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  5. Mathematical model substantiation of test diagnostic for aeronautical complex aircraft

Mathematical model substantiation of test diagnostic for aeronautical complex aircraft

V.V. Ardelian, D.N. Obidin, A.P. Musienko
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Method of diagnosing test elements Piloting the aircraft navigation system, which is fully determined by the nature of the diagnostic core, is investigated and proved. The basic feature of the diagnostics test elements of flight and navigation system is determined.
Keywords: functional stability, elements of flight and navigation system, diagnostic core test diagnostics
Reference:
Ardelian, V.V., Obidin, D.M. and Musiienko, A.P. (2016), "Obgruntuvannia matematychnoi modeli testovoho diahnostuvannia pilotazhno-navihatsiinoho kompleksu povitrianoho sudna" [Mathematical model substantiation of test diagnostic for aeronautical complex aircraft], Information Processing Systems, Vol. 8(145), pp. 17-20.