Linearization of Anti-Tank Guided Missile

Mohamed Abdallah Mohamed; Ahmed Nasr Ouda; Bahaaeldin Gamal Abdelaty; Ahmed Hassan

doi:doi:10.11648/j.acis.20190701.12

| Peer-Reviewed

Linearization of Anti-Tank Guided Missile

Mohamed Abdallah Mohamed, Ahmed Nasr Ouda, Bahaaeldin Gamal Abdelaty, Ahmed Hassan

Published in Automation, Control and Intelligent Systems (Volume 7, Issue 1)

Received: 25 February 2019 Accepted: 11 April 2019 Published: 17 May 2019

Views: Downloads:

Download PDF

Share This Article

Twitter
Linked In
Facebook

Abstract

Anti-tank surface to surface guided missile systems are considered to be one of the most powerful weapons in the modern war. Due to their effectiveness against either fortifications or tanks in addition to their relative low weight, they are deployed in the field easily. One of the most challenges the engineers face while designing a guided missile is the autopilot design. The autopilot loop or the inner loop of the missile should steer the missile during its spatial flight till hitting the target even it is moving or stationary. A higher maneuver target was hit by the missile, the more reliable autopilot you design. On designing a mature autopilot, a promising mathematical model of the missile should be in hand and mathematical linearized model should be derived. This paper presents a mathematical representation of an anti-tank guided missile the mathematical linearized model as well so that the design of the missile autopilot is presented in the future work.

Published in	Automation, Control and Intelligent Systems (Volume 7, Issue 1)
DOI	10.11648/j.acis.20190701.12
Page(s)	9-17
Creative Commons	This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.
Copyright	Copyright © The Author(s), 2019. Published by Science Publishing Group

Keywords

Guided Missiles, Autopilot, Linearization, Anti-tank, Classical Controller, Transfer Function

References

[1]	M. A. Mohamed, “Performance Enhancemet of Autopilot Design for Short Rnage Missile using Advanced Control Techniques,” Electric, Military Technical College, Cairo, 2016.
[2]	N. Jack N, Missile Aerodynamics, Mountain View, USA, 1988.
[3]	P. Zarcan, “Tactical and Strategic Missile Guidance,” Progress in Astronautics and Aeronautic. AIAA, 1994.
[4]	R. M. Goreckt, A baseline 6 degree of freedom mathematical model of generic missile, DSTO Systems Sciences Laboratory Australia 2003.
[5]	G. M. Siouris, Missile Guidance and Control Systems, Ohio, USA, 2003.
[6]	J. D. Anderson, FUNDAMENTALS OF AERODYNAMICS, 1991.
[7]	G. El-Sheikh, Guidance System and Theory, Cairo, 2010.
[8]	A. H. A. Elsayed Ahmed, A. N. Ouda, H. Eldin Hussein Ahmed, H. Mohamed Abd-Elkader, “Modeling of a Small Unmanned Aerial Vehicle,” the International Journal of advanced robotic and automation vol. 4, no. 126, 2015.
[9]	A. N. Ouda, “Adaptive Autopilot Design for Flying Vehicle,” the International journal of dynamic and control (IJDAC), 2017.
[10]	A. N. O. M. Abdallah, “Modeling and Simulation of An-Anti Tank Guided Missile” International Journal of Engineering Research and Technology vol. 7, no. 09, 2018.
[11]	L. S. a. Callaborators, Principles of Guided Missile Design, 1955.
[12]	B. G. A. Ahmed Hassan Ahmed, A. N. Ouda, Ahmed Mohsen Kamel and Yehia Zakaria El-Halwagy, “Autopilot Design of Unmanned Aerial Vehicle,” International journal of aeronautics and aerospace engineering, vol. 7, 2018.
[13]	A. N. O. El-gabri, Ahmed S. Ahmed, Yehia Z. Elhalwagy and Ahmed Khamis, “Command Guidance Missile Tracking Algorithms Evaluation Based On Visual Simulation,” International Journal of Engineering Research and Technology, vol. 7, pp. 110-116, 2018.
[14]	G. El-Sheikh and N. El. Hamwe, “Autopilot Design for a LOS Anti-tank Guided Missile,” Int. Conf. Aerosp. Sci. Aviat. Technol., 2019.

