Patent · US Active

Piloting assistance system and method for an aircraft

US11735056B2 · kind B2 · utility

0Cited by
3References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 16, 2019
Grant dateAug 22, 2023
Priority date
Expiry dateJul 12, 2040

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/55
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A piloting assistance system for an aircraft comprises a flight management computer and a guidance computer. The flight management computer transmits speed setpoints to the guidance computer so as to pilot the aircraft in accordance with an initial speed profile or in accordance with an RTA speed profile following the reception of an RTA constraint. In response to the reception of a setpoint speed selected by a flight crew member in the presence of the RTA constraint, the guidance computer pilots the aircraft at the selected speed and the flight management computer determines a deselection point for returning to a predetermined speed profile while still complying with the RTA constraint. The guidance computer commands the display, on a navigation screen, of a symbol corresponding to the position of the deselection point.

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