Haithem Ezzat Mohammed Taha <br/><br/>
Aircraft guidance along a prescribed trajectory using inverse simulation and model reference adaptive control /  
 توجيه الطائرات على مسار محدد باستخدام المحاكاه العكسية والتحكم المتضابط 
Haithem Ezzat Mohammed Taha ; Supervised Sayed Desouky Hassan , Gamal Mahmoud Elbayoumi , Mohammed Sayed Bayoumi 
 - Cairo :   Haithem Ezzat Mohammed Taha ,   2008 
 - 113P. :   charts ;   30cm 
<br/><br/>Thesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Aerospace Engineering 
<br/><br/> 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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<br/><br/><label>Subjects--Index Terms: </label>Adaptive control Autopilot Guidance