To provide a flight vehicle controller capable of suppressing the deterioration of a driving source and a battery while suppressing fuel consumption.SOLUTION: A flight vehicle controller 1 includes a generator 2, a driving source 3, a battery 4, an electric motor 5, a battery state detection section 8, and a charged amount control section 11. The battery state detection section 8 detects first charged electric energy which is the current charged amount of the battery. After a flight vehicle starts cruising, the charged amount control section 11 calculates second charged electric energy which is the charged amount of the battery 4 required for takeoff during the next flight, on the basis of flight plans 53 and 54 of the flight vehicle, predicts timing for supplying power from the generator 2 to the battery 4, on the basis of the first charged electric energy and the second charged electric energy, and starts power supply from the generator 2 to the battery 4 at this timing.SELECTED DRAWING: Figure 1

    【課題】燃料消費を抑制しつつ、駆動源及びバッテリの劣化を抑制することができる飛行体の制御装置を提供する。【解決手段】飛行体の制御装置1は、発電機2と、駆動源3と、バッテリ4と、電気モータ5と、バッテリ状態検出部8と、充電量制御部11と、を備える。バッテリ状態検出部8は、バッテリの現在の充電量である第一充電電力量を検出する。充電量制御部11は、飛行体が巡航を開始した後、飛行体の飛行計画53,54に基づいて、次回の飛行時の離陸に必要なバッテリ4の充電量である第二充電電力量を算出し、第一充電電力量及び第二充電電力量に基づいて、発電機2からバッテリ4へ電力を供給するタイミングを予測し、このタイミングにおいて発電機2からバッテリ4への電力供給を開始させる。【選択図】図1


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    Titel :

    FLIGHT VEHICLE CONTROLLER


    Weitere Titelangaben:

    飛行体の制御装置


    Beteiligte:
    HAGA HISAO (Autor:in)

    Erscheinungsdatum :

    2023-07-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Japanisch


    Klassifikation :

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



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