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Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

SCARLETT From the Integrated Modular Avionics the First Generation architecture to the Distributed Modular Electronics solution. Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009. Collaborative Project - Consortium. SCARLETT: Large-scale integrating project

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Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

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  1. SCARLETTFrom the Integrated Modular Avionics the First Generation architecture to the Distributed Modular Electronics solution Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  2. Collaborative Project - Consortium SCARLETT:Large-scale integrating project 38 Partners 16 countries Budget: 40 mln EUR Leader: THALES France Large Industrial Companies: Airbus, SAGEM, GEA,... Public Research centers: ONERA, NAL, ... Industrial Research centers SMEs Universities: Bremen, Bristol, Hamburg, Nottingham, Rzeszów Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  3. Collaborative Project - Schedule Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  4. Distributed Modular Electronics • Next generation IMA platform will need to provide more computing power and interface capability • Volume / weight / power consumption constraints will remain Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  5. Additional market expectation • Increase operational reliability Toolset Toolset Toolset Toolset F1 F6 F4 F5 F2 F3 OS OS OS OS C C C C I I Reduce cost of avionics parts I I P P P P Non - O O O O M M AFDX M M switch switch switch switch AFDX Reduce Set of Part Numbers Save weight, volume, power consumption Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  6. Additional market expectation Reduce development cycle Scalability to various aircraft types • Increase operational reliability Toolset Toolset Toolset Toolset F1 F6 F4 F5 F2 F3 IMA-2G OS OS OS OS C C C C I I Reduce cost of avionics parts I I P P P P Non - O O O O M M AFDX M M Avoid unscheduled maintenance switch switch switch switch AFDX Reduce Set of Part Numbers Save weight, volume, power consumption Industry-wide step changes are required Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  7. SCARLETT Approach Reduce development cycle Scalability to various aircraft types • Increase operational reliability SCARLETT IMPLEMENTATION OF IMA2G : Distributed Modular Electronics • 1 – Provide a scalable solution • 2 – Define minimal set of modules • 3 – Increase number of supported function • 4 – Develop new standards to support 2nd generation IMA Reduce cost of avionics parts • 5 – Provide enhanced process and toolset Avoid unscheduled maintenance • 6 – Demonstrate fault tolerance -- and reconfiguration Reduce Set of Part Numbers Save weight, volume, power consumption Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  8. IMA 2G will provide the system designer with more options for integration in terms of computing power and communication IMA 2G increases the integration level in terms of Criticality level of hosted systems Number of hosted systems in IMA System integration level General: Changes from IMA 1G to 2G Aircraft Designerand Systems Integrator Avionics Designer Work Load IMA 1G System Design System Design Platform Design System Design Work Load IMA 2G Platform Design • IMA 2G means an increased complexity in terms of technology and processes • IMA 2G objective is to optimize tool usage and their processes System Design System Design System Design Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  9. SP3. Platform integration • Definitions • Common Resources – An IMA Component which can be configured to perform a variety of functions • AFDX – Avionic Full Duplex Switched Ethernet • IMA Perimeter – The list of systems hosted by IMA Components • Only a few different hardware modules: • CPM – Core Processing Module • RPC – Remote Power Centre • REU – Remote Electronics Unit • RDC – Remote Data Concentrator • IRDC Intelligent RDC • IOM – Input Output Module • Smart Device (Sensor or Actuator) Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  10. SCARLETT Schedule Step 1 Step 2 Step 3 ANALYSIS & DEFINITIONS Aircraft / System Requirements DME Platform Concepts DME Architecture DME Specifications