Patent · US Active

Assembly for the flight management of an aircraft and method for monitoring guidance instructions for such an assembly

US10261510B2 · kind B2 · utility

1Cited by
3References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 24, 2016
Grant dateApr 16, 2019
Priority date
Expiry dateNov 24, 2036

Classification

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

Abstract

The invention relates to a flight management assembly (1) comprising two guidance chains (2A, 2B), each one provided with a flight management system (3A, 3B), each of said flight management systems (3A, 3B) carrying out at least one calculation of guidance instructions for the aircraft, the flight management assembly (1) also comprising at least one monitoring unit (4A, 4B) designed to monitor the guidance instructions calculated by the two flight management systems (3A, 3B) in such a way as to be able to detect and identify a defective flight management system, the monitoring unit (4A, 4B) comprising a monitoring device (5) which verifies particularly whether the following three conditions are met: a first derivative of extrapolated cross tracks is positive; a second derivative of extrapolated cross tracks is positive; and extrapolated positions of the aircraft are on the same side of an active segment of the flight plan followed by the aircraft as the current position of the aircraft.

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