| 000 | 017600000a22003490004500 | ||
|---|---|---|---|
| 003 | EG-GICUC | ||
| 005 | 20250223025509.0 | ||
| 008 | 081025s2008 ua d f m 000 0 eng d | ||
| 040 |
_aEG-GICUC _beng _cEG-GICUC |
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| 041 | 0 | _aEng | |
| 049 | _aDeposite | ||
| 097 | _aM.Sc | ||
| 099 | _aCai01.13.01.M.Sc.2008.Ha.A | ||
| 100 | 0 | _aHaithem Ezzat Mohammed Taha | |
| 245 | 1 | 0 |
_aAircraft guidance along a prescribed trajectory using inverse simulation and model reference adaptive control / _cHaithem Ezzat Mohammed Taha ; Supervised Sayed Desouky Hassan , Gamal Mahmoud Elbayoumi , Mohammed Sayed Bayoumi |
| 246 | 1 | 5 | _aتوجيه الطائرات على مسار محدد باستخدام المحاكاه العكسية والتحكم المتضابط |
| 260 |
_aCairo : _bHaithem Ezzat Mohammed Taha , _c2008 |
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| 300 |
_a113P. : _bcharts ; _c30cm |
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| 502 | _aThesis (M.Sc.) - Cairo University - Faculty Of Engineering - Department Of Aerospace Engineering | ||
| 520 | _aThe 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 | ||
| 530 | _aIssued also as CD | ||
| 653 | 4 | _aAdaptive control | |
| 653 | 4 | _aAutopilot | |
| 653 | 4 | _aGuidance | |
| 700 | 0 |
_aGamal Mahmoud Elbayoumi , _eSupervisor |
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| 700 | 0 |
_aMohammed Sayed Bayoumi , _eSupervisor |
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| 700 | 0 |
_aSayed Desouky Hassan , _eSupervisor |
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| 856 | _uhttp://172.23.153.220/th.pdf | ||
| 905 |
_aNazla _eRevisor |
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| 905 |
_aSoheir _eCataloger |
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| 942 |
_2ddc _cTH |
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| 999 |
_c14295 _d14295 |
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