TY  - GEN
AU  - Haithem Ezzat Mohammed Taha
AU  - Gamal Mahmoud Elbayoumi , 
AU  - Mohammed Sayed Bayoumi , 
AU  - Sayed Desouky Hassan , 
TI  - Aircraft guidance along a prescribed trajectory using inverse simulation and model reference adaptive control / 
PY  - 2008///
CY  - Cairo : 
PB  - Haithem Ezzat Mohammed Taha , 
KW  - Adaptive control
KW  - Autopilot
KW  - Guidance
N1  - Thesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Aerospace Engineering; Issued also as CD
N2  - 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
UR  - http://172.23.153.220/th.pdf
ER  -