The present invention relates to a method for estimating a minimum run distance for takeoff of an aircraft. According to the present invention, A minimum runway length required for the takeoff of the aircraft from a runway in a confined environment, such as an aircraft carrier flight deck, is estimated. Therefore, a reliable estimation result can be obtained only with aircraft performance without a complicated flight dynamics formula. The method for estimating the minimum run distance for the takeoff of the aircraft of the present invention comprises: a definition step; a first estimation step; a second estimation step; a third estimation step; and a summation step.

    본 발명은 항공모함 비행갑판과 같이 제한된 환경의 활주로에서 항공기의 이륙을 위해 필요한 최소한의 활주로 길이를 추정함으로써 복잡한 비행역학 공식 없이도 항공기 성능만으로 신뢰할 만한 추정결과를 얻을 수 있는 항공기 이륙을 위한 최소 활주거리 추정 방법에 관한 것이다.


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    Title :

    METHOD FOR ESTIMATING MINIMUM RUN DISTANCE FOR AIRCRAFT TAKE OFF


    Additional title:

    항공기 이륙을 위한 최소 활주거리 추정 방법


    Contributors:

    Publication date :

    2022-10-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    B63B Schiffe oder sonstige Wasserfahrzeuge , SHIPS OR OTHER WATERBORNE VESSELS / B63G OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS , Angriffs- oder Verteidigungsanordnungen auf Schiffen / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen




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