Februar 2012

Avionic DeveloperPraktikum

Figures

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AerospaceMaritime SystemsAutomotiveEnergy

Market Areas

Formation: 2006

Employees: >40

Head Office: Ottobrunn/Munich

Offices: Munich, Berlin

Company

Engineering Services

System & Software Solutions

Embedded Systems

Competencies

AVIONIC DESIGN SERVICE GmbH Haidgraben 2 85521 OttobrunnPhone: +49 (0) 89 673 597 98 – 0

Internet: www.ads-avionics.comEmail: office@ads-avionics.com

AVIONIC DESIGN SERVICE GmbH Division BerlinATRIUM Friedrichstr. 6010117 BerlinPhone: +49 (0) 30 30 329 26 – 0

Email: office-berlin@ads-avionics.com

Costomer Req.

System Req.

SW Req.

SW Design

Coding

Target Test

Modul Test

System/HW Tests

Qualification

Design & StressEngineering

D&S

Project & Process Management

Process AnalysisRequirement Mgt

Configuration & Change Mgt

P & P

I&VInnoVation

System & SW ArchitectureRapid-Prototyping

Pre-Validation

Org Aufbau – Kompetenz-Anordnung

Validation & VerificationSystem/System Integration

System TestingHW & SW Integration

System TestingComponent Tests

V&V

Validation & VerificationSW Integration

Host TestingFormal Qualifiaction Testing

System EngineeringSystem Architecture

System Analysis & DesignReq. Engineering

Simulation

S&S

Software EngineeringSW Analysis & Design

Req. EngineeringCoding & Unit TestingReverse-Engineering

Simulation

Airworthiness & Qualification

Certification and Qualification

Systems & Software

A&Q Airworthiness &

Qualification Certification and

QualificationSystems & Software

A&Q

Avionic Developer

Helmet Mounted Sight & Display (HMSD)

Radio Frequency Indicator (RFI)

Control & Display Unit (CDU)

Multi Function Display (MFD)

Embedded Hardware

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I&V

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Avionic Developer System Architecture

C o re Bus

A / A 5 A rinc 4 2 9 / 4 5 3A u a ud io lineD d iscreteD 1 / 2 D S1 0 1 / 1 0 2R2 / 8 RS4 2 2 / 4 8 5 (hd lc). .. .. . STA N AG 3 3 5 0FG Fill G unC C centra l clea rwo w weight o n wheelRcfg Reco n figura tio n

Legend

Test

Test

M issio nBus

TC S

D AU

D a taReco rd

Vo iceReco rd

VFDRA

DC

, WM

CFC

C, A

CC

Fuel, Electr.

Hydr, E

ng D

eiceE

vent

DA

C C

MTC 1-2

DMG

Mis DTDHMSD CP

FCSCFP, FMCJSS

PM C 1 -2

D TDR8

wo w(Rcfg )

PMS

A R8 R8 D FS

BS

MM

C Cwo w(Rcfg)

Pt, Ps, T(Rcfg )

LS/ D M E

D VS

IRS / G PS 1 -2

RA

A D C 1 -2

FCS

DS

U

HM

SD

PH

MS

D C

WX

RFC

S

D

A

A

A

A

A

N A S

MTC

1-2

MTC

1-2W

XR

1-2

DM

G 1-2

FLIRO

WS

C M C 1 -2

Ba ck U pInstrum

stick

H/C Pltf

FCC 1-2DSU

D KU 1 - 2

BC

R8D

D

W a rningInd ica t

W M C

H/CPltfFCSMiss

D

RF I 1 -2

VD U

R8D

AA

A

CDS

D A A D

M FD1 -4

A A A 5

IRS(D H )A dvPnlPTTEW SO W S

C C

C C C CFG

BSM MC Cwo w

V/ U H F 1

C P fo r 1 + 2V/ U H F 2

D F/ H o m

H F / SSB

VH F FM

AC VM U

A udio U nit (including W TG / D VO functio n)

ext/ int co m- ctr

int co m-ctr

C ryptoV/ U H F 1

V/ U H F 2 C rH F C ryp

IF F M 4

IFF(+ C P)

D

A

Ground

Gunner

Cabin

A uA u

D 1 D 2

D 2

1 1 1

D 1

A u A uA u

D

D

CIS

DA u

DR2A u

M ID S

D 1

I&V

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Avionic Developer

Configuration MgmtQuality AssuranceTraceability

Methods

Tools

Development

Standards & Guidelines

Application Partition

HMI Data

I/O Data

ARINC653 OS

PPC HW

System Partition

(TEIL) SYSTEM TESTSW/SW & SW/HW Integration

Embedded Hardware

TARGET

Avionic Developer

I&V

DKU/CDU MFD RFI

Application Partition

HMI Data

I/O Data

ARINC653 OS

PPC HW

System Partition

Flight Simulator X-Plane

HMSD

Application Partition

HMI Data

I/O Data

ARINC653 OS EM

System Partition

Avionic Developer – Aufbau Komplett

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Embedded H/W

ApplicationSimulation

Consumer PC

HOST

(TEIL) SYSTEM TESTSW/SW & SW/HW Integration

Embedded Hardware

TARGET

CDUexecutable

MFDexecutable

RFIexecutable

HMSDexecutable

Consumer PC

HOSTI&V

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System Architecture & Behavior

Pilot Request

Display update

Compare I/O data for check OK

Behavior and Algorithm to control the Equipments

Data exchange with MFDs• Redundancy Mgt• Reconfiguration• Cold/Warmstart• Maintenance IBIT• Availability

Milbus

On-BoardComputer

Arinc

Operational Software

Response

Control

Equipment

CDU

MFD

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Avionic Praktikum Projekt Entwicklung:• Bearbeitung eines Mini-Projektes entlang des V-

Modells von der Spezifikation über SW Design und Coding bis hin zum Testen und der Qualifikation

Beispiele:• Radio Ansteuerung für die Funktionalität „Fixed

Frequency“• Ansteuerung eines Direction Finders • Navigation „Direct To“; „Course From“• Transponder Code Mode S • …

Avionic Praktikum Projekt - Vorgehen

Avionic Praktikum Projekt - Ablauf

Operational Function

procedure Set_Active_Freq is

Local_Freq: Vuhf_Types.Frequency := 118.000,

beginVuhf_Hld.Get_Dc_Vuhf_Act_Freq (value => Local_Freq, Index_1 => Ofrs.Types.Vuhf_1);

Vuhf_Lld.Put_Cmcc_Vuhf_Act_Freq (value => Local_Freq, Index_1 => Ofrs.Types.Vuhf_1);

end Set_Active_Freq;

Test System

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SIM-Picture