Method and device for optimizing the landing of an aircraft on a runway
US9547312B2 · kind B2 · utility
4Cited by
1References
15Claims
0Family size
Assignee
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Key dates
| Filing date | Jan 19, 2015 |
| Grant date | Jan 17, 2017 |
| Priority date | — |
| Expiry date | Jan 23, 2035 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/80
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
A guiding unit and a computation unit, the computation unit comprising elements for saturating, if necessary, a usual optimized slope for the landing, following a comparison with a slope computed on the basis of a performance criterion relative to a deceleration capability of the aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.