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International Journal of System Signal Control and Engineering Application

ISSN: Online
ISSN: Print 1997-5422
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Impact on Failure in an Electro Mechanical Actuator Based Servo System Using Sequel

A. Nivedita and S. Suja
Page: 41-47 | Received 21 Sep 2022, Published online: 21 Sep 2022

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Abstract

Main focus of this research is the modeling of Electro Mechanical Actuator (EMA) based servo system using sequel, identifying and analyzing the impact of failures on the system by simulation. EMA systems combine high performance speed, current and position control with the flexibility to adapt the systems to the rapidly changing needs of the industries. In the aerospace applications EMA is used in the field of flight control system, missiles or launch vehicles, since, it is compact and offer high power to weight ratios and motion velocities. Any undetected actuator failure lead to serious consequences. EMA consists of electrical, electronic and mechanical subsystems that result in intricate failures. Any fault in these sub-systems needs to be successfully analysed.


How to cite this article:

A. Nivedita and S. Suja. Impact on Failure in an Electro Mechanical Actuator Based Servo System Using Sequel.
DOI: https://doi.org/10.36478/ijssceapp.2018.41.47
URL: https://www.makhillpublications.co/view-article/1997-5422/ijssceapp.2018.41.47