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Helicopter flight trim, stability and control / Ahmed Aboulftouh Mohamed Ahmed ; Supervised Mohamed Madbouli Abdelrahman , Gamal Mahmoud Sayed Elbayoumi

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Ahmed Aboulftouh Mohamed Ahmed , 2015Description: 149 P. ; 30cmOther title:
  • الإتزان و الإستقرار و التحكم فى طائرة مروحية [Added title page title]
Subject(s): Online resources: Available additional physical forms:
  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: This 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
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Item type Current library Home library Call number Copy number Status Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2015.Ah.H (Browse shelf(Opens below)) Not for loan 01010110067855000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.M.Sc.2015.Ah.H (Browse shelf(Opens below)) 67855.CD Not for loan 01020110067855000

Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

This 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

Issued also as CD

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