Flight phase stability indicator system and method
US10514707B1 · kind B1 · utility
Assignee
Inventors
Key dates
| Filing date | Jun 26, 2014 |
| Grant date | Dec 24, 2019 |
| Priority date | — |
| Expiry date | Oct 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.