Patent · US Active

Flight phase stability indicator system and method

US10514707B1 · kind B1 · utility

3Cited by
5References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 26, 2014
Grant dateDec 24, 2019
Priority date
Expiry dateOct 19, 2035

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/0684
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A flight phase stability indicator system and method for generating and presenting stability indicator(s) are disclosed. A processor receives flight phase data representative of an identification of a current operational flight phase; receives navigation data comprised of aircraft position, a planned flight trajectory, and runway data if runway data is needed for the current operational flight phase; determines stability data representative of a stability of the current operational flight phase based upon at least the navigation data; generates presentation data responsive to the determination and representative of the flight phase stability indicator and/or presentation(s) of flight phase stability; and presents the indicator represented in the presentation data on or through a presentation unit comprised of a visual display, aural advisory unit, and/or tactile advisory unit.

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