{
  "$type": "site.standard.document",
  "description": "The method involves correcting an instruction of braking according to a pitching angle (theta) of an aircraft (1) during braking. The correction process is carried out by subtracting the instruction of braking from a breaking setpoint correction value. The breaking setpoint correction value is…",
  "path": "/patents/990271",
  "publishedAt": "2013-05-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T17/00",
    "MESSIER BUGATTI DOWTY [FR]"
  ],
  "textContent": "The method involves correcting an instruction of braking according to a pitching angle (theta) of an aircraft (1) during braking. The correction process is carried out by subtracting the instruction of braking from a breaking setpoint correction value. The breaking setpoint correction value is calculated according to the pitching angle when the aircraft runs at a ground speed (V) with a lower threshold speed (Vseuil). The breaking setpoint correction value is set to zero when the ground speed is greater than or equal to the threshold speed.",
  "title": "Braking control method for landed airplane, aiming to optimise its pitching anle."
}