{
  "$type": "site.standard.document",
  "description": "A system can include an inertial measurement unit, a magnetometer configured to measure a magnetic field, and a processing system having an ORSE filter. The processing system can be configured to determine an estimated position based on a change in velocity or angular rate based on data received…",
  "path": "/patents/1267358",
  "publishedAt": "2020-07-16T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C21/165",
    "LOCKHEED MARTIN CORPORATION"
  ],
  "textContent": "A system can include an inertial measurement unit, a magnetometer configured to measure a magnetic field, and a processing system having an ORSE filter. The processing system can be configured to determine an estimated position based on a change in velocity or angular rate based on data received from the inertial measurement unit, determine a difference between the measured magnetic field from the magnetometer and the expected magnetic field measurement, and determine a state estimate using the ORSE filter by updating a time propagation of state and covariance with a measurement update of the state and covariance. The processing system can be configured to transform a change in velocity, a change in angulate rate, and the measured magnetic field to an Earth-centered inertial reference frame for the ORSE filter.",
  "title": "TERRESTRIAL LAND AIR AND SEA NAVIGATION SYSTEM"
}