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Next Generation of Avionics Laboratory Development Platforms Embedded Tech Trend - January 2016 Wayne McGee – [email protected]

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Page 1: Next Generation of Avionics Laboratory Development Platforms - … · 2017-03-30 · Next Generation of Avionics Laboratory Development Platforms. Embedded Tech Trend - January 2016

Next Generation of Avionics Laboratory Development Platforms

Embedded Tech Trend - January 2016Wayne McGee – [email protected]

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Traditional Method for System Development

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(A) Lab System

(B) Pre-flight System

(C) Production System

Integration Validation

Integration Validation

Integration Validation

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Goal

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Reduce program NRE$

Increase TRL1 2 3 4 5 6 7 8 9

Decrease Risk

Enable technology

Speed up programdevelopment cycle

CompletionStart

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Traditional Lab Difficulties

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Cost

Time

Complexity

Risk of errors

Cabling

Test platform not representative of the final solution

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“”

Provide a laboratory systemthat employs the same set ofShop Replaceable Units (SRUs)that will be used in a deployedsystem

Conceptual Approach (Top Down)

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Cover most common avionics requirements.

Base the design on an open architecture via VITA standards.

Address consideration for Safety and Design Assurance Level (DO-254, DO-178C)

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Recipe and Key Elements

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CPU A

IO rich 3U VPX board modules

Upgradable SBC mezzanine

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Recipe and Key Elements

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Full mesh interconnect for multi processor applications

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Recipe and Key Elements

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Commercial connectors allowing the use of standard cables

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Recipe and Key Elements

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Open to customizationand adaptation

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Recipe and Key Elements

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Early Profiling and Concept Validation

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Benchmark application performance in near-realistic environment

Platform architecture validation

Integrate SW application and API drivers

Validate BIT coverage

“”

Allow equipment manufacturer to accurately specify application requirements

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Works Right Out of the Box

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Ready to use. Is supported by pre integrated SW modules BSP Drivers Middleware Tools

Support for ecosystem/partner SW and middleware

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Address Ground Based Installation

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Rackable solution

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Future Needs & Trends

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Growth provision (slots, interfaces, HW performance)

Address open architecture and interoperability

Address new coming technology , processors and interfaces

Reliability, Availability, Maintainability and Testability (RAMT) and in particular Built in test

SWaP optimization

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Conclusion

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Typically saves 6 to 12 month of program schedule

Early platform architecture validation

Reduces program risks and cost

Deployable as a ground based fixed installation

“”

A new type of laboratory platformsbecomes a key element for the successof C4ISR avionic programs !

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Creative Electronic SystemsWayne McGeeVP Sales, General ManagerNorth America(919) [email protected]

Thank You

www.CES-SWaP.comMore info:

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