HARDWARE CONNECTIVITY METHODS FOR LIVE WIRES

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" HARDWARE CONNECTIVITY METHODS FOR LIVE WIRES "

Document Type	:	Latin Dissertation
Language of Document	:	English
Record Number	:	151814
Doc. No	:	ET23606
Main Entry	:	Krishna Konda
Title Proper	:	HARDWARE CONNECTIVITY METHODS FOR LIVE WIRES
Note	:	This document is digital این مدرک بصورت الکترونیکی می باشد
Abstract	:	Wires in aircraft are often decades old. h order to detect the faults in the wirethat are inevitable, Utah State University is developing a method of testing them in situ.The method consists of placing Frequency Domain Reflectometer (FDR), microcontroller,and communication interface into the aircraft connector, making it a "smart connector."The aircraft wires are digital buses, which are unidirectional and bidirectional. The FDRin the smart connector sends out an analog sine wave into these unidirectional andbidirectional data buses.........-....,....-...,..tested for theQ1 PC1 bus cardBoth these projects mere sofixare des elopment efforts tonards contributing to dlfferentaspects of Roboucs and lZ1echatronics projects m the Controls and Roboucs Group..
Subject	:	Electericl tess
	:	برق
electronic file name	:	TL46850.pdf
Title and statement of responsibility and	:	HARDWARE CONNECTIVITY METHODS FOR LIVE WIRES [Thesis]