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Development of an iterative solution to the fire control problem / Ahmed Mohamed Hussein Ahmed ; Supervised Mohamed Sayed Bayoumi , Mohamed Kahlil Ibrahim

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Ahmed Mohamed Hussein Ahmed , 2015Description: 134 P. : charts , facsimiles ; 30cmOther title:
  • {uFE97}طو{uئآئإ}ر {uئإء٣}ل {uئإ٩٧}{uئإؤآ}راري {uئإؤئ}{uئإإ٣}{uئإآ٣}{uئإ٨٤}{uئإؤئ}{uئإ٩٤} ا{uئإؤئ}{uئإ٩٧}{uئإء٣}{uئإؤآ}م {uئإؤ٣}{uئإئ٢} ا{uئإؤئ}{uئإإ٣}{uئإؤ٨}ذو{uئإؤ٣}{uئإ٨إ}ت [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: The fire control problem can be defined as how to point a gun so that the fired projectile will hit the target. This research aims to develop a new method of solving the fire control problem for air-defense applications. This method is based on the iterative numerical solution of the equations of motion of the projectile in real time using a point-mass or a six-degrees-of-freedom ballistic trajectory model while utilizing a complete aerodynamic model for the projectile obtained using PRODAS software package. The effect of computational time on the hit accuracy and the maximum target{u2019}s speed that can be handled is also studied. The method is tested using computer simulations against different target scenarios and successful hits are obtained using a few iterations. The results also revealed the effect of computational time on decreasing the hit accuracy and the target{u2019}s maximum speed 
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Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2015.Ah.D (Browse shelf(Opens below)) Not for loan 01010110066737000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2015.Ah.D (Browse shelf(Opens below)) 66737.CD Not for loan 01020110066737000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

The fire control problem can be defined as how to point a gun so that the fired projectile will hit the target. This research aims to develop a new method of solving the fire control problem for air-defense applications. This method is based on the iterative numerical solution of the equations of motion of the projectile in real time using a point-mass or a six-degrees-of-freedom ballistic trajectory model while utilizing a complete aerodynamic model for the projectile obtained using PRODAS software package. The effect of computational time on the hit accuracy and the maximum target{u2019}s speed that can be handled is also studied. The method is tested using computer simulations against different target scenarios and successful hits are obtained using a few iterations. The results also revealed the effect of computational time on decreasing the hit accuracy and the target{u2019}s maximum speed 

Issued also as CD

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