01367nas a2200241 4500000000100000000000100001000000100002008004100003260000900044653002100053653002100074653002200095653003500117653000800152653004800160653002000208100002300228700002000251245011900271300001200390490000700402520071600409 2012 d c201210aAssurance Method10aComputation Node10aFunctional Safety10aFunctional-Architectural Model10aI&C10aOn-board Instrumentation and Control System10aReconfiguration1 aAleksandr Kharybin1 aViktoriya Pohyl00aMethods of Assuring the Functional Safety of Aircraft On-Board Instrumentation&Control Systems in Their Life Cycle a296-3120 v283 a
This paper describes an approach for assuring the functional safety of perspective aircraft on-board Instrumentation & Control (I&C) systems on the basis of reconfigurable computation nodes (CN). The functional-architectural model of aircrafts on-board I&C systems with possibility for CN reconfiguration, as well as enhanced method for assuring the functional safety of aircrafts on-board I&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.