000 02361cam a2200337 a 4500
003 EG-GiCUC
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008 151118s2015 ua dh f m 000 0 eng d
040 _aEG-GiCUC
_beng
_cEG-GiCUC
041 0 _aeng
049 _aDeposite
097 _aM.Sc
099 _aCai01.13.01.M.Sc.2015.Ah.D
100 0 _aAhmed Mohamed Hussein Ahmed
245 1 0 _aDevelopment of an iterative solution to the fire control problem /
_cAhmed Mohamed Hussein Ahmed ; Supervised Mohamed Sayed Bayoumi , Mohamed Kahlil Ibrahim
246 1 5 _a{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
260 _aCairo :
_bAhmed Mohamed Hussein Ahmed ,
_c2015
300 _a134 P. :
_bcharts , facsimiles ;
_c30cm
502 _aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 _aThe 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 
530 _aIssued also as CD
653 4 _aBallistics
653 4 _aFire Control
653 4 _aSpherical Dartboard Method
700 0 _aMohamed Kahlil Ibrahim ,
_eSupervisor
700 0 _aMohamed Sayed Bayoumi ,
_eSupervisor
856 _uhttp://172.23.153.220/th.pdf
905 _aNazla
_eRevisor
905 _aSoheir
_eCataloger
942 _2ddc
_cTH
999 _c53366
_d53366