Patent · US Active

System and method for assisting in the landing of an aircraft

US11928977B2 · kind B2 · utility

0Cited by
6References
12Claims
0Family size

Assignee

Inventor

Key dates

Filing dateNov 1, 2021
Grant dateMar 12, 2024
Priority date
Expiry dateJun 4, 2042

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG08G5/26
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A system for assisting in the landing of an aircraft including a processing unit configured to: during a first phase of a landing runway approach procedure, when the aircraft flies above a predetermined height with respect to a landing runway threshold, determine a bias of position and speed information from an inertia unit of the aircraft, as a function of the merged position and speed information determined as a function of information from a receiver of ILS guidance signals and of information from a signal receiver of a satellite navigation system, then, during a second phase of the approach procedure, when the aircraft flies below the predetermined height, determine so-called adjusted aircraft position and speed information by applying, to information from the inertial unit, a correction corresponding to the bias determined during the first phase of the approach procedure.

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