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management system for aircraft

A management system and aircraft technology, applied in traffic control systems, control/regulation systems, instruments, etc., can solve the problems of high cost of time scale and difficulty in expanding the flight management system, and achieve the effect of short time period and improved flexibility

Active Publication Date: 2018-03-30
AIRBUS OPERATIONS (SAS)
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] However, the ever-increasing functional requirements for guiding flights have led to a significant development of the flight management system, which has become, over time and with new procedures, a system that is difficult to scale up
Thus, many functional areas are already linked to the system (navigation, guidance, decision support...), involving complexities such that any modification, even relatively minor ones, today requires the use of Extensive effort on implementation and verification, which results in timescale and considerable cost for implementation

Method used

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Embodiment Construction

[0061] exist figure 1 , the management system 1 comprises a flight path management function 2 comprising means for routinely Integrated means for determining at least one flight path of an aircraft. The flight path management function 2 also has the purpose of defining a flight plan to be followed by the aircraft on the basis of received data and different parameters. The system 1 also includes the following other main functions:

[0062] - navigation functions that allow the calculation of the position of the aircraft3;

[0063] - Function 5 for calculating the deviation between the position of the aircraft and the flight path to follow. The position of the aircraft is received by the navigation function 3 and compared with the position in accordance with the flight plan provided by the flight path management function 2 in order to provide the guidance function 4 with flight path corrections to be applied to the aircraft;

[0064] - at least one navigation database manage...

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Abstract

The invention relates to a management system for aircraft. The system (1) comprises at least the following main functions: a flight path management function (2), a navigation function (3) allowing calculation of the position of the aircraft, a function for calculating deviations between the position of the aircraft and the flight route to be followed functions (5), management functions (6) of at least one navigation database, management functions (7) of aircraft performance calculations and functions (8) of management interfaces and displays, each of said main functions being assigned to specific equipment of the aircraft , the flightline management function (2) is linked to each of the other main functions.

Description

technical field [0001] The present invention relates to a management system for aircraft, in particular for transport aircraft, which has an optimized scalable architecture and which is able to manage the aircraft not only during flight but also during phases on the ground, especially at airports . Background technique [0002] It is well known that transport aircraft are managed by electronic systems whose arrangement and interaction follow complex architectures. This is especially true in the case of flight management systems (FMS) equipped with flight management functions. This incorporates a considerable number of functions, such as flight planning, calculation of the flight path to be followed by the aircraft and also calculation of deviations from this flight path in order to correct the position of the aircraft. It thus offers the crew the possibility to define a route to be followed before the flight, and then maintain or even scale up this route during the flight ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G08G5/00
CPCG05D1/0083G08G5/0021G08G5/0034G08G5/0052G08G5/065B64C19/00G05D1/00
Inventor J-C.梅雷G.泰瑟姆
Owner AIRBUS OPERATIONS (SAS)
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