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.
- Copyright
- © 2013, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
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 (CAC2S 2013) PB - Atlantis Press SP - 327 EP - 331 SN - 1951-6851 UR - https://www.atlantis-press.com/article/6328 ID - PRAKASH2013/04 ER -