Airbus FANS B project presentation

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AERONAUTICAL COMMUNICATIONS PANEL (ACP)
WORKING GROUP N (NETWORKING) – 4TH MEETING
New Orleans (U.S.A.), 10th – 19th November 2004
Airbus FANS B project presentation
Presented by Stéphane Tamalet
(Airbus – ICCAIA Panel member)
Summary
On June 2004, Airbus has decided to launch the development of the FANS-B project for the Aircraft of
the “Single Aisle” family (A318/A319/A320/A321). The FANS B project aims at offering the option for
installation of a certified and integrated implementation of ATC datalink functions based on the ICAO
standards (ATN) and complying with performance required in dense continental areas. The availability of
the first generation of the FANS B systems is scheduled for 4Q2006 for installation on aircraft of pioneer
Airlines participating to the Link 2000+ program.
This Information Paper gives an overall presentation of the FANS B project, providing details on the
development roadmap and on the system characteristics.
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1. Introduction
On June 2004, Airbus has decided to launch the development of the FANS-B project for the Aircraft of
the “Single Aisle” family (A318/A319/A320/A321). The FANS B project aims at offering the option for
installation of a certified and integrated implementation of ATC datalink functions based on the ICAO
standards (ATN) and complying with performance required in dense continental areas. The availability of
the first generation of the FANS B systems is scheduled for 4Q2006 for installation on aircraft of pioneer
Airlines participating to the Link 2000+ program.
This Information Paper gives an overall presentation of the FANS B project, providing details on the
development roadmap and on the system characteristics.
2. The FANS project
The Future Air Navigation System (FANS) concept consists in upgrading Communication, Navigation
and Surveillance (CNS) systems in order to allow introduction of efficient Air Traffic Management.
As depicted on Figure 1 below, the FANS B project corresponds to the 3rd development step in the Airbus
framework for implementation of CNS/ATM services.
FANS product development
•
Consistent with
•Air Traffic Alliance Roadmap
•ICAO ATMCP concept
“CNS/ATM"
FANS B
Pre-FANS
Airline Datalink
C: AOC over
ACARS
S: Transponder
N: Classical means
ATM: Conventional
Air Traffic Control
procedures
FANS A/FANS A+
Oceanic/Remote
airspace/Accommodation
C & S: ATC & AOC
datalink over ACARS
N: GPS-based
ATM: ATC processes
enhancement with initial
A/G automation
North America,
Europe
High Density airspace
ASAS Package 1
C: ATC over ATN
S: Elementary &
Enhanced Surveillance
N: RNP, MLS, GLS
ATM: First Applications
of A/G automation to
ATC/ATM
4D Trajectory
Management
Automated support to
Air Traffic
Management
Figure 1: The FANS project
The “pre-FANS” phase of the FANS project aimed at the upgrade of the aircraft architecture in order to
offer flexibility for installation of AOC applications and provision for hosting ATC applications.
The “FANS A” phase consisted in the upgrade of the preFANS installations with ACARS-based FANS A
(CPDLC & ADS) applications for oceanic/remote area (low/medium density airspace), in conjunction
with GPS based navigation.
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The “FANS B” phase corresponds to the upgrade of the Pre-FANS installations with ATN-based ICAO
SARPs compliant ATC services for high density airspace in continental areas, in conjunction with Low
RNP capabilities for approach navigation and Elementary & Enhanced (ADS-B out) capabilities for
surveillance.
The “CNS/ATM” phase is the target , compliant with the ATMCP Operational Concept Document
(OCD); it is intended to provide 4D Trajectory Management (through datalink and navigation
capabilities) with initial ASAS package 1 applications (through ADS-B capabilities).
The FANS project development is governed by the Airbus FANS policy, which can presently be
summarized as follows:

to promote the use of FANS B on the A/C which primarily operate in the high density congested
airspace : i.e. the Single Aisle family.

to cover oceanic/long range/remote (low/medium density) operations with FANS A on the A/C
flying in these areas (A330/A340/A380 and long range A319/320/321)

to promote/collaborate with ATS Organisations such that
o
no operational limitation will be applied in high density airspace for non CNS/ATM
package 1 A/C, either through voice control or through data link accommodation for this
airspace.
o
Global convergence to a performance based approach (RCP), which should allow
operation of CNS/ATM package 1 A/C, as non CNS/ATM package 1 A/C, all around the
world (no technology specific areas).
