To prevent deformation and damage of a flying body caused by correction of an attitude of a position and a direction of the flying body, when the attitude is corrected after the flying body lands on a stage.SOLUTION: When a flying body 32 lands on a landing and takeoff surface 12a, a control device 16 moves any one position correction mechanism of position correction mechanisms 18R and 18L toward a center line O, and thereby corrects the attitude of the flying body 32. Then, the control device 16 moves the other position correction mechanism toward the center line O. Thereby, the flying body 32 is gripped by the position correction mechanisms 18R and 18L. When the flying body 32 lands on the position on the position correction mechanism 18 side, for example, the control device 16 previously moves the position correction mechanism 18R, and then moves the position correction mechanism 18L.SELECTED DRAWING: Figure 8

    【課題】飛行体がステージ上に着陸した後に飛行体の位置や向き等の姿勢を矯正する場合に、その矯正に起因する飛行体の変形や破損を防止すること。【解決手段】飛行体32が離着陸面12a上に着陸した場合、制御装置16は、位置矯正機構18R,18Lのいずれか一方の位置矯正機構を中心線Oに向けて移動させることで、飛行体32の姿勢を矯正する。その後、制御装置16は、他方の位置矯正機構を中心線Oに向けて移動させる。これにより、位置矯正機構18R,18Lによって飛行体32が把持される。例えば、飛行体32が、位置矯正機構18側の位置に着陸した場合、制御装置16は、先に位置矯正機構18Rを移動させ、その後、位置矯正機構18Lを移動させる。【選択図】図8


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    Title :

    LANDING AND TAKEOFF ASSISTING DEVICE


    Additional title:

    離着陸補助装置


    Contributors:

    Publication date :

    2023-12-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    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 / B64C AEROPLANES , Flugzeuge



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