MAKS Avionics · PDF fileAvionics Systems Hosted on a distributed modular electronics Large scale dEmonstrator for multiple tYpe of aircraft 1 Presented by Prepared by

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

1

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”

MAKS Avionics Conference

August 27th, 2015

Moscow, Russia

Marc GATTI (THALES Avionics)

Thierry MARET (THALES Avionics) / Marc GATTI (THALES Avionics)

IMA2G Issues and challenges

ASHLEY-WP73-THA-DISM-PRES-0428 Issue 1

2

This document is produced under the grant agreement no ACP2-GA-2013-605442.



Thanks to the European Community (EC) and their Framework Programs like H2020 to progress in the mastering of aeronautic technologies becoming more and more complex

Collaborative work is virtuous, and we have a good example within ASHLEY which is managed by the European IMA Domain Leader

We (European Industrial) are completely in line with the ambitious objectives required by ACARE in term of SWaP (Size, Weight, volume and Power Consumption)

To access to a full IM2G we need to mature the requirements to be fulfilled and we need to have access to significant investment on the subject in the next coming years

ASHLEY is one of the European Study than can help to promote real visible progress done on the IMA2G roadmap

General Introduction

Preface

3




This publication only reflects the view of the ASHLEY Consortium or selected

participants thereof. Whilst the ASHLEY Consortium has taken steps to

ensure that this information is accurate, it may be out of date or incomplete,

therefore, neither the ASHLEY Consortium participants nor the European

Community are liable for any use that may be made of the information

contained herein.

This document is published in the interest of the exchange of information and

it may be copied in whole or in part providing that this disclaimer is included in

every reproduction or part thereof as some of the technologies and concepts

predicted in this document may be subject to protection by patent, design

right or other application for protection, and all the rights of the owners are

reserved.

The information contained in this document may not be modified or used for

any commercial purpose without prior written permission of the owners and

any request for such additional permissions should be addressed to the

ASHLEY co-ordinator (Thales Avionics S.A., 105 Av. du General Eisenhower,

BP 63647, 31036 Toulouse, FRANCE, for the attention of the ASHLEY Project

Manager) in the first instance.

4




ASHLEY Project Information

Name of the project:

Avionics Systems Hosted on a distributed modular

electronics Large scale dEmonstrator for multiple tYpe of

aircraft

Acronym: ASHLEY

Starting Date: October 1st, 2013

Ending Date: March 31st, 2017

Duration: 42 months

Total Cost: 39,8 M€

5




ASHLEY consortium: 13 countries

6




ASHLEY consortium : 36 beneficiaries

7




ASHLEY Project Summary

The Integrated Modular Avionics (IMA) concept proposes an integrated

architecture with application software portable across an assembly of

common hardware modules.

ASHLEY will consolidate and integrate the results of SCARLETT and

several national collaborative research projects to achieve

demonstration of the most advanced building blocks available today in a

whole aircraft-level platform.

8




From the Federated Architecture Concept to the IMA1G concept

F3

LRU

Proprietary

Solution

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

One single system per LRU

F2

LRU

Proprietary

Solution

F1

LRU

Proprietary

Solution

F3

F2

F1

C

PU

IO

OS

Federated

Architecture

Concept

Integrated

Modular Concept

(IMA1G)

