The invention discloses a multimodal flight conversion control method for a hybrid layout rotary-wing unmanned aerial vehicle, and relates to the technical field of flight control for unmanned aerial vehicles. Based on composite multimodal multipurpose aircrafts, the hybrid layout rotary-wing unmanned aerial vehicle comprises five types of flight modal; and aiming at a take-off/air-drop stage, a task arriving stage, a task executing stage, a task evacuating stage and a landing/recovery stage respectively, the multimodal flight conversion control method provides seven modal conversion modes and conversion opportunities. According to the multimodal flight conversion control method provided by the invention, the hybrid layout rotary-wing unmanned aerial vehicle can be reasonably converted among various modal types to meet different task requirements, and the multimodal flight capability and the multitask capability of the hybrid layout rotary-wing unmanned aerial vehicle can be sufficiently exerted; and the general land take-off and landing capability of the hybrid layout rotary-wing unmanned aerial vehicle can be sufficiently exerted, the flexible water-surface/carrier-borne/vehicle-mounted/airborne drop and other deployment modes of the hybrid layout rotary-wing unmanned aerial vehicle can be utilized, and the high-speed cruise capability and the low-altitude and low-speed capability of the hybrid layout rotary-wing unmanned aerial vehicle can be sufficiently exerted, so as to achieve the rapid arriving and evacuating as well as low-speed and low-altitude task executing capabilities of the hybrid layout rotary-wing unmanned aerial vehicle.


    Access

    Download


    Export, share and cite



    Title :

    Multimodal flight conversion control method for hybrid layout rotary-wing unmanned aerial vehicle


    Contributors:
    CAI ZHIHAO (author) / LIN QING (author) / YAN KUN (author) / WANG YINGXUN (author)

    Publication date :

    2016-01-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    ROTARY-WING UNMANNED AERIAL VEHICLE

    LEUSCHNER ANDRIES | European Patent Office | 2019

    Free access

    ROTARY-WING UNMANNED AERIAL VEHICLE

    LEUSCHNER ANDRIES HERMANN | European Patent Office | 2023

    Free access

    ROTARY-WING UNMANNED AERIAL VEHICLE

    LEUSCHNER ANDRIES HERMANN | European Patent Office | 2021

    Free access

    Wing structure of unmanned aerial vehicle and light flying wing layout unmanned aerial vehicle

    CHENG JIALIN / ZHI YAFEI / WANG JUE et al. | European Patent Office | 2024

    Free access

    Flying wing layout unmanned aerial vehicle stability augmentation control method

    ZOU YANG / ZHANG QUHUI / XIAO BEN | European Patent Office | 2021

    Free access