To provide a flight vehicle controller capable of suppressing the deterioration of a battery while maintaining a flight state.SOLUTION: A flight vehicle controller 1 includes a generator 11, a driving source 12, a battery 13, an electric motor 3, a rotor blade 4, a battery state detection section 5, a variable pitch mechanism 6, and a pitch change control section 7. The electric motor 3 is driven by power supplied from at least one of the generator 11 and the battery 13. The rotor blade 4 is driven by the electric motor 3. The battery state detection section 5 detects the state of charge of the battery 13. The variable pitch mechanism 6 changes the pitch of the rotor blade 4. The pitch change control section 7 determines whether to change the pitch of the rotor blade 4, on the basis of the charging rate of the battery detected by the battery state detection section 5.SELECTED DRAWING: Figure 1

    【課題】飛行状態を維持しつつ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11と、駆動源12と、バッテリ13と、電気モータ3と、回転翼4と、バッテリ状態検出部5と、可変ピッチ機構6と、ピッチ変更制御部7と、を備える。電気モータ3は、発電機11及びバッテリ13の少なくとも一方から供給される電力により駆動される。回転翼4は、電気モータ3により駆動される。バッテリ状態検出部5は、バッテリ13の充電状態を検出する。可変ピッチ機構6は、回転翼4のピッチを変更する。ピッチ変更制御部7は、バッテリ状態検出部5により検出されたバッテリの充電率に基づいて、回転翼4のピッチを変更するか否かを判定する。【選択図】図1


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    Title :

    FLIGHT VEHICLE CONTROLLER


    Additional title:

    飛行体の制御装置


    Contributors:
    HAGA HISAO (author)

    Publication date :

    2023-07-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

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



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