| Peer-Reviewed

Linearization of Anti-Tank Guided Missile

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

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    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

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    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

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  • @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}
    }
    

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    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
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Author Information
  • Electrical Engineering Department, Technical Research Center, Cairo, Egypt

  • Electrical Engineering Department, Technical Research Center, Cairo, Egypt

  • Electrical Engineering Department, Technical Research Center, Cairo, Egypt

  • Electrical Engineering Department, Technical Research Center, Cairo, Egypt

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