ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS
: In this paper the drag perturbation for the law orbit are studded ,Koll-method is suitable to used hear, equation of motion it's solved by numerical integration ;Rang-Kota-method was used ; to find the components of velocity and position and find the orbital parameters with perturbation .Stud...
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| Format: | Article |
| Language: | English |
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University of Anbar
2012-06-01
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| Series: | مجلة جامعة الانبار للعلوم الصرفة |
| Subjects: | |
| Online Access: | https://juaps.uoanbar.edu.iq/article_15315_384280dbc6950738d9c09696d3dbf66b.pdf |
| _version_ | 1827396411308638208 |
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| author | Abdulh Rahman Hussain Salih |
| author_facet | Abdulh Rahman Hussain Salih |
| author_sort | Abdulh Rahman Hussain Salih |
| collection | DOAJ |
| description | : In this paper the drag perturbation for the law orbit are studded ,Koll-method is suitable to used hear, equation of motion it's solved by numerical integration ;Rang-Kota-method was used ; to find the components of velocity and position and find the orbital parameters with perturbation .Study the effect of drag perturbation on the position , of satellite with time and on perigee , apogee , a ,e and age of satellite, Study the variation of satellite position and age with height we can increase the age of satellite to 40 times by increase the perigee height only 2 times, and by decrease A/m ratio and eccentricity also by rotate in the direction of the earth rotate. |
| first_indexed | 2024-03-08T18:50:35Z |
| format | Article |
| id | doaj.art-fb1609d490b24e15931a5cbf6647528a |
| institution | Directory Open Access Journal |
| issn | 1991-8941 2706-6703 |
| language | English |
| last_indexed | 2024-03-08T18:50:35Z |
| publishDate | 2012-06-01 |
| publisher | University of Anbar |
| record_format | Article |
| series | مجلة جامعة الانبار للعلوم الصرفة |
| spelling | doaj.art-fb1609d490b24e15931a5cbf6647528a2023-12-28T21:52:41ZengUniversity of Anbarمجلة جامعة الانبار للعلوم الصرفة1991-89412706-67032012-06-0122627210.37652/juaps.2008.1531515315ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITSAbdulh Rahman Hussain Salih0Sciences of college/ University of Baghdad: In this paper the drag perturbation for the law orbit are studded ,Koll-method is suitable to used hear, equation of motion it's solved by numerical integration ;Rang-Kota-method was used ; to find the components of velocity and position and find the orbital parameters with perturbation .Study the effect of drag perturbation on the position , of satellite with time and on perigee , apogee , a ,e and age of satellite, Study the variation of satellite position and age with height we can increase the age of satellite to 40 times by increase the perigee height only 2 times, and by decrease A/m ratio and eccentricity also by rotate in the direction of the earth rotate.https://juaps.uoanbar.edu.iq/article_15315_384280dbc6950738d9c09696d3dbf66b.pdfatmosphericdrag perturbationsatellites orbits |
| spellingShingle | Abdulh Rahman Hussain Salih ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS مجلة جامعة الانبار للعلوم الصرفة atmospheric drag perturbation satellites orbits |
| title | ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS |
| title_full | ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS |
| title_fullStr | ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS |
| title_full_unstemmed | ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS |
| title_short | ATMOSPHERIC DRAG PERTURBATION EFFECT ON THE SATELLITES ORBITS |
| title_sort | atmospheric drag perturbation effect on the satellites orbits |
| topic | atmospheric drag perturbation satellites orbits |
| url | https://juaps.uoanbar.edu.iq/article_15315_384280dbc6950738d9c09696d3dbf66b.pdf |
| work_keys_str_mv | AT abdulhrahmanhussainsalih atmosphericdragperturbationeffectonthesatellitesorbits |