On the basis of this policy,
-
FANS A was initially developed on “Long Range” Aircraft (Airbus A330/340 family) and is in
the final stage of its development (certification by end 2004) for the Airbus A319/320/321 family.
-
The development of FANS B has been launched for the Airbus A318/319/320/321 family.
The Figure 2 summarizes the current status of the implementation of FANS on Airbus Aircraft.
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FANS Airbus offer
PreFANS
FANS A
SA
LR
Basic since 1999
N/A
Target : 1Q2005
(under development)
FANS B
(CPDLC/ATN
subset)
Basic since 2000
Target 2S2006
Long term
(under development)
solution
The differences between the FANS1/A standard and the ICAO CNS/ATM package 1 standard are such
that on board cohabitation of both applications is not acceptable neither in term of technical development
nor in term of operations and training. The Airbus FANS policy is to offer a single capability on a given
A/C, exclusive installation of CNS/ATM-1 (FANS B) applications or of FANS A applications.
However, an A/C equipped with ATN router for its ATC applications will also continue to provide an
ACARS router capability to allow continuous AOC operations including in the areas where ATN ground
network will not be operative.
3. FANS B development Roadmap
3.1. General
The FANS B will be developed along a three steps incremental approach :
-
FANS B Step 1 corresponds to the use of ATC data link as supplemental/alternate mean of
communication in upper airspace for R/T reduction.
-
FANS B Step 2 corresponds to the use of ATC data link as primary means of communication in
upper airspace for better traffic flow management.
-
FANS B Step 3 corresponds to the use of data link as primary means of communication in upper
and lower airspace (excluding TMA and airports) for cooperative ATM.
3.2. FANS B step 1
FANS B step 1 consists in the development of functions compatible with ATN Baseline 1 including
initial 4 D Services while ACARS AOC capability is maintained all flight along.
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Expected benefits consist in :
-
Reduction of frequency congestion (use of datalink for routing communications)
-
Optimization of ATC services (direct access to controller in regard to current situations of vocal
saturation, clarification of pilot request)
-
Improvement of the workload sharing between tactic & radarist controller (use of datalink for
routing and tactical communications)
The FANS B step 1 development will be divided in two successive builds: step 1A and step 1B:
3.2.1.
FANS B step 1A so called “CPDLC / ATN Upgrade ”
With FANS B Step1A, Airbus develops a product compliant with initial continental ATC data link
implementation (Link 2000+, FAA CPDLC Build 1A (TBC)). FANS B step 1 A has been proposed as
option for initial operation in Europe ( Maastricht, Karlsruhe, Reims, Madrid, ...) and over Miami to a
limited number of airlines.
The FANS B Step1A objectives are to:
-
Upgrade data link router with ATN stack and AVLC (ACARS VHF Link controlled)
enhancement,
-
Introduce ATC data link applications with the Link 2000+ CPDLC message set extended with the
additional messages from the FAA CPDLC Build 1A program,
-
Propose In Service Evaluation to a limited number of airlines. (participation to Eurocontrol Link
2000+ pioneer program)
This package include:
-
VDL Mode 2 ATN function for ATC use.
-
Capability for ACARS AOC applications sharing the VDL Mode 2 link (using ACARS over
AVLC (AOA) protocol) with ATC ATN-based applications
-
Capability of High-speed data loading (A615A compatibility)
-
Capability for HFDL and Satcom for AOC communication over ACARS.
The development will be done with a design assurance level D (DO178B).
The development is started, with the objective of certification by mid-2006, and installation on A/C of
pioneer airlines by end 2006
3.2.2.
FANS B step 1 B
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FANS B Step 1 B is the final phase covering all FANS B step 1 objectives. This product is the offer in
response to the Eurocontrol Link 2000+ mandate for ATC data link.
It is characterized by:
-
Design Assurance level C for ATSU development.
-
Full CPDLC compliant with ATN baseline 1 standard (ED110 A)
-
Option for automation function (frequency auto-loading on RMP (ACM related ), FMS
integration (ATC Flight Plan Integration),...)
