Parametric Comparison of Four Different Missile System
Öz
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.
Anahtar Kelimeler
Kaynakça
- [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.
Ayrıntılar
Birincil Dil
İngilizce
Konular
Mühendislik
Bölüm
Araştırma Makalesi
Yayımlanma Tarihi
1 Eylül 2019
Gönderilme Tarihi
5 Mayıs 2019
Kabul Tarihi
22 Temmuz 2019
Yayımlandığı Sayı
Yıl 2019 Cilt: 2 Sayı: 2
APA
Topalömer, M., & Gündoğan Türker, Ç. (2019). Parametric Comparison of Four Different Missile System. International Journal of Engineering and Natural Sciences, 2(2), 15-20. https://izlik.org/JA93HS42CY
AMA
1.Topalömer M, Gündoğan Türker Ç. Parametric Comparison of Four Different Missile System. IJENS. 2019;2(2):15-20. https://izlik.org/JA93HS42CY
Chicago
Topalömer, Mehmet, ve Çiğdem Gündoğan Türker. 2019. “Parametric Comparison of Four Different Missile System”. International Journal of Engineering and Natural Sciences 2 (2): 15-20. https://izlik.org/JA93HS42CY.
EndNote
Topalömer M, Gündoğan Türker Ç (01 Eylül 2019) Parametric Comparison of Four Different Missile System. International Journal of Engineering and Natural Sciences 2 2 15–20.
IEEE
[1]M. Topalömer ve Ç. Gündoğan Türker, “Parametric Comparison of Four Different Missile System”, IJENS, c. 2, sy 2, ss. 15–20, Eyl. 2019, [çevrimiçi]. Erişim adresi: https://izlik.org/JA93HS42CY
ISNAD
Topalömer, Mehmet - Gündoğan Türker, Çiğdem. “Parametric Comparison of Four Different Missile System”. International Journal of Engineering and Natural Sciences 2/2 (01 Eylül 2019): 15-20. https://izlik.org/JA93HS42CY.
JAMA
1.Topalömer M, Gündoğan Türker Ç. Parametric Comparison of Four Different Missile System. IJENS. 2019;2:15–20.
MLA
Topalömer, Mehmet, ve Çiğdem Gündoğan Türker. “Parametric Comparison of Four Different Missile System”. International Journal of Engineering and Natural Sciences, c. 2, sy 2, Eylül 2019, ss. 15-20, https://izlik.org/JA93HS42CY.
Vancouver
1.Mehmet Topalömer, Çiğdem Gündoğan Türker. Parametric Comparison of Four Different Missile System. IJENS [Internet]. 01 Eylül 2019;2(2):15-20. Erişim adresi: https://izlik.org/JA93HS42CY