Cite This Article

Plain Text BibTeX RIS

APA Style

Mohamed Abdallah Mohamed, Ahmed Nasr Ouda, Bahaaeldin Gamal Abdelaty, Ahmed Hassan. (2019). Linearization of Anti-Tank Guided Missile. Automation, Control and Intelligent Systems, 7(1), 9-17. https://doi.org/10.11648/j.acis.20190701.12

Copy | Download

ACS Style

Mohamed Abdallah Mohamed; Ahmed Nasr Ouda; Bahaaeldin Gamal Abdelaty; Ahmed Hassan. Linearization of Anti-Tank Guided Missile. Autom. Control Intell. Syst. 2019, 7(1), 9-17. doi: 10.11648/j.acis.20190701.12

Copy | Download

AMA Style

Mohamed Abdallah Mohamed, Ahmed Nasr Ouda, Bahaaeldin Gamal Abdelaty, Ahmed Hassan. Linearization of Anti-Tank Guided Missile. Autom Control Intell Syst. 2019;7(1):9-17. doi: 10.11648/j.acis.20190701.12

Copy | Download

@article{10.11648/j.acis.20190701.12,
  author = {Mohamed Abdallah Mohamed and Ahmed Nasr Ouda and Bahaaeldin Gamal Abdelaty and Ahmed Hassan},
  title = {Linearization of Anti-Tank Guided Missile},
  journal = {Automation, Control and Intelligent Systems},
  volume = {7},
  number = {1},
  pages = {9-17},
  doi = {10.11648/j.acis.20190701.12},
  url = {https://doi.org/10.11648/j.acis.20190701.12},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.acis.20190701.12},
  abstract = {Anti-tank surface to surface guided missile systems are considered to be one of the most powerful weapons in the modern war. Due to their effectiveness against either fortifications or tanks in addition to their relative low weight, they are deployed in the field easily. One of the most challenges the engineers face while designing a guided missile is the autopilot design. The autopilot loop or the inner loop of the missile should steer the missile during its spatial flight till hitting the target even it is moving or stationary. A higher maneuver target was hit by the missile, the more reliable autopilot you design. On designing a mature autopilot, a promising mathematical model of the missile should be in hand and mathematical linearized model should be derived. This paper presents a mathematical representation of an anti-tank guided missile the mathematical linearized model as well so that the design of the missile autopilot is presented in the future work.},
 year = {2019}
}

Copy | Download

TY  - JOUR
T1  - Linearization of Anti-Tank Guided Missile
AU  - Mohamed Abdallah Mohamed
AU  - Ahmed Nasr Ouda
AU  - Bahaaeldin Gamal Abdelaty
AU  - Ahmed Hassan
Y1  - 2019/05/17
PY  - 2019
N1  - https://doi.org/10.11648/j.acis.20190701.12
DO  - 10.11648/j.acis.20190701.12
T2  - Automation, Control and Intelligent Systems
JF  - Automation, Control and Intelligent Systems
JO  - Automation, Control and Intelligent Systems
SP  - 9
EP  - 17
PB  - Science Publishing Group
SN  - 2328-5591
UR  - https://doi.org/10.11648/j.acis.20190701.12
AB  - Anti-tank surface to surface guided missile systems are considered to be one of the most powerful weapons in the modern war. Due to their effectiveness against either fortifications or tanks in addition to their relative low weight, they are deployed in the field easily. One of the most challenges the engineers face while designing a guided missile is the autopilot design. The autopilot loop or the inner loop of the missile should steer the missile during its spatial flight till hitting the target even it is moving or stationary. A higher maneuver target was hit by the missile, the more reliable autopilot you design. On designing a mature autopilot, a promising mathematical model of the missile should be in hand and mathematical linearized model should be derived. This paper presents a mathematical representation of an anti-tank guided missile the mathematical linearized model as well so that the design of the missile autopilot is presented in the future work.
VL  - 7
IS  - 1
ER  -

Copy | Download

Author Information

Mohamed Abdallah Mohamed

Electrical Engineering Department, Technical Research Center, Cairo, Egypt
Ahmed Nasr Ouda

