Dynamic modeling, guidance, and control of homing missile / by Hassan Ramadan Hassan Ali Elzahar ; Supervisors: Prof. Dr. Gamal Mahmoud Sayed El-Bayoumi, Prof. Osama Saeed Mohammadi Abdel Razek.
Material type:
TextLanguage: English Summary language: English, Arabic Producer: 2025Description: 130 pages : illustrations ; 30 cm. + CDContent type: - text
- Unmediated
- volume
- النمذجة الديناميكية و التوجية و التحكم للصواريخ ذاتية التوجية [Added title page title]
- 629
- Issues also as CD.
| Item type | Current library | Home library | Call number | Status | Barcode | |
|---|---|---|---|---|---|---|
Thesis
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قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2025.Ha.D (Browse shelf(Opens below)) | Not for loan | 01010110093374000 |
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| Cai01.13.01.M.Sc.2024.Mo.G Ground and wall effects on a hovering flapping airfoil / | Cai01.13.01.M.Sc.2025.Ah.O Obstacle avoidance algorithms analysis and implementation for quadcopter platform using indoor positioning system / | Cai01.13.01.M.Sc.2025.Am.N Numerical aerodynamic investigation of hovering insect at low reynolds number / Remainder of title / | Cai01.13.01.M.Sc.2025.Ha.D Dynamic modeling, guidance, and control of homing missile / | Cai01.13.01.M.Sc.2025.Ma.D Development of a thermal control system for earth observation 6U cubesat / | Cai01.13.01.Ph.D.1995.Mo.A Analytical Approach to turbofan engine modeling control and non -linear simulation / | Cai01.13.01.Ph.D.1995.Mo.A Aircraft acquisition and operation in a total quality environment / |
Thesis (M.Sc)-Cairo University, 2025.
Bibliography: pages 118 -121.
Homing missiles have transformed modern warfare by enabling precise and
autonomous targeting capabilities. However, the effectiveness of a homing missile system
relies heavily on its guidance law, autopilot control mechanisms, and tracking or seeker
technology. This thesis address that facts by modeling a complete homing missile system
with six degrees of freedom (6-DOF), utilizing tail control mechanism and an electro-
optical (EO) tracking device to target an aircraft from the ground. A 2D camera-based
image guidance system tracks the target and estimates its motion orientation using
developed algorithms that interacting with mathematical models of the target and EO
camera to captures the target’s 3D movement from its image plane coordinates. The study
simulations conducted in MATLAB® and Simulink® to demonstrate successful missile-
target engagements with both Pure Pursuit Guidance (PPG) and Proportional Navigation
Guidance (PNG) laws to compare the performance of for each law in multiple engagement
scenarios.
تعتمد فعالية أنظمة الصواريخ الموجهة بشكل كبير على قانون التوجيه، وآليات التحكم في الطيار الآلي، وتقنية التتبع أو الباحث. تتناول هذه الرسالة هذه الحقائق من خلال نمذجة نظام صاروخ موجه كامل بست درجات حرية، باستخدام وحدة تحكم ذيلية مع جهاز تتبع EO لاستهداف طائرة. يتتبع الهدف نظام توجيه صوري ثنائي الأبعاد قائم على كاميرا، ويقدر اتجاه حركته باستخدام خوارزميات مطورة لالتقاط حركة الهدف ثلاثية الأبعاد من إحداثيات مستوى صورته. أجريت عمليات المحاكاة في الدراسة باستخدام MATLAB® وSimulink®. ثم قورنت نتائج قوانين PPG وPNG من منظور الأداء.
Issues also as CD.
Text in English and abstract in Arabic & English.
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