Tools Capability Avionics Software and Hardware

vFull life cycle development (Avionics standards DO-178B, DoD-2167A and DO-254) vSoftware verification services (DO-178B and DoD-2167A) vVerification ...

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Tools Capability

Avionics Software and Hardware Engineering Services

¢ DSP-OS

Life Cycle Tools

¢ VDK v

¢ MicroC/OS

Requirements Management ¢ DOORS ¢ ReMa (Accord)

v Compliers ¢ C/C++/Ada 83 Compilers for

Capabilities

various hardware platforms

v Software Design

(Power PC, TI DSP, ADSP

¢ Mentor Graphics Case Tool

etc.)

¢ Rhapsody ¢ Teamwork/Ada

FPGA Tools

¢ Easy Case v

v

Software Testing

¢ XST, Synplify, SynplifyPro,

¢ RTRT

Precision

¢ IPL Cantata ¢ LDRA ¢ SmartTester for C (Accord) for

v

¢ Logiscope and Lint

v

¢ C-Cover ¢ Logiscope ¢ CodeTrax for C (Accord) v

Project Management ¢ MS-Project ¢ Smartworks Project Planner (Accord)

v CVS v RCS v PVCS

¢ GreenHills Integrity ¢ VxWorks ¢ OASYS-653 (Accord) ¢ MS-WinCE

v

Re-engineering of software and electronic hardware for Obsolescence Management as per DO-178B

Environmental qualification of airborne electronic hardware (DO-160F)

RTCA DO-178B and DO-254 Services

¢ Actel’s Libero 6.0

We plan, design, develop, implement and verify your product according to DO-178B and DO-254 standards using

¢ Altera’s MAXPlusII

refined processes and advanced tools. Our experience with DO-178B and DO-254 ranges from Level A through D, over a wide variety of platforms and domains. We offer services both offshore and on-site based on clients’ needs.

v

Coverage Analysis ¢ TransEDA VN-Cover

Hardware Tools v Spectrum Analyzer

Software Engineering Skills

Embedded Systems Engineering Skills

¢ Programming

¢

Languages:

Ada,

C,

C++,

Design and Engineering of real time embedded systems with FPGAs, ASICs, Microprocessors

ASSEMBLY languages

v Logic Analyzer

and Digital Signal Processors

v Multifunction Counters

ACCORD

¢ Operating Windows,

v Development tools and ICE for all ADI DSPs, TI DSPs, ARM Processor, PowerPC v Orcad, Cadstar Viewer, Alegro,

&

Environments: VAX/VMS,

Real

UNIX, Time

Linux,

Operating

¢

Accord Software & Systems Pvt. Ltd. # 37, K.R. Colony, Domlur Layout, Bangalore - 560 071, INDIA Tel : +91 - 80 2535 0105/0136/0138 Fax : +91 - 80 2535 2723

Humidity

¢ Hardware platforms: ADI DSPs, TI DSPs, ARM,

Accord Software & Systems, Inc. #26 West Lone Cactus Drive, Phoenix, Arizona, USA 85027 Voice : +1.623.271.8800 Fax : +1.623.271.8243

¢

PowerPC

Algorithm

development

for

customized

Software

radios,

Spread

Spectrum

communication Systems, hybrid navigation

Standards ¢

Chamber

Design and Engineering of analog as well as highspeed digital circuits

Systems

URL : www.accord-soft.com Email : [email protected]

v Matlab v Te m p e r a t u r e

v RTOS

Certification activities (DO-178B) such as Low Level Requirements generation and various reviews

excellent track record from the prestigious programs reflects our commitment to quality and schedule.

Simulation

PspiceT Software Engineering Tools

v

development life cycle. Accord can offer quick ramp-up of team to meet your changing program schedules. Our

v Digital Oscilloscopes v ClearCase

Verification of complex hardware involving programmable devices (DO-254)

With more than 800 person years of experience in Avionics domain, Accord can assist you in all phases of

v Signal Generators Configuration Management

v

¢ Xilinx ISE 9.1.03i

v Coverage Analysis

¢ VectorCAST Cover

Back end design

¢ Altera’s MAXPlusII

¢ IPL AdaTEST

Software verification services (DO-178B and DoD-2167A)

v

¢ Actel’s Libero 6.0

(Accord)

v

and DO-254

¢ Xilinx ISE 9.1.03i

assembly

Full life cycle development (Avionics standards DO-178B, DoD-2167A and DO-254)

Sysnthesis,

ispLEVER

¢ VectorCAST C/C++

¢ SmartAct

Front end design

v

ARINC 653, ARINC 615A, ARINC 665, ARINC

systems ¢

¢

MIL 1553B

Engineering

Systems

to

meet

environmental specifications

743, ARINC 429 ¢

Engineering for mass manufacture

stringent

Project Management

Risk Management

With our mature project management processes we

Risk Management process at Accord comprises of:

Typical Project Activities Project Activities

Input

ensure the projects are always completed on schedule within budget and with the highest quality. For project Management we use SmartWorks Project Planner and

¢

Planning for the risk management

¢

Identifying the risks (using a Global Risk Database)

¢

Microsoft Project TM.

