| 000 | 01686nam a2200349 a 4500 | ||
|---|---|---|---|
| 003 | EG-GiCUC | ||
| 005 | 20250223025916.0 | ||
| 008 | 090815s2009 ua eh 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 | _aCai01.13.07.M.Sc.2009.Em.D | ||
| 100 | 0 | _aEmad Mahros Rabee Mohammed | |
| 245 | 1 | 0 |
_aDesign of a real time control system for missiles guidance / _cEmad Mahros Rabee Mohammed ; Supervised Hassen Taher Dorrah , Gamal Mahmoud Sayd |
| 246 | 1 | 5 | _aتصميم نظام تحكم فى الزمن الحقيقى لتوجيه الصواريخ |
| 260 |
_aCairo : _bEmad Mahros Rabee Mohammed , _c2009 |
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| 300 |
_a130 Leaves : _bfacsimiles , plans ; _c30cm |
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| 502 | _aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Electrical Power and Machines | ||
| 520 | _aThe objective of this thesis is to investigate and enhance the system performance of a homing guided missile via synthesizing its homing head using proposed classical and advanced control techniques. Thus, the thesis presents the derivation of missile 6DOF model augmented by a more realistic homing head. The design and analysis is carried out with the linearized models at pre-specified flight conditions | ||
| 530 | _aIssued also as CD | ||
| 653 | 4 | _aAerodynamic characteristies | |
| 653 | 4 | _aFuzzy logic base | |
| 653 | 4 | _aSeeker homing head | |
| 700 | 0 |
_aGamal Mahmoud Sayd , _eSupervisor |
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| 700 | 0 |
_aHassen Taher Dorrah , _eSupervisor |
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| 856 | _uhttp://172.23.153.220/th.pdf | ||
| 902 | _a1 | ||
| 905 |
_aMustafa _eRevisor |
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| 905 |
_aSamia _eCataloger |
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| 942 |
_2ddc _cTH |
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| 999 |
_c23318 _d23318 |
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