{
  "$type": "site.standard.document",
  "description": "An antiskid brake control system, comprising: a brake control unit, BCU (150); a wheel/brake assembly (132,134) comprising a wheel (24), a brake stack (26), and an actuator (28) configured to apply a braking force onto the brake stack; and a wheel speed sensor (27) in electronic communication with…",
  "path": "/patents/1399416",
  "publishedAt": "2025-06-25T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B60T8/1703",
    "GOODRICH CORP [US]"
  ],
  "textContent": "An antiskid brake control system, comprising: a brake control unit, BCU (150); a wheel/brake assembly (132,134) comprising a wheel (24), a brake stack (26), and an actuator (28) configured to apply a braking force onto the brake stack; and a wheel speed sensor (27) in electronic communication with the BCU, the wheel speed sensor configured to detect a wheel speed corresponding to the wheel; wherein the BCU is configured to: receive an aircraft mass from an avionics unit; calculate an aircraft kinetic energy; generate an antiskid brake command signal based upon the aircraft kinetic energy; and send the antiskid brake command signal to a brake control component for controlling the braking force.",
  "title": "SYSTEMS AND METHODS FOR AIRCRAFT ANTISKID BRAKING"
}