Flight management system of an aircraft

Patent metadata

Field	Value
Publication number	US-10216180-B2
Application number	US-201715422002-A
Country	US
Kind code	B2
Filing date	Feb 1, 2017
Priority date	Nov 26, 2013
Publication date	Feb 26, 2019
Grant date	Feb 26, 2019

Abstract

A flight management system architecture with separate core and supplementary modules. In the core module, generic functionalties relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalties specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of aircraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionaltities that respectively interface with generic and specific man-machine interfaces.

First claim

The invention claimed is:

1. A flight management system of an aircraft, comprising:
a core module configured to implement one or more core functionalities related to a flight management of the aircraft, wherein the core module is implemented in a core partition;
a supplementary module configured to implement one or more supplementary functionalities, wherein the supplementary module is distinct from the core module and the supplementary module is implemented in a supplementary partition; and
an exchange interface configured to exchange messages between the core module and the supplementary module,
wherein the core module comprises a core interface configured to interface with an on-board system of the aircraft including a first generic man-machine interface,
wherein the supplementary module comprises a supplementary interface configured to interface with a second man-machine interface connected to the supplementary module
wherein the core partition and the supplementary partition are at least one of:
(a) temporally segregated such that activities of one of the core partition and the supplementary partition do not affect timings of activities of the other of the core partition and the supplementary partition, and
(b) spatially segregated such that one of the core partition and the supplementary partition is prevented from accessing a memory space of the other of the core partition and the supplementary partition.

2. The flight management system as claimed in claim 1 , wherein the supplementary functionalities are specific to an entity to which the aircraft belongs.

3. The flight management system as claimed in claim 1 , wherein the supplementary interface is configured to enable the supplementary module to access the on-board systems of the aircraft, either directly or indirectly via the core interface.

4. The flight management system as claimed in claim 1 ,
wherein each core functionality of the core module and/or each supplementary functionality of the supplementary module is implemented in at least one of the core partition and the supplementary partition, and
wherein the core and the supplementary functionalities communicate with each other via the exchange interface.

5. The flight management system as claimed in claim 4 , wherein the core and the supplementary functionalities communicate with each other by a mechanism of response to requests respectively addressed to the functionalities.

6. The flight management system as claimed in claim 4 , wherein the core module and the supplementary module are implemented on a same hardware equipment.

7. The flight management system as claimed in claim 4 ,
wherein the core module and the supplementary module are implemented in separate hardware equipment, and
wherein the hardware equipment of the core and supplementary modules communicate via a network.

8. The flight management system as claimed in claim 1 , wherein the at least one of the following core functionalities includes one or more of:
a flight plan management functionality,
a trajectory calculation functionality to calculate a trajectory in space,
a prediction functionality to predict values taken along a given trajectory of the aircraft by physical quantities related to flight conditions,
an extrapolation functionality to extrapolate values taken along a given trajectory of the aircraft by physical quantities related to meteorological conditions based on a given model,
a position calculation functionality to calculate a current position of the aircraft,
a deviation calculation functionality to calculate deviations between the current position of the aircraft and a position of a given theoretical trajectory,
a guidance functionality to generate guidance instructions to guide the aircraft on a given trajectory,
one or more cockpit management functionalities to enable the cockpit of the aircraft to be managed according to a split type philosophy,
an aerodrome identification functionality to identify the aerodromes closest to the current position of the aircraft,
a flight plan transmission functionality to transmit flight plan availability data, and
a flight plan insertion functionality to insert a new flight plan.

9. The flight management system as claimed in claim 1 , wherein the at least one of the following supplementary functionalities includes one or more of:
a search control functionality to control a search to identify closest aerodromes,
a classification functionality to classify, according to criteria chosen by a crew in a request, results obtained in response to the request,
an entity selection functionality to select an entity in response to a request,
a flight plan generation functionality to generate an alternative flight plan to an already established flight plan, and
a flight plan check functionality to check for an availability of a flight plan.

10. The flight management system as claimed in claim 1 , wherein the supplementary functionalities are one or more of:
new functions with respect to the core functions of the core module not provided through the cord module,
alternative functions to the core functions of the core module to which the alternative functions provide behavioral modifications, and/or
supplementary services so as to supplement the core services of the core module which use one of more of the supplementary functionalities.

11. A flight management system of an aircraft, comprising, onboard the aircraft:
a core module that implements one or more core functionalities related to a flight management of the aircraft;
a supplementary module that implements one or more supplementary functionalities specific to an entity to which the aircraft belongs; and
an exchange interface connected between the core module and the supplementary module configured to exchange messages between the core module and the supplementary module,
wherein the core module comprises a core interface, which is different from the exchange interface, that interfaces with an on-board system of the aircraft, the on-board system comprising a first man machine interface,
wherein the supplementary module comprises a supplementary interface, which is different from the exchange interface, that interfaces with a second man-machine interface,
wherein the core module is implemented in a core partition and the supplementary module is implemented in a supplementary partition, the core partition and the supplementary partition being separate partitions of a computing system onboard the aircraft,
wherein the core partition and the supplementary partitions are at least one of:
(A) temporally segregated wherein activities of one of the core partition or the supplementary partition do not affect timings of activities of the other partition of the core partition and the supplementary partition, and
(b) spatially segregated wherein one of the core partition and the supplementary partition is prevented from accessing a memory space of the other partition of the core partition and the supplementary partition.

12. The flight management system as claimed in claim 11 , wherein the one or more supplementary functionalities are specific to a specific aircraft model, a family of aircraft, a company, an alliance and/or all or part of a fleet of aircraft.

13. The flight management system as claimed in claim 11 , wherein the supplementary interface is configured to enable the supplementary module to access the on board systems of the aircraft, either directly or indirectly via the core interface.

14. The flight management system as claimed in claim 11 , wherein each of the at least on core functionalities is implem

Assignees

• Airbus Operations Sas

Inventors

• Mere Jean-Claude
• Neri Pierre
• Bernat Julien
• Vie Marc

Classifications

• G05D1/101 Primary

  specially adapted for aircraft · CPC title

• H04L67/12

  specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks · CPC title

• G05D1/00 Primary

  Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots (drive control systems specially adapted for autonomous road vehicles B60W60/00) · CPC title

• G08G5/003

  Physics · mapped topic

• H04L43/0823

  Errors, e.g. transmission errors · CPC title