Re-configurable avionics architecture algorithm for embedded applications

Ananda, CM (2007) Re-configurable avionics architecture algorithm for embedded applications. In: IADIS International Conference on Intelligent System and Agents, 3-5 Jul 2007, Lisbon, Portugal.

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    Abstract

    The paper presents a new method for re-configuration of tasks or a process in an embedded avionics application. The13; proposed algorithm works based on four control parameters: re-configurability Information factor, Schedulability13; Test/TL/UF, Context Adaptability/suitability and Context Flight Safety. The algorithm is data centric and interfaces13; system health as control input and initiation of the re-configuration is only after successful evaluation of the parameter metrics. It enhances the availability and reliability of the system under failed conditions by efficient selection and procedural re-configuration with safe state exit. The advantage of the new approach over the non-configurable systems is the increased availability of flight critical applications under failed conditions. It also preserves the advantages of non-Reconfigurable systems over federated architecture. Invalid failure of control parameter brings the system to safe state. The scheme, algorithm and the control parameters metrics and their validation approach are described. The algorithm is13; novel in terms of dynamic re-configuration compared to existing static avionics architecture

    Item Type: Conference or Workshop Item (Paper)
    Uncontrolled Keywords: Flight critical systems;Line replaceable unit;Integrated modular avionics;Time loading;Major frame
    Subjects: AERONAUTICS > Air Transportation and Safety
    AERONAUTICS > Avionics & Aircraft Instrumentation
    Division/Department: Aerospace Electronics and Controls Division
    Depositing User: Ms. Alphones Mary
    Date Deposited: 03 Nov 2009
    Last Modified: 17 Jun 2010 15:17
    URI: http://nal-ir.nal.res.in/id/eprint/5214

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