DME Platform Demonstrators EVALUATORS DEVELOPMENT DME Platform Elements As Mock-ups Tools Set Integration Generic Platform CAPABILITIES DEMONSTRATIONS & ASSESSMENT DME Platform System/ Services Demonstrators DME Platform Operational Demonstrators Results/Assessment Definitions Mock-ups Demonstrators Definition T0+36 T0+6 T0+24 T0 Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  11. SP3. Platform integration Outputs • Generic Platform • verified • CPMs, Network and Remote Electronics • integrated • verified • Test Applications for Demonstrators • verified Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  12. SP3. Platform integration WP3 Partners Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  13. SP3. Platform integration M9 M12 M15 M24 M18 M21 M27 M30 M33 M36 SP3 WP3.1 To November 2010 From April 2009 WP3.2 WP3.3 4 Decision Gate 4 Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  14. WP3.3. Application Development • WP3.3. Application Development for Demonstration (Leader: General Electric Aviation, UK) • T1. High Performances Data Distribution demonstration • T2. I/O intensive demonstration • T3. Time Critical demonstration • Braking Control Application • Fire/Smoke Detection Control Function • Elevator Control Application (RUT) • T4. Reconfiguration and Maintenance demonstration Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  15. Elevator Control Application Indirect (Fly-by-Wire) Flight Control System Rate Command / Attitude Hold Control Designers’ tasks: • Structure of pitch control system • Control law calculation • Properties of actuators and actuators’ controllers • Synchronization of actuators’ load moments Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  16. Elevator Control Application AFDX Network Only AFDX & Fieldbus AFDX + IRDC Fast Loop Fast Loop Fast Loop Fast Loop Slow Loop Slow Loop Slow Loop Slow Loop Slow Loop Slow Loop CPM OS CPM OS CPM OS CPM OS CPM OS CPM OS ADFX SW ADFX SW Fieldbus) ADFX SW RDC RDC RDC RDC Fast Loop Fast Loop IRDC OS IRDC OS Sensor & Actuator Simulations Sensor & Actuator Simulations Sensor & Actuator Simulations Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  17. Elevator Control Application • Time Critical Systems • Guaranteed (maximum) Response time • Systems who have to perform a defined function within a time period • Maximum response time t < tMAX • Within a defined time period tMIN < t < tMAX • Only periodic functions so far • Avionics must support: • Short periods / high rate • Must provide low latencies • Must provide deterministic behaviour • Real Time Operating System - Time Critical Requiments • VxWorks – Wind River • PikeOS – SysGo • ARINC 653 - Avionics application softwarestandard interface Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  18. Elevator Control Application Structure of the elevator control application Flight Computer Modules 0 – (HC) Handling Control Module 1 – (PS) Pitch Stabilization Module 2 – (AS) Actuators Synchronization Module 3 – (AC1) Actuator Controller No 1 4 – (AC2) Actuator Controller No 2 Modules for simulation and testing 5 – (AR)Actuators and Elevator Dynamics Model 6 – (DA) Model of Aircraft Longitudinal Dynamics 7 – (PT) Model of Pilot's Steering Signal Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  19. Schedule & Progress of WP3.3Elevator Control Application / RUT Not Yet Carried out Waiting for validation Unvalid task Validated task Implemented Process TODAY To be delivered to Wp4.3 RequirementsSpecification Application Build Testing 4 5 3 1 Preliminary Design & Interface Specification Application Design Prototype Delivery for Initial Integration 2 6 Final Delivery To WP4.3 7 09/09 INIT 11/09 02/10 05/10 10/10 08/10 09/10 1 2 3 4 5 6 7 mm/yy mm/yy mm/yy mm/yy mm/yy mm/yy mm/yy Re-Assessed Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  20. The future of SCARLETTSCARLETT and Way Forward FUTURE PROGRAMMES SUKHOI SJ AIRBUS A400M IMA2G AIRBUS A380 NEVADA SCARLETT IMA1G VICTORIA Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

  21. The future of SCARLETTSCARLETT and Way Forward FUTURE PROGRAMMES SUKHOI SJ AIRBUS A400M IMA2G AIRBUS A380 NEVADA SCARLETT IMA1G VICTORIA Thank you for your attention Cooperation fields for Aeronautical Research and Technology – Rzeszów, 14.12.2009

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