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Orbit selection for optical and radar remote sensing satellite / Mohamed Sayed Ahmed Elzanaty ; Supervised Mervat Elsayd Awad , Elamira Hend Said Khattab , Mohammad Ahmad Fouad Ali Basha

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Mohamed Sayed Ahmed Elzanaty , 2019Description: 117 P. : charts , facsimiles ; 25cmOther title:
  • الاختيار الامثل لمدارات الاقمار الصناعية الكهروبصرية والرادارية للاستشعار عن بعد [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (M.Sc.) - Cairo University - Faculty of Science - Department of Astronomy and Meteorology Summary: This thesis aimed to determine and select the best choice of orbits for low earth orbit satellite.The orbit selection procedures are very essential and complex, concerning swap between a numbers of various parameters where the designer picks the best orbital parameters to meet the mission requirements. The orbit typically defines the space mission lifetime, cost, environment, communication links, coverage, availability of launch vehicle, and the payload performance. The numerical and mathematical models are expressed to compute the satellite{u2019}s orbit by MATLAB software under the gravitational second zonal harmonic effect
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Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.12.01.M.Sc.2019.Mo.O (Browse shelf(Opens below)) Not for loan 01010110080455000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.12.01.M.Sc.2019.Mo.O (Browse shelf(Opens below)) 80455.CD Not for loan 01020110080455000

Thesis (M.Sc.) - Cairo University - Faculty of Science - Department of Astronomy and Meteorology

This thesis aimed to determine and select the best choice of orbits for low earth orbit satellite.The orbit selection procedures are very essential and complex, concerning swap between a numbers of various parameters where the designer picks the best orbital parameters to meet the mission requirements. The orbit typically defines the space mission lifetime, cost, environment, communication links, coverage, availability of launch vehicle, and the payload performance. The numerical and mathematical models are expressed to compute the satellite{u2019}s orbit by MATLAB software under the gravitational second zonal harmonic effect

Issued also as CD

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