RELIABILITY EVALUATION MATHEMATICAL MODEL OF AVIONICS ITEM WITH AN UNLOADED RESERVE

O. A. Kuznetsova


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Abstract

Faultness evaluation mathematical model for avionics item with loaded duplication and an additional unloaded reserve is designed. The model takes into account incomplete operation control of devices, and time delay in the engaging of unloaded device. Comparative analysis of structural reservation variants is done.


Keywords: reliability, faultness, unloaded reserve, operation control
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