000 01523cam a2200337 a 4500
003 EG-GiCUC
005 20250223031420.0
008 160201s2015 ua f m 000 0 eng d
040 _aEG-GiCUC
_beng
_cEG-GiCUC
041 0 _aeng
049 _aDeposite
097 _aM.Sc
099 _aCai01.13.01.M.Sc.2015.Ah.H
100 0 _aAhmed Aboulftouh Mohamed Ahmed
245 1 0 _aHelicopter flight trim, stability and control /
_cAhmed Aboulftouh Mohamed Ahmed ; Supervised Mohamed Madbouli Abdelrahman , Gamal Mahmoud Sayed Elbayoumi
246 1 5 _aالإتزان و الإستقرار و التحكم فى طائرة مروحية
260 _aCairo :
_bAhmed Aboulftouh Mohamed Ahmed ,
_c2015
300 _a149 P. ;
_c30cm
502 _aThesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 _aThis thesis describes the development of helicopter trim, stability and control analysis. The thesis is divided into two main parts. The first part is the solution of the helicopter trim problem. The second part of this thesis is the application of the optimal control theory to the full scale helicopter
530 _aIssued also as CD
653 4 _aHelicopter
653 4 _aOptimal control
653 4 _aTrim
700 0 _aGamal Mahmoud Sayed Elbayoumi ,
_eSupervisor
700 0 _aMohamed Madbouli Abdelrahman ,
_eSupervisor
856 _uhttp://172.23.153.220/th.pdf
905 _aNazla
_eRevisor
905 _aSamia
_eCataloger
942 _2ddc
_cTH
999 _c54834
_d54834