Patent · US Active

Display of aircraft altitude

US9989378B2 · kind B2 · utility

2Cited by
3References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 15, 2014
Grant dateJun 5, 2018
Priority date
Expiry dateJan 15, 2034

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01C23/00
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A method for displaying an attitude of an aircraft includes receiving a roll angle, a pitch angle and a yaw angle of the aircraft, generating a display image indicating the roll angle, the pitch angle and the yaw angle, and displaying the display image on a display device. The display image includes a spherical shell with a track angle scale projected onto the spherical shell along a latitude line of the spherical shell and with a pitch angle scale projected onto the spherical shell along a longitude line of the spherical shell. Furthermore, the display image includes a graphical aircraft attitude indicator inside the spherical shell rotated with respect to the spherical shell such that the graphical aircraft attitude indicator indicates the roll angle, the pitch angle and the yaw angle of the aircraft with respect to the spherical shell.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.