CONTROL DEVICE

In a control device (110) including a control unit (112) that controls an EPU (10) for powering a rotor (30) included in an electric aircraft (20), the EPU includes a motor (11), an inverter (121), a control circuit (122), and a first sensor (13, 14, 15) that detects an operation-related value. If t...

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Bibliographische Detailangaben
Hauptverfasser:	FUJII, Keita, KAWAZU, Shinsuke, TAKEMURA, Yuichi, FUKUSHI, Masato
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	In a control device (110) including a control unit (112) that controls an EPU (10) for powering a rotor (30) included in an electric aircraft (20), the EPU includes a motor (11), an inverter (121), a control circuit (122), and a first sensor (13, 14, 15) that detects an operation-related value. If there is no a sudden change in the operation-related value detected by the first sensor, the control unit controls the EPU based on the operation-related value detected by the first sensor. When the sudden change occurs, the control unit stops using the operation-related value detected by the first sensor to control the EPU. After the occurrence of the sudden change, when the sudden change ends before a predetermined period elapses, the control unit resumes using the operation-related value detected by the first sensor to control the EPU, and when the sudden change has not ended, the control unit continues the stoppage.