An implementation and verification of a high-precision orbit propagator / Ahmed Mohamed Ismail Atallah ; Supervised Tamer Mekky Ahmed , Atef O. Sherif
Material type: TextLanguage: English Publication details: Cairo : Ahmed Mohamed Ismail Atallah , 2018Description: 125 P. : charts , facsimiles ; 30cmOther title:- تنفيذ و تحقيق محاكى مدار عالى الدقة [Added title page title]
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Item type | Current library | Home library | Call number | Copy number | Status | Date due | Barcode | |
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Thesis | قاعة الرسائل الجامعية - الدور الاول | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2018.Ah.I (Browse shelf(Opens below)) | Not for loan | 01010110076445000 | |||
CD - Rom | مخـــزن الرســائل الجـــامعية - البدروم | المكتبة المركزبة الجديدة - جامعة القاهرة | Cai01.13.01.M.Sc.2018.Ah.I (Browse shelf(Opens below)) | 76445.CD | Not for loan | 01020110076445000 |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
This work aims to implement a high-precision orbit propagator. The basic propagator modules are the force models, numerical integrator, time systems, and coordinate systems.The force models include: the geopotential, drag, third-body, solar radiation pressure, solid Earth tides, and Earth radiation pressure. The DOPPRI8 method was used to integrate the resulting set of equations.The implemented propagator demonstrated millimeter level of positional difference with industry standard propagators for conservative forces and matches to the meter-level when nonconservative forces are considered
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