The invention relates to an unmanned aerial vehicle rotor disturbance correction method and device, and the method comprises the steps: constructing an unmanned aerial vehicle wind speed measurement simulation numerical model based on an environment flight envelope and unmanned aerial vehicle flight parameters; the environment flight envelope is used for setting a mapping relation of flight parameters of the unmanned aerial vehicle in an environment scene; and setting simulation parameters in the unmanned aerial vehicle wind speed simulation numerical model and carrying out a simulation experiment to obtain an estimated quantity of the drainage disturbance influence of the rotation of the unmanned aerial vehicle rotor wing. Fluid simulation under different flight envelope conditions is carried out on an unmanned aerial vehicle wind speed measurement system, the disturbance influence of unmanned aerial vehicle rotors on measurement of an anemograph is estimated according to the difference between a wind speed simulation value at the position of the anemograph and a set value, and an estimated value is obtained and then substituted into an unmanned aerial vehicle motion and attitude compensation algorithm. Therefore, the influence of the disturbance of the rotor wing on the measurement result of the anemograph and the influence caused by the attitude, movement and acceleration of the unmanned aerial vehicle can be corrected, and a more accurate three-dimensional wind speed measurement result can be obtained.

    本发明涉及一种无人机旋翼扰动校正方法及装置,所述方法包括基于环境飞行包线和无人机飞行参数,构建无人机风速测量仿真数值模型;所述环境飞行包线用于设置无人机飞行参数在环境场景中的映射关系;在所述无人机风速仿真数值模型中设置仿真参数并进行仿真实验,得到无人机旋翼旋转的引流扰动影响的估算量。本发明通过对无人机风速测量系统开展不同飞行包线条件下的流体仿真,根据风速仪位置处的风速模拟值与设定值之差估算无人机旋翼对风速仪测量的扰动影响得到估算值,然后代入无人机运动与姿态补偿算法中,以实现校正因旋翼扰动对风速仪测量结果的影响,以及由于无人机的姿态、运动及其加速导致的影响,获取更为准确的三维风速测量结果。


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    Title :

    Unmanned aerial vehicle rotor disturbance correction method and device


    Additional title:

    无人机旋翼扰动校正方法及装置


    Contributors:
    KO SANG WOO (author) / ZHANG KUI (author) / GUO JUNFEI (author) / LI JINQIAO (author) / LIU HONGTAO (author)

    Publication date :

    2023-02-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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