DOIONLINE 
DOIONLINE Publish In |
International Journal of Electrical, Electronics and Data Communication (IJEEDC)-IJEEDC |
 Journal Home Volume Issue |
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Issue |
Volume-5,Issue-11 ( Nov, 2017 ) | |||||||||
Paper Title |
Modeling and Analysis of a Prototype of Multiple Launch Rocket System using Matlab Simulink | |||||||||
Author Name |
Narongkorn Dernlugkam, Rungtawan Chodsirisak | |||||||||
Affilition |
Military Vehicle Division, Quality Control and Standardization Division Defence Technology Institute (Public Organisation) Ministry of Defence, The Kingdom of Thailand | |||||||||
Pages |
7-11 | |||||||||
Abstract |
This paper presented the control modeling and analysis of the prototype of Multiple Launch Rocket System (MLRS) using Matlab Simulink. The mathematical model was determined using physical law and theoretical foundation of the turning mechanism control system and the elevating mechanism control system. Then, the model was identified in Matlab Simulink and analyzed in open-loop frequency characteristic analysis, closed-loop frequency characteristic analysis, step response characteristic analysis, and sinusoidal response analysis. The simulation results showed a good stability performance for both open-loop control and closed-loop control systems. We observed the fast response of tracking and controlling with the overshoot less than 3% and the steady-state error less than 0.2 Mil. Index terms - Modeling, Multiple Launch Rocket System, Matlab Simulink. | |||||||||
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