Patent · US Active

Method for aiding navigation for an aircraft during descent and during approach at reduced thrust

US9188978B2 · kind B2 · utility

9Cited by
0References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 23, 2014
Grant dateNov 17, 2015
Priority date
Expiry dateOct 23, 2034

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/80
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A method for aiding navigation for an aircraft between a descent start point and a computation end point, comprises the computation steps of: collecting a flight plan consisting of a succession of waypoints and of the associated vertical constraints; determining a corridor consisting of a floor trajectory and of a ceiling trajectory defining the minimum and maximum altitudes permitted to the aircraft; splitting the corridor into several cells defined between two waypoints furthest apart and between which the ceiling trajectory is distinct from the floor trajectory; determining for at least one cell a vertical trajectory complying with the altitude constraints and comprising the longest possible IDLE segment; and a step consisting in determining and displaying maneuvering points of the aircraft making it possible to follow the target vertical trajectory.

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