<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="7.x">Drupal-Biblio</source-app><ref-type>17</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Aleksandr Kharybin</style></author><author><style face="normal" font="default" size="100%">Viktoriya Pohyl</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">Methods of Assuring the Functional Safety of Aircraft On-Board Instrumentation&amp;Control Systems in Their Life Cycle</style></title><secondary-title><style face="normal" font="default" size="100%">Information &amp; Security: An International Journal</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">Assurance Method</style></keyword><keyword><style  face="normal" font="default" size="100%">Computation Node</style></keyword><keyword><style  face="normal" font="default" size="100%">Functional Safety</style></keyword><keyword><style  face="normal" font="default" size="100%">Functional-Architectural Model.</style></keyword><keyword><style  face="normal" font="default" size="100%">I&amp;C</style></keyword><keyword><style  face="normal" font="default" size="100%">On-board Instrumentation and Control System</style></keyword><keyword><style  face="normal" font="default" size="100%">Reconfiguration</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">2012</style></year><pub-dates><date><style  face="normal" font="default" size="100%">2012</style></date></pub-dates></dates><number><style face="normal" font="default" size="100%">24</style></number><volume><style face="normal" font="default" size="100%">28</style></volume><pages><style face="normal" font="default" size="100%">296-312</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">This paper describes an approach for assuring the functional safety of perspective aircraft on-board Instrumentation &amp; Control (I&amp;C) systems on the basis of reconfigurable computation nodes (CN). The functional-architectural model of aircrafts on-board I&amp;C systems with possibility for CN reconfiguration, as well as enhanced method for assuring the functional safety of aircrafts on-board I&amp;C systems on their design stage and a new method for assuring this feature during the operational stage of such systems, based on the proposed model and which consider the on-line criticality and reliability control results of certain elements and functional subsystems is proposed and discussed.</style></abstract><issue><style face="normal" font="default" size="100%">2</style></issue></record></records></xml>