Method and device for automatic control of an aircraft deceleration in running phase
US6991304B2 · kind B2 · utility
22Cited by
9References
10Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Dec 11, 2001 |
| Grant date | Jan 31, 2006 |
| Priority date | — |
| Expiry date | Dec 11, 2021 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C25/426
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
The invention relates to a system to control the deceleration of an aircraft during the taxiing phase on a landing strip, the system has a detector of the current position of the aircraft on the strip, and of the current speed of the aircraft on the strip, a calculator receiving position and speed values from the detector, to define, as a function of the desired final speed of the aircraft at the so-called final position on the strip, a deceleration set-point modification time, after the current time, and a new deceleration set-point to apply from the modification time, to reach the final position at the desired speed.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.