{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
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  "description": "A gyrometer (7) is arranged at the vibration node of a fuselage (2). Each accelerometer (5,6) is arranged at the vibration antinode of the fuselage. The gyrometer and accelerometers are connected to a flight control computer (12) such that measurement signals from the gyrometer and accelerometers…",
  "path": "/patents/1092603",
  "publishedAt": "2003-10-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C21/166",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "A gyrometer (7) is arranged at the vibration node of a fuselage (2). Each accelerometer (5,6) is arranged at the vibration antinode of the fuselage. The gyrometer and accelerometers are connected to a flight control computer (12) such that measurement signals from the gyrometer and accelerometers are used as flight control parameters.",
  "title": "Fly-by wire-controlled aircraft with a flexible and vibratable body"
}