Function

Suppliers

Module

Supplier

From the Federated

Architecture

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

A664 switch

On

e sy

stem

des

ign

er

Man

y s

yst

em

des

ign

ers

9




IMA1G – An example

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Raw

Sensors

Actuators

Analogue

Discrete

Raw

Sensors

ATAxx

LRU

Analogue

Actuators

Analogue

Raw

Sensors

Analogue

Actuators

Analogue

Raw

Sensors

Analogue

Avionics Bay

ATAvv CPIOM 1

ATAww.bb RDC

A429

IOM

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Arin

c664

Arin

c664

A

rinc664

Arin

c664

Arin

c664

Arin

c664

ATAvv RDC

ATAww.aa RDC

A429

A429

Discrete

A429

ATAww.aa

CPIOM 2

ATAww.bb

ATAww.cc

ATAyy.aa

CPIOM 3

ATAyy.bb

ATAyy.cc

ATAzz.aa

CPIOM 4

ATAzz.bb

Discrete Analogue

Arin

c664

Arin

c664

CAN

10




IMA1,5G – An example

SMART

Sensors

SMART

Actuators

Analogue

Raw

Sensors

Actuators

Analogue

Raw

Sensors

Analogue

Actuators

Analogue

Raw

Sensors

Analogue

Avionics Bay

Field Bus

Common RDC

Discrete

Common RDC

ATAvv CPIOM 1

CPIOM 1

ATAyy.bb

CPIOM 1

ATAxx

ATAyy.cc

ATAww.aa

ATAww.bb

ATAww.cc

ATAyy.aa

ATAzz.aa

Common RDC

ATAzz.bb

Field Bus

REU

Arinc664

Arinc664

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Sw

itch

Arin

c664

Arin

c664

A

rinc664

A

rinc664

Arin

c664

Arin

c664

11




Distributed Architecture

PSB

2 PSB

1 CPM s PS

M - N PS M - E Optiona

l modul es

CPM Spar e

ASM 1 ASM

2

AFDX

LRU

ADCN network

Open World Avionics server

Ethernet network

IFE

R - switch

Arinc664

Actuators with some closed loops

RE U

Optional Field Bus

SMAR T

RE U

TBD

Serial Bus

RLR U

R - switch

Avionics World ATA42 ATA42 / ATAxx shared

RLR U RD

C

RLR U RD

C RLR U

SC I

Arinc664

PSB

2 PSB

1 CPM s PS

M - N PS M - E Optiona

l modul es

CPM Spar e

ASM 1 ASM

2

AFDX

LRU PSB

2 PSB

2 PSB

1 PSB

1 CPMs PSM PSM Optional modules CPM

Spare ASM1 ASM2

AFDX

LRU

Open World Avionics server

Ethernet network

IFE

R - switch R - switch


RE U


RE U RE U REU

CPC CABINET

Optional connection Field Bus

SMAR SMART

RE U RE REU

R - switch Arinc664

- switch - Rswitch

High speed serial Bus, Arinc664.. TBD

Arinc664

Serial Bus

Arinc664 RLR U RLRU

R - switch R - switch

Avionics World ATA42

Avionics World ATA42 ATA42 perimeter

ATAxx module

RLR RLRU RD RDC

Arinc664 Backup connection

RLR U RLR RD

C RDC RLR U RLRU

SC I

Arinc664 Gateway

PSM CPM LP

DCDMs ASM PSM

, , Field bus

discrete

analogue,

ATA24 Loads

Serial Bus

R - switch AFDX

- switch - Rsw itch AFDX serial

Bus..

