Patent · US Active

Method and device for guiding an aircraft during a low level flight

US9304514B2 · kind B2 · utility

5Cited by

5References

12Claims

0Family size

Assignee

AIRBUS OPERATIONS SAS · FR

Inventors

Boris Kozlow · Toulouse, FR
Yohann Roux · Cugnaux, FR
Julien Nico · Tournefeuille, FR

Key dates

Filing date	Jan 7, 2015
Grant date	Apr 5, 2016
Priority date	—
Expiry date	Jan 7, 2035

Classification

Technology area (CPC G)Physics
CPC primaryG08G5/74
WIPO fieldControl
WIPO sectorInstruments

Abstract

A calculation unit configured to define a safety corridor, whose width is increased compared with a nominal width, at least by one width of an escape trajectory with a spiral climb of the aircraft, wherein the safety corridor that is thus defined by the calculation unit is used by a construction unit for forming a flight trajectory for a low level flight of an aircraft.

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