和舵面操纵量,当飞行状态参数和舵面操纵量满足预设的第一条件时,获取飞行器的副翼舵面偏转角;当副翼舵面偏转角满足预设的第二条件时,以侧滑角速率生成侧滑角指令,并根据校正空速值计算限制值;基于侧滑角指令生成方向舵面指令和副翼舵面指令,并根据方向舵面指令和副翼舵面指令控制副翼舵面偏转角。本发明所提供的技术方案能够解决现有技术中需要依赖飞机驾驶员调整舵面偏转角的技术问题,本方案能够降低飞行巡航阻力,在满足相同的机动性能及结构安全的情况下,有效减轻驾驶员操纵负担,提高飞机巡航性能。


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    Title :

    Aircraft control surface deflection angle control method and device and storage medium


    Additional title:

    飞行器舵面偏转角控制方法、装置及存储介质


    Contributors:
    LI WENDAN (author) / LIU JUN (author) / CHEN SHI (author) / ZHENG XIAOHUI (author) / LI YONGTAO (author) / WU DAWEI (author)

    Publication date :

    2024-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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