Method for Estimation the Veracity of Diagnosis of the Aircraft Navigation and Landing Radio-Electronic Systems

Abstract

The method for estimation of veracity of the diagnostics of an aircraft landing and navigation radio-electronic system dismantled units is given in this article. It considers the stimulating signals source instability and the object of diagnosis reliability. Settlement formulas are offered for an assessment of the veracity indicators. These formulas take into account specifics of the aircraft landing and navigation system diagnosis device.