Resource Management

Analyzing the risks with Probability Impact Matrix

¢

Prioritizing the risks by quantitative risk analysis

¢

Planning the risk responses

¢ ¢

Project Kickoff

Project Familiarization

Project Planning Data

Project Planning

Accord’s Quality Procedure

complete projects on schedule. Accord has a large pool of talented and trained resources, which can be mobilized for

Customer Project Documents

Change Management

Problem Reporting

Quality Audits

Project Support

Release Activities

Project Monitoring

Customer Feedback / Deviations Process Improvement

¢

AS 9100 Rev B

¢

CMMI Level 5

¢

ISO 9001:2008 & TickIT

Test Planning

Compiler Validation Report, Problem Reports

D

Filled Review Checklists and Problem Reports

D

Requirement, Design and Source Code

D

Test Files, Test Reports, Review Records, Problem Reports

D

Documents Required for Certification

D

Monthly and Weekly Status reports

D

Release Logs

D

Other Agreed Deliverables

D

Status Reporting

Project Metrics Process & Product QA Audit Findings Meeting Minutes, Review Records, Other QA Artefacts

DERs in DO-178B And DO-254.

Quality System

CM Planning

Project Meeting

Metrics Collection

projects at short notice. Our team members have been extensively trained by FAA-

Quality Planning

D

Tool Qualification Artefacts

Planning Phase

Updating the Global Risk Database

Avionics projects often require ramping up of resources to

Project specific Internal Checklists Schedule / GANTT Chart, Risk Register, Resource Allocation Detail

Execution Phase

Statement of Work

Monitoring and controlling the risks

Project Artefact Quality Plan, CM Plan, Unit Test Plan

Project Closure

Product Conformity Report

Legend

Analysis (by EPG)

D

Deliverable On-Site Activity

Partial List of Aerospace Programs Airbus A400m ¢

Full life cycle development according to DO-178B standard (Level A and Level D) for the Data loader software based on ARINC 615A

We can assist you during

Airbus A380 Verification and Validation (DO-178B) :

Planning

Requirements Analysis

v

Plan for software and hardware aspects of certification

v

v

Plan for development, verification, configuration management and quality assurance

v

v

Documents produced ¢ Plan for Software Aspects of Certification (PSAC)

¢

Generate high-level requirements and derived high-

¢

Doors and Slides Management System (Level A)

level requirements

¢

Integrated Modular Avionics (Level A)

Documents produced

¢

Slats and Flaps Control Computer (Level A)

¢ Hardware Requirements Specification (HRS)

¢

Onboard Airport Navigation System (Level D)

¢

Secured Communication interface(Level B)

¢ Software Requirements Specification (SRS)

¢ Plan for Hardware Aspects of Certification (PHAC)

Boeing 787 Dreamliner

¢ Hardware Development Plan (HDP) ¢ Software Verification Plan (SVP)

Implementation

¢ Hardware Verification Plan (HVP)

v

¢

Verification and Validation, Compiler validation, Tool qualification of Wing Ice Protection System in accordance with DO-178B, Level A

¢

Code validation for audio subsystem in accordance with DO-178B Level C

Generate source code and Hardware item

¢ Quality Assurance Plan (QAP) ¢ Configuration Management Plan(CMP)

Verification Design v

Generate Architecture design, low-level requirements and derived low-level requirements

v

Documents produced

Cockpit Display Systems (Level B)

v

Perform reviews of requirement, design and code

v

Perform analysis like control and data flow analysis, stack depth analysis, timing throughput analysis and requirements and structural coverage analysis

v

¢

Design, develop and execute requirements based tests

¢ Software Design Document (SDD)

¢ Unit, Integration and System tests for software

¢ Hardware Design Document (HDD)

¢ Behavioral and place and route tests for PLDs v

NH 90 Helicopter

Documents produced ¢ Requirement based Test Result (RTR)

Integration

¢ Coverage Analysis Report (CAR)

v

Link and load the executable object code into the

¢ Traceability Matrix

target hardware

¢ Requirements based Test Plan (RTP)

Smart Multifunction Display Unit (SMD) verification and validation activities

TEJAS (Light Combat Aircraft) ¢

Implementation and Verification of Flight Control System Software (DoD-2167A)

¢

Requirements Analysis, Design and Verification of Mission Computer (DoD-2167A) Software

¢

Development of Real-time Avionics Line Replaceable Units Simulator, Pilot-machine Interface for Cockpit Evaluator and Multifunction Display Software for Cockpit Evaluator