{
  "$type": "site.standard.document",
  "description": "The method involves automatically controlling a flying vehicle (1) when using a longitudinal pitch rate gyro (2), by an automatic controlling unit (8) to rotate the pitch rate gyro around a longitudinal axis (3) by alternating a rotation direction, for eliminating effects of a scaling factor of the…",
  "path": "/patents/996059",
  "publishedAt": "2012-11-14T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F42B10/02",
    "MBDA FRANCE [FR]"
  ],
  "textContent": "The method involves automatically controlling a flying vehicle (1) when using a longitudinal pitch rate gyro (2), by an automatic controlling unit (8) to rotate the pitch rate gyro around a longitudinal axis (3) by alternating a rotation direction, for eliminating effects of a scaling factor of the pitch rate gyro. Correction of drifts is obtained by rotation of the flying vehicle. An independent claim is also included for a pitch rate gyro.",
  "title": "Method for automatically managing a pitch rate gyro mounted on a aircraft"
}