{
  "$type": "site.standard.document",
  "description": "A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described, the control unit (46, 46') is programmed to receive at input at least a first signal associated with real or simulated flight parameters (ALT, OAT; ALT'…",
  "path": "/patents/1399459",
  "publishedAt": "2025-01-15T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B64C27/00",
    "LEONARDO SPA [IT]"
  ],
  "textContent": "A control unit (46, 46') for an aircraft (1, 1') capable of hovering or for a flight simulation system of the aircraft (1, 1') is described, the control unit (46, 46') is programmed to receive at input at least a first signal associated with real or simulated flight parameters (ALT, OAT; ALT', OAT') of the aircraft (1, 1') and to provide at output a second signal (VNE, VNE') associated with a forward velocity to never exceed of the aircraft (1, 1'); the control unit (46, 46') is programmed to process a third signal (GW, GW') associated with an actual or simulated weight of the aircraft (1, 1'); to associate plurality of tables (T1, T2, .. , Tn) to respective intervals (I1, I2, .. Ij) of values of the third signal (GW, GW'); each table (T1, T2, .. , Tn) associating a plurality of values of the second signal (VNE, VNE') with a respective first signal (ALT, OAT; ALT', OAT'; AEO, OEI, Power off; AEO', OEI', Power off'); and to process the second signal (VNE, VNE'), based on the table (T1, T2, .. , Tn) associated with the relative interval (T1, T2, .. Ij) of the third signal (GW, GW') and the respective first signals (ALT, OAT; ALT', OAT').",
  "title": "CONTROL UNIT AND INDICATOR FOR AN AIRCRAFT CAPABLE OF HOVERING OR FOR A FLIGHT SIMULATION SYSTEM OF SAID AIRCRAFT, AND RELATIVE METHOD FOR ASSISTING THE PERFORMANCE OF A MANEUVRE"
}