최소 1개 틸트식 추진 유닛을 구성하는 항공기의 감속 프로세스를 제어하도록 형상화된 컨트롤 시스템으로, 1개 이상의 각각의 틸트식 추진 유닛은 틸팅이 가능하여 적어도 항공기를 기준으로 한 일반 세로 추력 벡터 방향과 일반 수직 추력 벡터 방향 사이에서 방향이 변경될 수 있는 추력을 제공할 수 있다.

    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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    Titel :

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


    Weitere Titelangaben:

    틸트식 추진 유닛을 가진 항공기 조종을 위한 시스템, 방법 및 컴퓨터 프로그램 제품


    Erscheinungsdatum :

    2018-04-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

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




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