Electrical Engineering Department, Technical Research Center, Cairo, Egypt
Bahaaeldin Gamal Abdelaty

Electrical Engineering Department, Technical Research Center, Cairo, Egypt
Ahmed Hassan

Electrical Engineering Department, Technical Research Center, Cairo, Egypt

Download PDF

Sections

Plain Text BibTeX RIS

APA Style

Mohamed Abdallah Mohamed, Ahmed Nasr Ouda, Bahaaeldin Gamal Abdelaty, Ahmed Hassan. (2019). Linearization of Anti-Tank Guided Missile. Automation, Control and Intelligent Systems, 7(1), 9-17. https://doi.org/10.11648/j.acis.20190701.12

Copy | Download

ACS Style

Mohamed Abdallah Mohamed; Ahmed Nasr Ouda; Bahaaeldin Gamal Abdelaty; Ahmed Hassan. Linearization of Anti-Tank Guided Missile. Autom. Control Intell. Syst. 2019, 7(1), 9-17. doi: 10.11648/j.acis.20190701.12

Copy | Download

AMA Style

Mohamed Abdallah Mohamed, Ahmed Nasr Ouda, Bahaaeldin Gamal Abdelaty, Ahmed Hassan. Linearization of Anti-Tank Guided Missile. Autom Control Intell Syst. 2019;7(1):9-17. doi: 10.11648/j.acis.20190701.12

Copy | Download

@article{10.11648/j.acis.20190701.12,
  author = {Mohamed Abdallah Mohamed and Ahmed Nasr Ouda and Bahaaeldin Gamal Abdelaty and Ahmed Hassan},
  title = {Linearization of Anti-Tank Guided Missile},
  journal = {Automation, Control and Intelligent Systems},
  volume = {7},
  number = {1},
  pages = {9-17},
  doi = {10.11648/j.acis.20190701.12},
  url = {https://doi.org/10.11648/j.acis.20190701.12},
  eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.acis.20190701.12},
  abstract = {Anti-tank surface to surface guided missile systems are considered to be one of the most powerful weapons in the modern war. Due to their effectiveness against either fortifications or tanks in addition to their relative low weight, they are deployed in the field easily. One of the most challenges the engineers face while designing a guided missile is the autopilot design. The autopilot loop or the inner loop of the missile should steer the missile during its spatial flight till hitting the target even it is moving or stationary. A higher maneuver target was hit by the missile, the more reliable autopilot you design. On designing a mature autopilot, a promising mathematical model of the missile should be in hand and mathematical linearized model should be derived. This paper presents a mathematical representation of an anti-tank guided missile the mathematical linearized model as well so that the design of the missile autopilot is presented in the future work.},
 year = {2019}
}

Copy | Download

TY  - JOUR
T1  - Linearization of Anti-Tank Guided Missile
AU  - Mohamed Abdallah Mohamed
AU  - Ahmed Nasr Ouda
AU  - Bahaaeldin Gamal Abdelaty
AU  - Ahmed Hassan
Y1  - 2019/05/17
PY  - 2019
N1  - https://doi.org/10.11648/j.acis.20190701.12
DO  - 10.11648/j.acis.20190701.12
T2  - Automation, Control and Intelligent Systems
JF  - Automation, Control and Intelligent Systems
JO  - Automation, Control and Intelligent Systems
SP  - 9
EP  - 17
PB  - Science Publishing Group
SN  - 2328-5591
UR  - https://doi.org/10.11648/j.acis.20190701.12
AB  - Anti-tank surface to surface guided missile systems are considered to be one of the most powerful weapons in the modern war. Due to their effectiveness against either fortifications or tanks in addition to their relative low weight, they are deployed in the field easily. One of the most challenges the engineers face while designing a guided missile is the autopilot design. The autopilot loop or the inner loop of the missile should steer the missile during its spatial flight till hitting the target even it is moving or stationary. A higher maneuver target was hit by the missile, the more reliable autopilot you design. On designing a mature autopilot, a promising mathematical model of the missile should be in hand and mathematical linearized model should be derived. This paper presents a mathematical representation of an anti-tank guided missile the mathematical linearized model as well so that the design of the missile autopilot is presented in the future work.
VL  - 7
IS  - 1
ER  -

Copy | Download