TY  - JOUR
T1  - Impact on Failure in an Electro Mechanical Actuator Based
Servo System Using Sequel
AU - Suja, S. AU - Nivedita, A. 
JO  - International Journal of System Signal Control and Engineering Application
VL  - 11
IS  - 3
SP  - 41
EP  - 47
PY  - 2018
DA  - 2001/08/19
SN  - 1997-5422
DO  - ijssceapp.2018.41.47
UR  - https://makhillpublications.co/view-article.php?doi=ijssceapp.2018.41.47
KW  - subsystems
KW  -undetected actuator
KW  -weight ratios
KW  -sequel
KW  -Electro Mechanical Actuator (EMA)
KW  -successfully analysed
AB  - 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.
ER  -