{
  "$type": "site.standard.document",
  "coverImage": {
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  "description": "An aircraft controller , aircraft braking system and method for determining braking parameters. The aircraft controller is configured to determine information associated with an aircraft taxiing route associated with an aircraft . On the basis of the information, the aircraft controller determines…",
  "path": "/patents/1329277",
  "publishedAt": "2022-10-13T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T8/1703",
    "AIRBUS OPERATIONS LIMITED"
  ],
  "textContent": "An aircraft controller , aircraft braking system and method for determining braking parameters. The aircraft controller is configured to determine information associated with an aircraft taxiing route associated with an aircraft . On the basis of the information, the aircraft controller determines a first braking parameter for a first main landing gear of the aircraft and a second braking parameter for a second main landing gear of the aircraft during a landing event. The first and second braking parameters are determined to result in asymmetrical braking between the first and second main landing gears during the landing event.",
  "title": "AIRCRAFT BRAKING SYSTEM"
}