Dynamic determination method for determining the position of a stopping point of an aircraft on a landing strip and related system
US11069248B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Mar 1, 2019 |
| Grant date | Jul 20, 2021 |
| Priority date | — |
| Expiry date | Sep 17, 2039 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG08G5/21
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A dynamic determination method for determining the position of a stopping point of an aircraft on a landing strip and related system includes determining a first table of average time from touchdown of the aircraft as a function of the ground speed, based on an average deceleration profile of the aircraft; determining a first deceleration profile adapted to the current conditions, based on an engine thrust computed for each ground speed from the average time determined in the first table; determining a second table of time adapted to the current conditions based on the first deceleration profile; determining a second deceleration profile adapted to the current conditions, based on an engine thrust computed for each ground speed from the time determined in the second table; and computing the position of the stopping point from the second adapted deceleration profile.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.