Please use this identifier to cite or link to this item:
http://148.72.244.84/xmlui/handle/xmlui/9992Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Mohammed S. Rasheed | - |
| dc.date.accessioned | 2023-11-23T07:26:01Z | - |
| dc.date.available | 2023-11-23T07:26:01Z | - |
| dc.date.issued | 2013-10-01 | - |
| dc.identifier.issn | 2222-8373 | - |
| dc.identifier.uri | http://148.72.244.84:8080/xmlui/handle/xmlui/9992 | - |
| dc.description.abstract | in this paper, the two body problem equation in parabolic orbit in celestial mechanics is solved using new iterative method with quadratic convergence. Initial solution is suggested depending on the time , earth gravitational constant and the angular distance to be , . The proposed methods considerably to be improvement of Newton's method with less iteration are needed to reach the solution of two body problem in parabolic orbit. | en_US |
| dc.description.sponsorship | djps.uodiyala.edu.iq/pages?id=52 | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | university of Diyala | en_US |
| dc.subject | Parabolic orbit, Barker's formula, Two body problem, Iterative methods, Order of convergence, Astrophysics. | en_US |
| dc.title | Solve the Position to Time Equation for an Object Travelling on a Parabolic Orbit in Celestial Mechanics | en_US |
| dc.type | Article | en_US |
| Appears in Collections: | مجلة ديالى للعلوم الاكاديمية / Academic Science Journal (Acad. Sci. J.) | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 37-47 E.pdf | 549.1 kB | Adobe PDF | View/Open |
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