The automatic monitoring system of a condition of elements of a glass cover of aircrafts

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The automatic monitoring system of aircraft glass elements condition is developed on the basis of step-by-step computer restoration methods of the written down wavefront of laser radiation intensity change at its passage through testing object and a method of the analysis of speckle-structures registered on the CCD-matrix at reflection of laser radiation from classified defect.

Holographic image, spekl-structure, defect definition

Короткий адрес: https://sciup.org/148201245

IDR: 148201245

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