A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    System, a method and a computer program product for maneuvering of an air vehicle with tiltable propulsion unit


    Beteiligte:
    DEKEL GUY (Autor:in) / ZIVAN LIOR (Autor:in) / EFRATY YOAV (Autor:in) / WOLFF AMIT (Autor:in) / VOLOVICK AVNER (Autor:in)

    Erscheinungsdatum :

    2019-11-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen





    SYSTEM METHOD AND COMPUTER PROGRAM PRODUCT FOR MANEUVERING OF AN AIR VEHICLE WITH TILTABLE PROPULSION UNIT

    DEKEL GUY / ZIVAN LIOR / EFRATY YOAV et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    SYSTEM, A METHOD AND A COMPUTER PROGRAM PRODUCT FOR MANEUVERING OF AN AIR VEHICLE WITH TILTABLE PROPULSION UNIT

    DEKEL GUY / ZIVAN LIOR / EFRATY YOAV et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    System, a method and a computer program product for maneuvering of an air vehicle with tiltable propulsion unit

    DEKEL GUY / ZIVAN LIOR / EFRATY YOAV et al. | Europäisches Patentamt | 2017

    Freier Zugriff