{
  "$type": "site.standard.document",
  "description": "This inertial navigation unit comprises a navigation data acquisition unit (1) and a first navigation stage (2) capable of calculating hybrid navigation values by combining navigation data. It further includes a second navigation stage (3) capable of calculating certified navigation values…",
  "path": "/patents/1363350",
  "publishedAt": "2024-05-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C21/16",
    "SAFRAN ELECTRONICS & DEFENSE"
  ],
  "textContent": "This inertial navigation unit comprises a navigation data acquisition unit (1) and a first navigation stage (2) capable of calculating hybrid navigation values by combining navigation data. It further includes a second navigation stage (3) capable of calculating certified navigation values independently of the hybrid navigation values, said certified navigation values being certified with a geolocation error limit",
  "title": "METHOD AND UNIT FOR CALCULATING INERTIAL NAVIGATION DATA"
}