Provided are a fixed wing unmanned aerial vehicle and a method for operating the same. The fixed wing unmanned aerial vehicle includes, but is not limited to, a failure detection system configured to detect faults in one or more of the plurality of components, a capability evaluation system communicatively coupled to the failure detection system and configured to determine a capability level of the fixed wing unmanned aerial vehicle based on the faults in the one or more of the plurality of components, and a trajectory generation system communicatively coupled to the failure detection system and the capability evaluation system and configured to generate a touch down trajectory for the fixed wing unmanned aerial vehicle based on the determined capability level of the fixed wing unmanned aerial vehicle, wherein the touch down trajectory comprises a stall maneuver configured to minimize a lateral energy of the fixed wing unmanned aerial vehicle when the determined capability level is below a predetermined threshold.

    고정익 무인 항공기 및 이를 작동시키는 방법이 제공된다. 고정익 무인 항공기는, 이에 한정되지 않는, 복수의 컴포넌트들 중 하나 이상에서 고장을 검출하도록 구성된 고장 검출 시스템, 고장 검출 시스템에 통신가능하게 결합되고, 복수의 컴포넌트들 중 하나 이상에서의 고장에 기초하여 고정익 무인 항공기의 역량 수준을 결정하도록 구성된 역량 평가 시스템, 및 고장 검출 시스템 및 역량 평가 시스템에 통신가능하게 결합되고, 고정익 무인 항공기의 결정된 역량 수준에 기초하여 고정익 무인 항공기의 착지 궤적을 생성하도록 구성된 궤적 생성 시스템을 포함할 수 있고, 결정된 역량 수준이 사전결정된 임계치 미만이면, 착지 궤적은 고정익 무인 항공기의 측방향 에너지를 최소화하도록 구성된 실속 기동을 포함한다.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    - UNMANNED AERIAL VEHICLE OFF-SITE LANDING SYSTEM


    Weitere Titelangaben:

    무인 항공기 오프-사이트 랜딩 시스템


    Beteiligte:
    YANG LIU (Autor:in) / ALAN BRUCE HICKMAN (Autor:in) / XIAODONG CHEN (Autor:in) / SHUAI CHEN (Autor:in) / WENWAN FENG (Autor:in) / LEI ZHANG (Autor:in) / YUNFEI ZOU (Autor:in)

    Erscheinungsdatum :

    2020-10-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Unmanned aerial vehicle off-site landing system

    LIU YANG / HICKMAN ALAN BRUCE / CHEN XIAODONG et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    UNMANNED AERIAL VEHICLE OFF-SITE LANDING SYSTEM

    LIU YANG / HICKMAN ALAN BRUCE / CHEN XIAODONG et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    Unmanned aerial vehicle landing platform and unmanned aerial vehicle landing system

    ZHANG DULI / GONG YUSHUAI | Europäisches Patentamt | 2023

    Freier Zugriff

    UNMANNED AERIAL VEHICLE LANDING PLATFORM AND UNMANNED AERIAL VEHICLE LANDING SYSTEM

    ZHANG DULI / GONG YUSHUAI | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle landing platform, unmanned aerial vehicle landing control method and unmanned aerial vehicle system

    CUI PENG / GONG YUSHUAI / XU LIJUN et al. | Europäisches Patentamt | 2023

    Freier Zugriff