SOLUTION: To provide a control device 10 including a power system 28 of an air vehicle 12 that can supply power to electrical loads 38, 44 including a VTOL motor 54 and a cruise motor 56, an acquisition unit 86, a determination unit 88 that determines whether a power surplus state can occur in which surplus power P8, obtained by subtracting power consumption P4 to P7 from the sum of generated power P1 and regenerated power P2, P3, is greater than the maximum inputtable power, and a control unit 90 that can execute power consumption increase control to increase power consumption by reducing operating efficiency of the cruise motor when the determination unit determines that a power surplus state can occur.SELECTED DRAWING: Figure 1
【解決手段】飛行体12の電力システム28は、VTOLモータ54とクルーズモータ56とを含む電気負荷38、44に電力を供給し得る。制御装置10は、取得部86と、発電電力P1と回生電力P2、P3との和から消費電力P4~P7を減じた余剰電力P8が、最大入力可能電力より大きくなる状態である電力余剰状態が生じ得るか否かを判定する判定部88と、電力余剰状態が生じ得ると判定部が判定した場合に、クルーズモータにおける運転効率を低下させることにより消費電力を増加させる消費電力増加制御を実行し得る制御部90と、を備える。【選択図】図1
CONTROL DEVICE AND FLYING VEHICLE
制御装置及び飛行体
10.10.2024
Patent
Elektronische Ressource
Japanisch
IPC: | H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02H EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS , Schutzschaltungsanordnungen |
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