An experimental model of small satellite motion in two dimensions using gimbaled structure and two reaction wheels / Sherif Hassan Mohamed Hassan ; Supervised Mohamed B. Argoun , Gamal M. Elbayoumi

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Sherif Hassan Mohamed Hassan

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Material type: Text

TextLanguage: English Publication details: Cairo : Sherif Hassan Mohamed Hassan , 2016Description: 97P. : charts , facsimiles ; 30cmOther title:

نموذج تجريبى لحركة قمر صناعى مصغر فى بعدين بإستخدام هيكل إطارى وعجلتى عزوم [Added title page title]

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Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: The objective of this work is to build a demonstration model of satellite motion control. The testbed assembly consists of a two axes gimbaled structure with mounted satellite model and two reaction wheels which are used for motion control. The objective of the testbed is to enable, examining and testing of preliminary satellite control algorithms. The purpose of the work is to tackle and discuss the technological issues involved in building such a device in a university lab environment. The work is supplemented by simulation of the testbed motion and comparing the results with results obtained from the experimental testbed

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Item type	Current library	Home library	Call number	Copy number	Status	Date due	Barcode
Thesis	قاعة الرسائل الجامعية - الدور الاول	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.01.M.Sc.2016.Sh.E (Browse shelf(Opens below))		Not for loan		01010110070442000
CD - Rom	مخـــزن الرســائل الجـــامعية - البدروم	المكتبة المركزبة الجديدة - جامعة القاهرة	Cai01.13.01.M.Sc.2016.Sh.E (Browse shelf(Opens below))	70442.CD	Not for loan		01020110070442000

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

The objective of this work is to build a demonstration model of satellite motion control. The testbed assembly consists of a two axes gimbaled structure with mounted satellite model and two reaction wheels which are used for motion control. The objective of the testbed is to enable, examining and testing of preliminary satellite control algorithms. The purpose of the work is to tackle and discuss the technological issues involved in building such a device in a university lab environment. The work is supplemented by simulation of the testbed motion and comparing the results with results obtained from the experimental testbed

Issued also as CD

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