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AIRBUS Use Case Flight Control Remote Module Presented by Pierre MOREAU Hardware Methodology & Certification Electronics Avionics & Simulation Products Department David GUIHAL Hardware Methodology On behalf of Alyotech Workshop Grenoble Minatec October 14-15 2010

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AIRBUS Use Case Flight Control Remote Module

Presented by

Pierre MOREAU Hardware Methodology & Certification Electronics Avionics & Simulation Products Department

David GUIHAL Hardware Methodology On behalf of Alyotech

Workshop Grenoble Minatec

October 14-15 2010

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket Page 2

Plan

1) Introduction

- Engineering Theme Stakes

- Equipment Development : State of the Art and Target (Model Based)

- Main Research Axis

2) Socket Airbus Use Case

- Environment

- Architecture

- Roadmap

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket Page 3

Plan

1) Introduction

- Engineering Theme Stakes

- Equipment Development : State of the Art and Target (Model Based)

- Main Research Axis

2) Socket Airbus Use Case

- Environment

- Architecture

- Roadmap

Page 4

The R&T Program Portfolio: Domain-level targets for the Future Aircraft

Flight Performance

Business Performance

• Mature @ EIS (Entry Into Service)

• Systems recurring cost –xx%

Systems

Structures

Cabin

Integration

Engine Suppliers’ Targets

Airbus Use Case Workshop Grenoble Minatec Socket October 14-15, 2010

Page 5

Avionics & Simulation Products

Expert for AIRBUS (Engineering, Procurement, A/C Programs) :

Bringing expertise during systems architecture and integration phases

In the fields of Software, Electronics and Power electronics

In the fields of Methods and Tools for System and computer design

From suppliers selection steps to development reviews

For technical and value analysis

For future avionics studies

Business Centre :

Developing and selling products resulting of aircraft programs, in its fields of competence

Airbus Use Case Workshop Grenoble Minatec Socket October 14-15, 2010

Page 6

ASF ASFASF ASF

Avionics & Simulation Products (continued)

Strategic domains : « safety critical » or A/C specific, AIRBUS only :

Electric Flight Control Systems

Warning and Maintenance Systems

Integrated Modular Avionics (cooperation with Thales Avionics)

This expertise is developed and maintained by real achievements in the fields of embedded software and electronics

Airbus Use Case Workshop Grenoble Minatec Socket October 14-15, 2010

Page 7

What is our Definition of a System ?

Aircraft Level

Aircraft Function System Level

Flight control, fuel management, hydraulics, electrical power & distribution…

Equipment Level

Flight control and guidance computer, flight warning computer…

And beyond…

System on Chip Airbus Use Case Workshop Grenoble Minatec Socket October 14-15, 2010

Page 8

Main Research Axis

Multi-formalism Design Process UML2, SYSML, AADL, SystemC, VHDL-AMS

Language transformations

Model based process description

HW Certification issues

Advanced Verification techniques and tools Formal techniques

Automated activities code and test generation, documentation

Design exploration techniques and tools HW-SW CoDesign, Architecture toolbox

Open source alternatives Traceability, editors, code coverage, rules checking

Workflow, Modification and configuration management

Process sub-theme

HW formal proof sub-theme

Infrastructure sub-theme

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket Page 9

Plan

1) Introduction

- Engineering Theme Stakes

- Equipment Development : State of the Art and Target (Model Based)

- Main Research Axes

2) Socket Airbus Use Case

- Environment

- Architecture

- Roadmap

10

Airbus Use Case Description

Environment :

Flight Control Remote Module

Avionics computer is dedicated to process data from sensors and to control actuators according

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket

11

Airbus Use Case Description

Main Functions : Acquisition function of Airborne Sensor Signals

Generation of Signals for Servo-control

Goal : SoC Implementation

Critical Avionics Development

Hardware : DAL A (selon DO-254)

Software : DAL A (selon DO-178)

Acquisition

Sensor

Control

Actuator

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket

12

Architecture

AHB AMBA 2.0 Media Architecture Bus

Embedded Software Control Loop function

ARM Processor Embedded Software Execution

With Local Memories

DMA Data Transfer HW Accelerator

DSP Sub-System Analog data I/O processing

Shared Memories Data & Instruction Storage

DMA Proc.

Ss Syst. DSP

Mem. DATA

Mem. CODE

ANI

ANO

DSI

DSO

MS MS

S S S

AHB

October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket

13

Expected Improvements

Functional Validation

High Level Modelling and Golden Reference

System Verification

Software Design

Shared HW Virtual Platform

Architecture Trade-Off

Model based

HW Design (DMA, DSP Sub-System)

Detailled Design Generation

HW Verification

System Integration Verification

Recurrent Activities

Requirements Traceability, Documents Generation October 14-15, 2010 Airbus Use Case Workshop Grenoble Minatec Socket

Expected Improvements