Stability Analysis of Autopilot Systems For Ballistic Missile Using MATLAB

Authors
A.J.ARUN JEYA PRAKASH, M. RAJA, SHIKHA GUPTA, SOORYA KUMAR, YADVENDER SINGH DHILLON
Corresponding Author
A.J.ARUN JEYA PRAKASH
Available Online April 2013.
Abstract
This paper deals with the modelling and stability analysis of the Automatic Flight Control systems for a Ballistic Missile using Matlab. The Root Locus Analysis of the System is programmed in Matlab for four different transfer functions corresponding to different Aerodynamic Coefficients for the Vanguard Missile. The Paper includes two configurations of the missile Autopilot system one with Lead Compensator and without it. A comparison of these configurations has been done for the Missile autopilot system.
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Proceedings
Proceedings of the Conference on Advances in Communication and Control Systems-2013
Part of series
Advances in Intelligent Systems Research
Publication Date
April 2013
ISBN
978-90-78677-66-6
ISSN
1951-6851
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - A.J.ARUN JEYA PRAKASH
AU  - M. RAJA
AU  - SHIKHA GUPTA
AU  - SOORYA KUMAR
AU  - YADVENDER SINGH DHILLON
PY  - 2013/04
DA  - 2013/04
TI  - Stability Analysis of Autopilot Systems For Ballistic Missile Using MATLAB
BT  - Proceedings of the Conference on Advances in Communication and Control Systems-2013
PB  - Atlantis Press
SP  - 327
EP  - 331
SN  - 1951-6851
UR  - https://www.atlantis-press.com/article/6328
ID  - PRAKASH2013/04
ER  -