{
  "$type": "site.standard.document",
  "description": "The method involves transforming an acceleration setpoint by predetermined relationships into a required longitudinal attitude setpoint that is transmitted to an automatic system (26). The acceleration setpoint is transmitted into a required load factor setpoint in a longitudinal direction of an…",
  "path": "/patents/990262",
  "publishedAt": "2013-05-29T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C23/00",
    "EUROCOPTER FRANCE [FR]"
  ],
  "textContent": "The method involves transforming an acceleration setpoint by predetermined relationships into a required longitudinal attitude setpoint that is transmitted to an automatic system (26). The acceleration setpoint is transmitted into a required load factor setpoint in a longitudinal direction of an aircraft (1) parallel to a roll axis of the aircraft, where the load factor setpoint is transmitted to another automatic system (25) for maintaining the load point by controlling a collective pitch of a set of blades (2') of a propulsion unit to comply with the former setpoint. An independent claim is also included for a device for assisting piloting of a rotary wing aircraft i.e. hybrid aircraft.",
  "title": "Method for assisted piloting of a rotary wing aircraft comprising at least one screw propeller, assisted piloting device and aircraft"
}