Load volume predication for slung loads of aerial vehicles are disclosed. A system can identify parameters of a load. The system can determine a volume occupied by a superposition of locations of the cone. The system can receive from sensors or models, characteristics of an environment associated with the aerial vehicle or the load. The system can detect an obstacle in the environment. The system can take a navigational action in response to detecting the obstacle.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HELICOPTER OBSTACLE AVOIDANCE WITH SLUNG LOAD


    Beteiligte:

    Erscheinungsdatum :

    14.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Helicopter obstacle avoidance with slung load

    DADKHAH TEHRANI NAVID / CARLSON SEAN S / POLYCARPE CAUVIN | Europäisches Patentamt | 2025

    Freier Zugriff

    Helicopter Slung Load Simulations Using Heli-Dyn+

    Gursoy, Gonenc / Tarimci, Onur / Yavrucuk, Ilkay | AIAA | 2012


    Helicopter Slung Load Simulations Using Heli-Dyn+

    Gursoy, G. / Tarimci, O. / Yavrucuk, I. et al. | British Library Conference Proceedings | 2012


    Helicopter Slung Load Stablization Using a Flight Director

    Mamers, M. / Bower, G. / American Helicopter Society | British Library Conference Proceedings | 2005


    HELICOPTER TRAJECTORY OPTIMIZATION AFTER AERIAL SLUNG LOAD RELEASE

    Wang, Luofeng / Chen, Renliang / Yan, Xufei | British Library Conference Proceedings | 2019