To accurately determine whether or not an aircraft can land.SOLUTION: A landing determination control system for determining whether or not an aircraft can land at a target landing point, comprises a control unit for determining whether or not the aircraft can land by using parameters for estimating a landing performance of the aircraft. The control unit executes the steps of: obtaining a motion response of the aircraft that is operated by inputting a motion signal to the aircraft; estimating the landing performance of the aircraft based on the parameters related to the obtained motion response; and determining whether or not the aircraft can land based on the estimation results.SELECTED DRAWING: Figure 2

    【課題】航空機の着地の可否を正確に判定する。【解決手段】航空機の目標着地点への着地の可否を判定する着地判定制御システムにおいて、前記航空機の着地性能を推定するためのパラメータを用いて、着地の可否を判定する制御部を備え、前記制御部は、前記航空機へ動作信号を入力することで動作する前記航空機の動作応答を取得するステップと、取得した前記動作応答に関する前記パラメータに基づいて、前記航空機の着地性能を推定し、推定結果に基づいて、着地の可否を判定するステップと、を実行する。【選択図】図2


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    Title :

    LANDING DETERMINATION CONTROL SYSTEM, AIRCRAFT, AND LANDING DETERMINATION METHOD


    Additional title:

    着地判定制御システム、航空機及び着地判定方法


    Contributors:
    KOJIMA TORU (author) / MORI TOMOHITO (author)

    Publication date :

    2024-08-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64U / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / 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