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.


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    Title :

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


    Contributors:
    DEKEL GUY (author) / ZIVAN LIOR (author) / EFRATY YOAV (author) / WOLFF AMIT (author) / VOLOVICK AVNER (author)

    Publication date :

    2017-08-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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