{
  "$type": "site.standard.document",
  "description": "A system for determining a deceleration rate of an aircraft, in various embodiments, includes at least one component capable of transmitting a first deceleration rate. The system also includes a brake control unit coupled to the at least one component and having a brake controller that is…",
  "path": "/patents/928140",
  "publishedAt": "2017-04-12T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T8/1703",
    "GOODRICH CORP [US]"
  ],
  "textContent": "A system for determining a deceleration rate of an aircraft, in various embodiments, includes at least one component capable of transmitting a first deceleration rate. The system also includes a brake control unit coupled to the at least one component and having a brake controller that is configured to receive the first deceleration rate from the at least one component and to determine a likely accurate deceleration rate based on the first deceleration rate, a second deceleration rate and a hierarchy of sources of deceleration rates.",
  "title": "IMPROVED ROBUSTNESS AND AVAILABILITY OF AIRCRAFT ACCELERATION EVALUATION"
}