{
"$type": "site.standard.document",
"description": "We propose a motor control system (1), preferably for an aircraft, most preferably for a passenger and/or load carrying multi-rotor aircraft, comprising: a plurality of motors (3), preferably electric motors, each of said motors having a motor control unit (2) for controlling a corresponding motor…",
"path": "/patents/1420727",
"publishedAt": "2024-07-10T00:00:00.000Z",
"site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
"tags": [
"B64C27/08",
"VOLOCOPTER GMBH [DE]"
],
"textContent": "We propose a motor control system (1), preferably for an aircraft, most preferably for a passenger and/or load carrying multi-rotor aircraft, comprising: a plurality of motors (3), preferably electric motors, each of said motors having a motor control unit (2) for controlling a corresponding motor (3), each of said motor control units (2) comprising a primary motor controller (COM) being devised for providing motor control commands (9) to said corresponding motor (3);said motor control system (1) further comprising: a system control unit (COMstring) in communication connection with each of said plurality of primary motor controllers (COM), said system control unit (COMstring) being devised for providing motor control commands (9) to said primary motor controllers (COM); a system monitoring unit (MONstring) in connection with said system control unit (COMstring) for monitoring an operation thereof; at least one sensor means (4) for determining an operation state of at least one of said plurality of motors (3), said sensor means (4) in operative connection with said system monitoring unit (MONstring); wherein said system monitoring unit (MONstring) is devised to disable communication between said system control unit (COMstring) and said primary motor controllers (COM) and/or between said primary motor controllers (COM) and said motors (3) based on an outcome of said monitoring and/or of said determining.",
"title": "MOTOR CONTROL SYSTEM, METHOD OF OPERATING A MOTOR CONTROL SYSTEM AND AIRCRAFT"
}