RDPC CABINET MPDM s

IMA2G – An example

12




Innovation beyond IMA 1G

From IMA 1G…

... to IMA 2G

Distributed

Modular Avionics A664

A664

13





A664

Separate I/O

from

computing

modules

R

P

C

R

D

C

R

E

U

Toolset Toolset Toolset

F1

F3

F2

F4

F5

F6

Toolset

C

P

M

OS

C

P

M

OS

C

P

M

OS

C

P

M

OS

switch switch switch switch switch switch

14





Increased

computing

module

performance

A664

Toolset Toolset Toolset

F1

F12

F2

F14

F15

F13

Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS

F2

F4

F6

F8

F9

F11

R

P

C

R

D

C

R

E

U

Spare


15





Middleware

providing

platform level

services

A664

Toolset Toolset Toolset Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS

Platform level services

F1

F12

F2

F14

F15

F13

F4

F6

F8

F9

F11

R

P

C

R

D

C

R

E

U

Spare

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

16




File Management – file stacks comparisons

CPM

OS

CPM

OS

CPM

OS

CPM

OS

F1F2

R

P

C

R

D

C

R

E

U

switchswitch switch switch switch switch

F3

FS1

CPM

OS

CPM

OS

CPM

OS

CPM

OS

F1F2

R

P

C

R

D

C

R

E

U


F3

FS1

IMA1G - local File stack

one filesystem used locally

• Applications and mass storage colocated on

the same module

OS-centric services

no simple way to access to remote mass

storage

17




File Management – file stacks comparisons

CPM

OS

CPM

OS

CPM

OS

CPM

OS

F1F2

R

P

C

R

D

C

R

E

U


F3

FS1

CPM

OS

CPM

OS

CPM

OS

CPM

OS

F1F2

R

P

C

R

D

C

R

E

U


F3

FS1

IMA1G - local File stack

one filesystem used locally

• Applications and mass storage colocated on

the same module

OS-centric services

no simple way to access to remote mass

storage

CPM

OS

CPM

OS

CPM

OS

CPM

OS

Middleware

F1F2

R

P

C

R

D

C

R

E

U


F3

FS1 FS2 FS3 FS4

CPM

OS

CPM

OS

CPM

OS

CPM

OS

Middleware

F1F2

R

P

C

R

D

C

R

E

U


F3

FS1 FS2 FS3 FS4

IMA2G - distributed File stack

many filesystem used by many functions

•Applications and mass storage hosted on

different modules

new platform-wide middleware services

18





Reconfiguration

mechanisms

A664

Toolset Toolset Toolset Toolset

CPM

OS

CPM

OS

CPM

OS

CPM

OS


F1

F12

F2

F14

F15

F13

F4

F6

F9

F11

F8

R

P

C

R

D

C

R

E

U


19





Integrated

processes and

toolset

A664

CPM

OS

CPM

OS

CPM

OS

CPM

OS


F1

F12

F2

F14

F15

F13

F4

F6

F8

F9

F11

Integrated Platform Toolset

R

P

C

R

D

C

R

E

U

Spare


20





SCALABILITY

=

Capability of the architecture to be adapted to…

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

21





SCALABILITY

=


IMA 1G

Single A/C

Family of A/C

Set of Families


transport, bizjet)

Needs of

various A/C

types

- weight / volume

- power consumption





requirements




Large number

and many types

of applications

10 20 30 40 50

22





SCALABILITY

=


IMA 1G

DME

Single A/C

Family of A/C

Set of Families


transport, bizjet)

Needs of

various A/C

types

- weight / volume

- power consumption





requirements




Large number

and many types

of applications

10 20 30 40 50

23




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

A350

IMA1.5G

24




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

25




Core

Resources

IMA 2G studies: Overview

NELA

SYSTAVIO

ASHLEY

PRIMAE

IDEE5

GEODESIE

A350

ATR B787

SSJ A400M

IMA 1G

SCARLETT

Configuration

Process

Network

Resources

Remote

Resources

Support and

training

Platform

Services

Applicative

middleware

Tools and

Framework

Installation and packaging

IMA 2G

Platform or

Function

Architecture

A380

26




ASHLEY Objectives

ASHLEY has the main objective

of consolidating and extending

the efforts of several independent

projects by improving the current

IMA2G Distributed Platform

Solution.

* DME Distributed Modular Electronics

27




DataBase

Middleware

Terrain Avoidance

Warning

Flight

Warning

Maintenance

Demonstration of Platform solution: DataBase Middleware

Ashley selected functions:

Mission Management

28





Cabin Utilities / High Lift DME

Remote

Solutions

Ventilation

Control

High Lift

Sec. Power

Distribution

Cabin

Demonstration of Platform solution: Remote architecture

29




Photonics &

smart

Sensors

Solutions

DME

Remote

Solutions


Fuel / Landing Gear

Braking Control

system Landing Gear

System Fuel Gauging &

Management

Systems

Validating IMA2G platform solution: Photonics/ Smart & Remote

30




WEBSITE

TWITTER

LINKEDIN

FACEBOOK

www.ashleyproject.eu

http://www.linkedin.com/pub/ashley-project/83/340/6ab

https://twitter.com/ASHLEY_Project

http://www.facebook.com/ashley.Project

ASHLEY Welcome You @

31




Contacts

Marc GATTI Thales Avionics

R&T Director

[email protected]

WEBSITE www.ashleyproject.eu

mailto:[email protected]











32

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 grant agreement no ACP2-GA-2013-605442.


Documents

MAKS Avionics · PDF fileAvionics Systems Hosted on a distributed modular electronics Large scale dEmonstrator for multiple tYpe of aircraft 1 Presented by Prepared by