Attitude analysis of a rigid spacecraft / Hani Mahmoud Mohammed ; Supervised M. K. M. Ahmed , Ashraf H. Owis , Yehia A. Abdelaziz
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TextLanguage: English Publication details: Cairo : Hani Mahmoud Mohammed , 2012Description: 195 P. ; 25cmOther title: - تحليل الهيئة لمركبة فضائية جاسئة [Added title page title]
- Issued also as CD
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Thesis
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قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.12.01.M.Sc.2012.Ha.A (Browse shelf(Opens below)) | Not for loan | 01010110058257000 | ||
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مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.12.01.M.Sc.2012.Ha.A (Browse shelf(Opens below)) | 58257.CD | Not for loan | 01020110058257000 |
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Thesis (M.Sc.) - Cairo University - Faculty of Science - Department of Astronomy and Meteorology
The present work deals with the attitude motion of an artificial satellite, that is symmetrical about one axes, with the earth considered oblate, under the effects of gravitational and lorentz force torques. The problem is treated in the Hamiltonian framework by defining potential like functions the negative gradient of which yield the torques. The orbital and attitude term are expressed in terms of the delaunay and andoyer variables, respectively
Issued also as CD
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