{
  "$type": "site.standard.document",
  "description": "The invention provides a method for determining a position error correction on a static pressure measurement at an aircraft flying through a flow field by means of a Taylor expansion series. The method comprises determining the constants of such a Taylor expansion series by the successive steps of…",
  "path": "/patents/1415099",
  "publishedAt": "2023-08-02T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C23/00",
    "STICHTING NATIONAAL LUCHT EN RUIMTEVAART LABORATORIUM [NL]"
  ],
  "textContent": "The invention provides a method for determining a position error correction on a static pressure measurement at an aircraft flying through a flow field by means of a Taylor expansion series. The method comprises determining the constants of such a Taylor expansion series by the successive steps of an initial determination using computational fluid dynamics and a 3D scan of the aircraft, a validation of the results by low altitude flyby's at a ground station and an extrapolation of the results to altitude by performing flight tests at constant altitude and conditions of constant atmospheric pressure.",
  "title": "METHOD FOR DETERMINING A POSITION ERROR CORRECTION ON A STATIC PRESSURE MEASUREMENT AT AN AIRCRAFT"
}