May 17th, 2012 – General Meeting (Peter Seiler – U of M)

The next general meeting of the ION North Star Section will be Thursday May 17th in Mechanical Engineering Building Room 1130 at the University of Minnesota ( custodia iphone outlet acheter coque iphone en ligne The keynote speaker at this meeting will be a presentation on the Design and Analysis of Safety Critical Systems by Peter Seiler from the University of Minnesota. Please email us at, if you plan to attend. custodia iphone Agenda: 6:00 Meet and Greet 6:30 Keynote Speaker 7:45 Section Business 8:00 Closing remarks Sandwiches and beverages will be served during the Meet and Greet portion of the meeting. The keynote presentation will be: Title: Design and Analysis of Safety Critical Systems Presenter: Peter Seiler (University of Minnesota) Abstract: The FAA (US) and JAA (European) certification authorities impose high demands on the reliability of safety-critical aircraft systems. cover iphone outlet coque iphone The high degree of reliability is typically achieved through the use of physically redundant components. custodia huawei shop coque iphone xs Commercial aircraft such as the Boeing 777 have redundant control surfaces, sensors, processors, hydraulic lines, and communication networks. cover iphone custodia coque iphone soldes This talk will first review the design challenges associated with redundancy management for commercial aircraft. One drawback of physical redundancy is the increased size, cost, weight, and power requirements. Some aircraft, e.g. custodia outlet samsung s8 UAVs, cannot be designed to meet the conflicting design requirements imposed by the use of physical redundancy for reliability. coque iphone Model-based fault detection provides an alternative means to achieve high levels of reliability without using redundant physical hardware. coque iphone x These analytical methods detect faults using dynamic models to relate the behavior of various subsystems and sensor measurements. coque iphone xr Systems that use analytical redundancy must also demonstrate the required levels of reliability to certification authorities. A major obstacle to the use of analytical fault detection in aerospace systems is the lack of appropriate tools to analyze and certify the performance of these systems.

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