To provide a multicopter which enables improvement of accuracy of position control under a situation that a thrust force (for example, a thrust force generated by driving of a cooling fan and exhaust air) acts.SOLUTION: In one embodiment of the disclosure, a multicopter 1 has an engine 41, a generator 42, and a cooling fan 43 which drives to generate airflow that cools the engine 41 and the generator 42 and further has a rotation control part 38 which rotates the multicopter 1 or the cooling fan 43. The cooling fan 43 is disposed so that a direction of a center axis FA of the cooling fan 43 is set to a horizontal direction. The rotation control part 38 performs wind direction facing rotation control which rotates the multicopter 1 or the cooling fan 43 so that a direction of a horizontal vector of a thrust vector generated by driving of the cooling fan 43 substantially faces a direction of a horizontal vector of a window force vector.SELECTED DRAWING: Figure 3

    【課題】推力(例えば、冷却ファンの駆動や排気により発生する推力)が作用する状況下にて位置制御の精度を向上させることができるマルチコプタを提供する。【解決手段】本開示の一態様は、エンジン41と、ジェネレータ42と、エンジン41とジェネレータ42とを冷却する気流を発生させるために駆動する冷却ファン43と、を有するマルチコプタ1において、マルチコプタ1または冷却ファン43を回転させる回転制御部38を有し、冷却ファン43は、当該冷却ファン43の中心軸FA方向が水平方向となるように配置されており、回転制御部38は、冷却ファン43の駆動により発生する推力ベクトルのうち水平方向のベクトルの向きと、風力ベクトルのうち水平方向のベクトルの向きとが略対向するように、マルチコプタ1または冷却ファン43を回転させる風向対向回転制御を行う。【選択図】図3


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    Title :

    MULTICOPTER


    Additional title:

    マルチコプタ


    Contributors:

    Publication date :

    2020-11-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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