{
  "$type": "site.standard.document",
  "description": "A method and its corresponding system for displaying an intercept point on a synthetic vision display on board a helicopter, wherein the display conforms to the flight path intercepting the terrain when the nose of the helicopter is pitched up during landing. A steep approach during landing may be…",
  "path": "/patents/971909",
  "publishedAt": "2014-07-30T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "G01C23/005",
    "HONEYWELL INT INC [US]"
  ],
  "textContent": "A method and its corresponding system for displaying an intercept point on a synthetic vision display on board a helicopter, wherein the display conforms to the flight path intercepting the terrain when the nose of the helicopter is pitched up during landing. A steep approach during landing may be detected by an evaluation of, for example, attitude of the helicopter, rate of descent, and airspeed.",
  "title": "Method and system for displaying a helicopter terrain intercept point during landing"
}