期刊名称：International Journal of Innovative Research in Computer and Communication Engineering
印刷版ISSN：2320-9798
电子版ISSN：2320-9801
出版年度：2015
卷号：3
期号：11
DOI：10.15680/IJIRCCE.2015.0311084
出版社：S&S Publications
摘要：A launch induced acoustic equipment represents a dynamic load on the exposed facilities and groundsupport equipment in the form of random pressures fluctuating around the ambient atmospheric pressure. In response tothese fluctuating pressures, structural vibrations are generated and transmitted throughout the structure and equipmentsupported to it. During the testing of aircrafts, there is a need of measuring and monitoring of various physicalparameters. These physical parameters like vibration, temperature, pressure, obstacle range etc., should be withinspecified limits. So based on the limits we can estimate and secure or protect them in required way to utilize in realtime. So for that purpose here we are including various sensors, controller. And it can be monitored on PC or LCD.
