{
  "$type": "site.standard.document",
  "description": "The indicator has a central processing unit (3) determining a trajectory change of an aircraft based on a vertical or lateral change. A display unit (5) presents, on a head up display (7), four indication units with two indicating a nearest vertical change and another two indicating a nearest…",
  "path": "/patents/1072299",
  "publishedAt": "2005-11-23T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C23/00",
    "AIRBUS FRANCE [FR]"
  ],
  "textContent": "The indicator has a central processing unit (3) determining a trajectory change of an aircraft based on a vertical or lateral change. A display unit (5) presents, on a head up display (7), four indication units with two indicating a nearest vertical change and another two indicating a nearest lateral change. The unit is formed to present two indication units indicating the trajectory change closer to an actual position of the aircraft. An independent claim is also included for an aircraft comprising a steering indicator.",
  "title": "Aircraft cockpit indicator"
}