Patent · US Active

Method for assisting in rejoining a vertical descent trajectory and associated device

US8447442B2 · kind B2 · utility

4Cited by
1References
14Claims
0Family size

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Inventors

Key dates

Filing dateDec 2, 2010
Grant dateMay 21, 2013
Priority date
Expiry dateOct 1, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/54
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A method is provided for assisting in rejoining a vertical descent trajectory that an aircraft is assumed to have to follow, using a flight management system FMS embedded onboard the aircraft, and includes the following steps: calculation of a vertical deviation VDEV, in the vertical plane, between the aircraft and the vertical descent trajectory, and comparison between the vertical deviation VDEV and a predetermined deviation threshold SVDEV; when the vertical deviation VDEV reaches the deviation threshold SVDEV, a step during which the activation of an optimized mode for catching up on the vertical descent trajectory is authorized; if the optimized mode for catching up on the vertical descent trajectory is activated, piloting of the aircraft by the flight management system FMS in optimized catch-up mode, that is to say at minimum thrust with a target rejoining speed in level VCRP and a target rejoining speed in downward trajectory, the target rejoining speed in level VCRP being equal to the maximum L/D ratio speed of the aircraft uprated by a first value V1 of between 5 and 15 knots, and the target rejoining speed in downward trajectory VCRD being equal to the maximum operating s…

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