{
  "$type": "site.standard.document",
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  "description": "Aircraft display system, comprising: - a display; - a display generation assembly on the display, capable of dynamically displaying on the display at least one horizon line (52), a slope scale (56) of the aircraft relative to the horizon line (52) and a speed vector symbol (60), representative of…",
  "path": "/patents/932890",
  "publishedAt": "2016-12-28T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T11/101",
    "DASSAULT AVIAT [FR]"
  ],
  "textContent": "Aircraft display system, comprising: - a display; - a display generation assembly on the display, capable of dynamically displaying on the display at least one horizon line (52), a slope scale (56) of the aircraft relative to the horizon line (52) and a speed vector symbol (60), representative of the slope of the aircraft relative to the horizon line (52). [0002] The display generation assembly is suitable for displaying, when approaching a landing runway (13), a rounding guidance symbol (64), the position of the rounding guidance symbol (64) on the display depending on the topographical slope of the landing runway (13) being approached.",
  "title": "DISPLAY SYSTEM OF AN AIRCRAFT, COMPRISING A FLARE GUIDING CUE AND RELATED METHOD"
}