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Federal Aviation Administration 0 Complex Integrated Avionics and System Safety June 9, 2005 0 Complex Integrated Avionic Systems and System Safety Presentation.

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Presentation on theme: "Federal Aviation Administration 0 Complex Integrated Avionics and System Safety June 9, 2005 0 Complex Integrated Avionic Systems and System Safety Presentation."— Presentation transcript:

1 Federal Aviation Administration 0 Complex Integrated Avionics and System Safety June 9, 2005 0 Complex Integrated Avionic Systems and System Safety Presentation to: Europe/U.S. International Aviation Safety Conference Name: Ali Bahrami Date: June 9, 2005 Federal Aviation Administration

2 Federal Aviation Administration 1 Complex Integrated Avionics and System Safety June 9, 2005 1 Integrated Mod Avionics (IMA) Ex. 777 Trends in Avionics: Integration and Complexity 1980 1990 2000 Electronic flight inst. Ex. 757/767 Integration within closely related functions Most functionality in hardware/firmware Integrated display system Ex. 747-400 Integration of most display- related avionics functions Most functionality re-programmable Integration of many avionics functions Card-based processors in cabinet racks Expanded IMA Ex. Falcon EASy, ERJ-170 Integration of avionics + some flt. control and airplane systems More generic processors & software-based functionality

3 Federal Aviation Administration 2 Complex Integrated Avionics and System Safety June 9, 2005 2 Trends in Avionics: Architectures  Huge increases in: Functional integration. Software size and complexity.  Shift in techniques for isolation/independence: Traditionally, redundant features were completely isolated – now they communicate with each other. High/low criticality functions traditionally physically isolated from each other – now share computing and databus resources.  Mix of new and reused (“legacy”) software.

4 Federal Aviation Administration 3 Complex Integrated Avionics and System Safety June 9, 2005 3 Trends in Avionics: TSO  TSOs: Traditionally, TSOs were used for simple equipment (e.g. seat belts) and well-defined “stand-alone” functions (e.g. air speed indicator). Installation issues were minimal. Now, TSO requirements cover only a small fraction of the designed functionality. TSO functionality may be embedded in an integrated avionics suite (“functional TSO”). Vendors need TSOA to ship “brain-dead” hardware which doesn’t comply with the full TSO requirements until installed and software is loaded.

5 Federal Aviation Administration 4 Complex Integrated Avionics and System Safety June 9, 2005 4 Trends in Avionics: Engineering and Business Practices  Increasing dependence on Commercial Off-the-Shelf (COTS) hardware and software. Examples: Microprocessors (from PC industry). Operating systems (e.g. Windows). Graphic processors (from video game industry).  Changes in manufacturer-vendor relationships and responsibilities.  Global design and manufacturing of highly integrated avionics functions.  Shift from airframe manufacturer as “designer/builder” to “integrator/assembler.”

6 Federal Aviation Administration 5 Complex Integrated Avionics and System Safety June 9, 2005 5 Certification Challenges  Integration and complexity: Current processes (e.g. DO-178B/ED-12B for software) were developed with much simpler architectures in mind. Experience is showing that there are complex and often unexpected “connections” between traditionally unrelated or independent functions, especially during failures. Failures become more difficult to predict and diagnose. It becomes less and less feasible to test all inter-related failure modes. Fully integrated test facilities become more challenging and expensive to build and operate.

7 Federal Aviation Administration 6 Complex Integrated Avionics and System Safety June 9, 2005 6 Certification Challenges  Software: Software-based isolation and independence is much more “fluid” and difficult to assure than relying on hardware. Mixing of COTS, reused, and new software – all developed by different processes and to different standards – makes assessing the safety issues much more difficult, especially in standardized ways.

8 Federal Aviation Administration 7 Complex Integrated Avionics and System Safety June 9, 2005 7 Certification Challenges  “Functional” TSO: Difficult to separate TSO issues from installation issues –TSO’d function may be part of the software that resides on a circuit card. –TSO compliance can only be assessed when installed in the host system. –Even simple issues like part marking become complicated. –TSO change processes were not developed with these complex TSO “packages” in mind.  Engineering and Business practices: COTS products are not developed to traditional aviation standards. Detailed certification data and knowledge often resides at vendor rather than manufacturer.

9 Federal Aviation Administration 8 Complex Integrated Avionics and System Safety June 9, 2005 8 How the Authorities Have Responded  The authorities have already taken a number of actions to support recent IMA trends and specific projects, including: Development of IMA AC and TSO. Development of an Order on software reuse. Approval of functional TSOs. Numerous DO-178B/ED-12B “workarounds.” Additional relevant guidance is in work.  However, continued industry support is needed…

10 Federal Aviation Administration 9 Complex Integrated Avionics and System Safety June 9, 2005 9 What is Needed to Support the Trend?  Current software certification methods did not envision modern IMA architectures, so we need new methods… That are equally effective in ensuring safety… While supporting the certification of IMA.  The current TSO process is not well-suited for embedded software functions, so we need new approaches to TSOA… Which allow design and production approval for traditional TSO functions in IMA architectures… While protecting the level of safety provided by type certification processes.

11 Federal Aviation Administration 10 Complex Integrated Avionics and System Safety June 9, 2005 10 What is Needed to Support the Trend?  When manufacturers out-source development and test: New processes for authorities/manufacturer/vendor communication are needed.  Testing: Testing of the IMA “pieces” will not find integration problems. The actual airplane is not an adequate test environment for many IMA issues. Full-scale integration test facilities may not be commercially viable. Industry needs to help develop new approaches to integration testing that will find and characterize IMA problems before certification.

12 Federal Aviation Administration 11 Complex Integrated Avionics and System Safety June 9, 2005 11 Authority-Industry Partnership  Cooperation is needed more than ever. Traditional certification processes were developed to match past commercial practices The pace of change is increasing  Industry will need to lead the effort to develop new methods of compliance. New methods cannot just “do less” – they MUST preserve, and where possible, improve the level of safety. Focus on safety-related issues while with IMA, it is more difficult to separate what is or is not “safety-related.”

13 Federal Aviation Administration 12 Complex Integrated Avionics and System Safety June 9, 2005 12 Summary and Future Perspectives  The authorities support industry’s efforts to advance the technology Historic cooperation between the authorities and industry has been essential in developing viable and effective methods of compliance and safety assurance.  Cooperation is even more critical as we collectively support rapid technological advances while at the same time increase the level of safety.  Potential broader issue: Does the overall safety assessment process need to be revisited, to account for the migration of functionality (and failure conditions) from hardware to software?


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