-
Data link recording.
Note: Development of ADS at this stage will be considered. Development of DCL/ATIS services will also
be considered (could be ATN or ARINC623 based)
FANS B Step 1 B should be launched within 2 years after step 1A certification.
3.3. FANS B step 2
FANS B step 2, which should be developed later, should offer first functionalities of 4D Trajectory.
Aircraft impacts will be more important : ATSU and FMS new software should be released at a
minimum.
3.4. FANS B step 3
FANS B step 3 objectives is to provide the level of functionalities required by the ATMCP OCD.
4. FANS B System Overview
4.1. Overview of the architecture
The next Figure, illustrates the implementation of the FANS B architecture onboard Airbus Aircraft (FANS
architecture).
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Flight Management Système :
• Data provider for CPDLC and ADS functions
• Processes some CPDLC msg (e.g.deferred
clearances)
• Allows coordination and exchange of F-PLN
between ATC, AOC and the aircraft
• New flight planning functions“UNDO”, “What if ”
Air trafic services Unit :
•Manage the ATS data link applications
•Manages the HMI, displays and warnings
• Automatically selects the best available medium
• Sustains the communications tasks
Navigation Sensors
Communication Devices
AMU
ADIRS
VOR
DME
ATSU
FMS
Satcom
AOC/ATC*
Datalink
Crew Interfaces
EFIS
ECAM
MCDU
ADIRS : Air Data Inertial Reference System
VOR / DME: VHF Omni-directional Range
/ Distance Measuring Equipment
ADF : Automatic Direction Finder
GPS : Global Positioning System
DCDU*
(ATC displays)
Data communication
Multi Mode Receiver
Navigation
GPS
ILS/GPS
/DGPS/(MLS)
VDR
including ACARS function
ADF
MMR
Audio
HFDR
ModeS
AMU :Audio Management Unit
VDR: VHF Data Radio
Satcom : Satellite Communications
HFDRr :High Frequency Data Radio
Mode S :Mode Select
Printer
Dedicated Control Display Unit:
EFIS / ECAM : Electronic Flight Instrument System / Electronic
Centralized Aircraft Monitoring
MCDU: Multipurpose Control and Display Unit
Printer :
• Core interface for ATC messages
• Provides for a minimum change to existing
procedures
This architecture is based on the Air Traffic Services Unit (ATSU).
The ATSU provides access to all data communications services and hosts the ATN protocols stack and
ACARS Routers, the VDL Mode 2 protocols and the CPDLC functions. The ATN protocols stack
operates over VDL Mode 2 only. The ACARS router operates over the VDL Mode 2 (through the
ACARS over AVLC layer) and Satcom and HFDL.
Access to the AMSS sub network is provided by a separate Satellite Data Unit. One of the onboard
VDRs is used for VDL Mode 2.
The FANS B Human-Machine Interface takes benefit from the experience and operational validation
gained with FANS A. It is fully integrated in the cockpit , and is designed along the same philosophy as
the one that has governed the design of FANS A service HMI (full time availability, readability for both
crew in primary field of view, continuity of the visual scan, appropriate co-ordination DCDU/MCDU for
flight planning management functions) with the aim to minimize the changes to existing procedures..
This crew interface is based on a Dedicated Control Display Unit (DCDU), which allows for the CPDLC
messages management. An overview of this interface is given in the next figure.
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4.2. Overview of the FANS B applications
FANS B corresponds to a set of Controller/pilot messages (CPDLC : Controller Pilot Data Link
Communication), compliant with EUROCAE ED-110A/RTCA DO-258A interoperability standard. The
following applications will be built onto this messages set:
-
Data Link Initiation Capability (DLIC)
-
ATC Communication Management (ACM)
-
ATC Clearances (ACL)
-
ATC Microphone Check (AMC)
The Airbus standard 623 applications are not part of the FANS B definitions. However the system will be
capable of hosting existing AOC suppliers software.
4.3. Overview of the ATN communication stack
The ATN communication stack will be compliant with the ICAO DOC 9705 Edition 2 (including a
number of the associated PDRs).
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5. Recommendation
The Working Group is invited to note the information presented in this paper.
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