vionics arge scale d - ASHLEY Project€¦ · A664 Modular Avionics A664. 7 ... Integrated...

Avionics Systems Hosted on a distributed modular electronics Large scale dEmonstrator for multiple tYpe of aircraft

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Presented by

Prepared by

This document is produced under the Grant Agreement 605442. It is the property of the ASHLEY consortium and shall not be distributed or reproduced without the formal approval of the ASHLEY Steering Committee.

“Unrestricted PUBLIC Access”

AERODAYS 2015

October 20th, 2015London, United Kingdom

Thierry MARET (THALES Avionics)

Thierry MARET (THALES Avionics)

ASHLEY at a glance

ASHLEY-WP73-THA-DISM-PRES-0462 Issue 1

Preface

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This document is produced under the Grant Agreement 605442. It is the property of the ASHLEY consortium and shall not be distributed or reproduced without the formal approval of the ASHLEY Steering Committee.


This publication only reflects the view of the ASHLEY Consortium or selectedparticipants thereof. Whilst the ASHLEY Consortium has taken steps toensure that this information is accurate, it may be out of date or incomplete,therefore, neither the ASHLEY Consortium participants nor the EuropeanCommunity are liable for any use that may be made of the informationcontained herein.

This document is published in the interest of the exchange of information andit may be copied in whole or in part providing that this disclaimer is included inevery reproduction or part thereof as some of the technologies and conceptspredicted in this document may be subject to protection by patent, designright or other application for protection, and all the rights of the owners arereserved.

The information contained in this document may not be modified or used forany commercial purpose without prior written permission of the owners andany request for such additional permissions should be addressed to theASHLEY co-ordinator (Thales Avionics S.A., 105 Av. du General Eisenhower,BP 63647, 31036 Toulouse, FRANCE, for the attention of the ASHLEY ProjectManager) in the first instance.

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This document is produced under the grant agreement no ACP2-GA-2013-605442. It is the property of the ASHLEY consortium and shall not be distributed or reproduced without the formal approval of the ASHLEY Steering Committee.


ASHLEY Project Information

Name of the project:

Avionics Systems Hosted on a distributed modular electronics Large scale dEmonstrator for multiple tYpe of aircraftAcronym: ASHLEY

Starting Date : October 1st, 2013Ending Date : March 31st, 2017

Duration : 42 months

Total Cost : 39,8 M€

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From the Federated Architecture Concept to the IMA1G concept

F3

LRUProprietary

Solution

Relies on Line Replaceable Unit (LRU) Solution� The system designer is the module and function supplier� One single system per LRU

F2

LRUProprietary

Solution

F1

LRUProprietary

Solution

F3F2F1

CPU

IO

OS

FederatedArchitecture

Concept

Integrated Modular Concept

(IMA1G)

FunctionSuppliers

Module Supplier

From the FederatedArchitecture

to the IMA1G concept

Relies on Line Replaceable Module (LRM) Solution� Clear separation between LRM suppliers and system designers� LRM resources are shared between LRM hosted Functions

A664switch

One

sys

tem

des

igne

r

Man

y sy

stem

des

igne

rs

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Innovation beyond IMA 1G

From IMA 1G…

... to IMA 2G

Distributed Modular AvionicsA664

A664

7




A664

Separate I/O from

computing modules

RPC

RDC

REU

Toolset Toolset Toolset

F1 F3F2 F4F5 F6

Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS

switchswitch switch switch switch switch

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Increased computing

module performance

A664

Toolset Toolset Toolset

F1 F12F2 F14F15F13

Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS

F2F4

F6 F8 F9F11

RPC

RDC

REU

Spare


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Middleware providing

platform level services

A664

Toolset Toolset Toolset Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS

Platform level services

F1 F12F2 F14F15F13F4F6 F8 F9F11

RPC

RDC

REU

Spare

switchswitch switch switch switch switch(e.g. DB service)

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Reconfiguration mechanisms

A664

Toolset Toolset Toolset Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS


F1F12

F2 F14F15F13F4F6 F9

F11F8

RPC

RDC

REU


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Integrated processes and

toolset

A664

CPM

OS

CPM

OS

CPM

OS

CPM

OS


F1 F12F2 F14F15F13F4F6 F8 F9F11

Integrated Platform Toolset

RPC

RDC

REU

Spare


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SCALABILITY =

Capability of the architecture to be adapted to…

IMA 1G

DME

Single A/C

Family of A/C

Set of Families (Regional / Large+small

transport, bizjet)

Needs of various A/C

types

- weight / volume- power consumption- environmental conditions

(thermal, vibration, etc)- Specific functions- Specific Input / Outputs

requirements

- high performance applications- time critical applications- avionics server functions

Large number and many types of applications

10 20 30 40 50

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Application of IMA in aircraft

ASHLEY makes the step from single building blocks towards the integrative IMA platform solution

Key challenges are:- Industrialization- Modularization- Integration - Services- Certification

Innovative Solutions for Future Programs

ASHLEY is on the path of future IMA2G-based aircraft programs

A350

IMA1.5G

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Core Resources

IMA 2G studies: Overview

NELA

SYSTAVIOASHLEY

PRIMAE

IDEE5

GEODESIE

A350

ATR B787

SSJA400M

IMA 1G

SCARLETT

Configuration Process

NetworkResources

RemoteResources

Support and training

Platform Services

Applicative middleware

Tools and Framework

Installationand packaging

IMA 2G

Platform or Function

Architecture

A380

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ASHLEY Objectives

ASHLEY has the main objectiveof consolidating and extendingthe efforts of several independentprojects by improving the currentIMA2G Distributed PlatformSolution.

* DME Distributed Modular Electronics

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Contacts

Thierry MARETThales AvionicsProject [email protected]

WEBSITE

www.ashleyproject.eu

Margarida PINTOISQDissemination [email protected]

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Avionics Systems Hosted on

a distributed modular electronics Large scale dEmonstrator

for multiple tYpe of aircraft

This document is the property of the ASHLEY consortium and shall not be distributed or reproduced without the formal approval of the ASHLEY Steering Committee.

Call identifier: FP7-AAT-2013-RTD-1

This project has received funding from the European Union’s Seventh Framework Programme for research, technological development and demonstration under g rant agreement no ACP2-GA-2013-605442.


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