{
  "$type": "site.standard.document",
  "description": "A control system includes: a VTOL rotor and a cruise rotor configured to generate a thrust; a power unit that has a power generation device configured to generate power and supply the power to the rotors, and a battery configured to store power which is supplied from the power generation device…",
  "path": "/patents/1352194",
  "publishedAt": "2023-10-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64D31/00",
    "HONDA MOTOR CO.,LTD."
  ],
  "textContent": "A control system includes: a VTOL rotor and a cruise rotor configured to generate a thrust; a power unit that has a power generation device configured to generate power and supply the power to the rotors, and a battery configured to store power which is supplied from the power generation device, and supply stored power to the rotors; and a control unit configured to calculate a charging time of the battery based on a required amount of power storage that should be stored in the battery when the aircraft flies in a predetermined flight condition, and a state of the battery, and determine a charge start time of the battery based on the charging time and a flight time it takes to reach the predetermined flight condition. With this, it is possible to suppress a deterioration.",
  "title": "CONTROL SYSTEM AND CONTROL METHOD, AND AIRCRAFT"
}