{
  "$type": "site.standard.document",
  "description": "A new axisymmetric Coriolis vibrating gyroscope includes a resonator configured to vibrate in a standing wave; a plurality of control elements; and a control circuitry, configured to iteratively control said control elements so as to maintain an angular direction of said vibration at a current…",
  "path": "/patents/1378536",
  "publishedAt": "2026-02-12T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C19/5776",
    "ISRAEL AEROSPACE INDUSTRIES LTD."
  ],
  "textContent": "A new axisymmetric Coriolis vibrating gyroscope includes a resonator configured to vibrate in a standing wave; a plurality of control elements; and a control circuitry, configured to iteratively control said control elements so as to maintain an angular direction of said vibration at a current setpoint; determine an angular direction of said vibration of said resonator from respective readings of at least two of said control elements; calculate a total angular rate; and update said setpoint to an angular direction of said vibration determined in a previous iteration",
  "title": "OPERATIONAL MODE FOR AXISYMMETRIC CORIOLIS VIBRATING GYROSCOPES"
}