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Aircraft guidance along a prescribed trajectory using inverse simulation and model reference adaptive control / Haithem Ezzat Mohammed Taha ; Supervised Sayed Desouky Hassan , Gamal Mahmoud Elbayoumi , Mohammed Sayed Bayoumi

By: Contributor(s): Language: Eng Publication details: Cairo : Haithem Ezzat Mohammed Taha , 2008Description: 113P. : charts ; 30cmOther title:
  • توجيه الطائرات على مسار محدد باستخدام المحاكاه العكسية والتحكم المتضابط [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 aim of this work is to fly an unmanned aircraft vehicle (UAV) on certain traiectory two methodologies are presented for such function the first one is the inverse dynamics methodology which is an inverse solution for the aircraft (a / c) differential equations of motion knowing the desired trajectory to get the a / c controllers needed to fulfill this trajectory
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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 Cai01.13.01.M.Sc.2008.Ha.A (Browse shelf(Opens below)) Not for loan 01010110050014000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2008.Ha.A (Browse shelf(Opens below)) 50014.CD Not for loan 01020110050014000

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

The aim of this work is to fly an unmanned aircraft vehicle (UAV) on certain traiectory two methodologies are presented for such function the first one is the inverse dynamics methodology which is an inverse solution for the aircraft (a / c) differential equations of motion knowing the desired trajectory to get the a / c controllers needed to fulfill this trajectory

Issued also as CD

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