Parametric Comparison of Four Different Missile System
Parametric Comparison of Four Different Missile System
In the design of a missile, the rocket engine, aerodynamics, structural warhead, fuse, launcher and control unit are important with the guidance system. Four different missiles named as Atgm_1, Low Drag_8, Patriot_TR, and New Missile are designed. The structure and working principle of the missiles are analized. The designed missiles were simulated at a platform with shooter and target values determined by the Rocket Simulator Program. Speed, distance, altitude, mach number and maneuverability number which are important criteria during the cruise, test flight or when the missiles take action to hit the target were evaluated by test flights in the simulation.
Keywords:
Defence Technologies, Defence Industry Missile Design, Test Flight,
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- [1] G. Yıldırım, “Guidance Systems in Missiles”, 2007.
- [2] G. Yılmaz, “ Comparative Analysis of Different Guidance Algorithms for an Air to Surface Missile“ , MSc Thesis, Baskent University, 2019.
- [3] C. Ada, “ Design and Comparison of Autopilots of an Air-to-Surface Anti-Tank Missile and its Terminal Guidance Systems“, MSc Thesis, Istanbul Technical University, 2011.
- [4] M. Becan, “Fuzzy Control in the Guided Missiles“, PhD Thesis, Istanbul Technical University, 2001.
- [5] E. Yalcin, “The Analyzing of Missile Guidance and Control Systems with Artificial Neural Networks“, MSc Thesis, Selcuk University, 2009.
- [6] G. Icoz, “Analytical Study of Guidance and Control Systems of Missiles and Rockets with Strike tot he Target“, Trakya University, 2010.
- [7] Savunma Sanayist. “Roket ve Füze Nedir?”, 2020.
- [8] M. Lorell, J. Lowell, M. Kennedy, H. Levaux, F. Cheaper, “Better: Commerical Approaches to Weapons Acquisiton”, 2000.
- [9] E.L. Fleeman, “Tactical Missile Design”, American Institute of Aeronautics and Astronautics, Inc., 2001.
- [10] Roketsan. “Model Roketçilik”, 2020.
- [11] Ö. Vural, “Fuzzy Logic Guidance System Design for Guided Missiles” Middle East Technical University, 2003.
- [12] M. Arıcan, “ The Investigation of an Air Breathing Rocket Engine Powered Vehicle“, MSc Thesis, Istanbul Technical University, 2003.
- [13] N. Sampo, “Aerodynamic Properties of Model Rockets”, 29 Haziran, 2020. http://sampo.kapsi.fi/tmp/techdoc/techdoc.html
- [14] Y.A. Cengel, J. Cimbala, “Fluid Mechanics Fundamental and Applications”, Wilmington: McGraw-Hill, 2014.
- [15] E. Tiryaki, “Calculation of Aerodynamic Coefficients, Stability, Properties and Trajectory of Spin-Stabilized Projectiles“, MSc Thesis, Ankara University, 2009.
- [16] E. Hardester, P. Kinghorn, “Rocket Fin Design”, 2013.
- [17] J. Strickland, “Missile Flight Simulation”, Lulu Press, 2015.
- [18] X. Liu, S. Tang, J. Guo, Y. Yun, Z. Chen, “Midcourse Guidance Law Based on High Target Acquisition Probability Considering Angular Constraint and Line-of-Sight Angle Rate Control” 2016.
- [19] Federation of American Scientists, “Warheads”,2020 https://fas.org/man/dod-101/navy/docs/fun/part13.html
- ISSN: 2651-5199
- Başlangıç: 2018
- Yayıncı: İstanbul Gedik Üniversitesi
Sayıdaki Diğer Makaleler
Parametric Comparison of Four Different Missile System
Mehmet TOPALÖMER, Çiğdem GÜNDOĞAN TÜRKER
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