{
  "$type": "site.standard.document",
  "description": "The invention relates to a camera body for an airborne or spaceborne surveying device adapted to be mounted on an aircraft or satellite and to survey the earth surface, the camera body comprising an optics interface configured for receiving projection optics, a holder coupled with the optics…",
  "path": "/patents/1409746",
  "publishedAt": "2025-09-24T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C11/02",
    "LEICA GEOSYSTEMS AG [CH]"
  ],
  "textContent": "The invention relates to a camera body for an airborne or spaceborne surveying device adapted to be mounted on an aircraft or satellite and to survey the earth surface, the camera body comprising an optics interface configured for receiving projection optics, a holder coupled with the optics interface, a sensor arranged on the holder and configured for being movable relative to the optics interface along a stabilisation axis, the stabilisation axis to be aligned with a movement direction of the aircraft or satellite relative to the earth surface, circuitry connected to the sensor and configured for generating surveying data, the holder comprising a first frame and a first movable part that is connected to the first frame via a first solid-state joint, the sensor arranged on the first movable part, the first solid-state joint configured for providing a movability of the first movable part relative to the first frame along the stabilisation axis, a motor having a mover and a stator, the motor connected to the circuitry, the mover operatively linked with the first movable part, and the stator fixedly arranged relative to the first frame. The invention further relates to an airborne or spaceborne surveying device adapted to be mounted on an aircraft or a satellite and to survey the earth surface, comprising at least one camera with projection optics and a camera body according to the description herein.",
  "title": "CAMERA BODY WITH MECHANICAL FMC STABILZATION FOR AN AIRBORNE OR SPACEBORNE SURVEYING DEVICE"
}