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Design of a real time control system for missiles guidance / Emad Mahros Rabee Mohammed ; Supervised Hassen Taher Dorrah , Gamal Mahmoud Sayd

By: Contributor(s): Material type: TextTextLanguage: eng Publication details: Cairo : Emad Mahros Rabee Mohammed , 2009Description: 130 Leaves : facsimiles , plans ; 30cmOther title:
  • تصميم نظام تحكم فى الزمن الحقيقى لتوجيه الصواريخ [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Electrical Power and Machines Summary: The objective of this thesis is to investigate and enhance the system performance of a homing guided missile via synthesizing its homing head using proposed classical and advanced control techniques. Thus, the thesis presents the derivation of missile 6DOF model augmented by a more realistic homing head. The design and analysis is carried out with the linearized models at pre-specified flight conditions
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Item type Current library Home library Call number Copy number Status Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.07.M.Sc.2009.Em.D (Browse shelf(Opens below)) Not for loan 01010110051386000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.07.M.Sc.2009.Em.D (Browse shelf(Opens below)) 51386.CD Not for loan 01020110051386000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Electrical Power and Machines

The objective of this thesis is to investigate and enhance the system performance of a homing guided missile via synthesizing its homing head using proposed classical and advanced control techniques. Thus, the thesis presents the derivation of missile 6DOF model augmented by a more realistic homing head. The design and analysis is carried out with the linearized models at pre-specified flight conditions

Issued also as CD

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