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<doi>0630-cd</doi>
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<title-group>
<article-title>Estimation of Reliability for Aircraft Systems as Regards the Impact of Destructive Ageing Processes</article-title>
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<author>Mariusz Zieja<sup>1</sup>, Mariusz Wa&#380;ny<sup>2,a</sup>, Michal Jasztal<sup>2,b</sup> and S&#322;awomir St&#281;pie&#324;<sup>2,c</sup></author>

<aff><sup>1</sup>Air Force Institute of Technology, Warsaw, Poland</aff>

<email><a href="mailto:mariusz.zieja@itwl.pl">mariusz.zieja@itwl.pl</a></email>

<aff><sup>2</sup>Military University of Technology, Warsaw, Poland</aff>

<email><a href="mailto:mariusz.wazny@wat.edu.pl"><sup>a</sup>mariusz.wazny@wat.edu.pl</a></email>

<email><a href="mailto:michal.jasztal@wat.edu.pl"><sup>b</sup>michal.jasztal@wat.edu.pl</a></email>

<email><a href="mailto:slawomir.stepien@wat.edu.pl"><sup>c</sup>slawomir.stepien@wat.edu.pl</a></email>

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<abstract>
<title>ABSTRACT</title>
<p>The study presents a method allowing to determine the time of the presence of the sensor of angle of attack and of angle of slideslip in usage based on the analysis of the values of diagnostic parameters registered during its operation. The presented method is universal and allows its use in a wide range of technical systems whose condition is determined on the basis of the analysis of diagnostic parameters.</p>
<p><italic>Keywords: </italic>Diagnostic parameter, Performance time, Sensor of angle of attack and of angle of slideslip.</p>
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