Formation dynamics in geostationary ring
A relative motion model for a satellite formation composed of two Earth-orbiting spacecraft located in the geostationary ring is developed taking into account major gravitational and non-gravitational forces. A previously existing model featuring perturbation due to J 2 is enhanced by the perturbati...
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| Veröffentlicht in: | Celestial mechanics and dynamical astronomy 2016-08, Vol.125 (4), p.485-500 |
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| container_title | Celestial mechanics and dynamical astronomy |
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| creator | Spiridonova, Sofya |
| description | A relative motion model for a satellite formation composed of two Earth-orbiting spacecraft located in the geostationary ring is developed taking into account major gravitational and non-gravitational forces. A previously existing model featuring perturbation due to
J
2
is enhanced by the perturbations due to solar radiation pressure arising from unequal area-to-mass ratios, as well as the secular and long-periodic gravitational perturbations due to the Sun and the Moon. The extended relative motion model is validated using several typical formation geometries against a reference generated by numerical integration of the absolute orbits of the two spacecraft. The results of this work can find application in future on-orbit servicing and formation flying missions in near-geostationary orbit. |
| doi_str_mv | 10.1007/s10569-016-9693-0 |
| format | Article |
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J
2
is enhanced by the perturbations due to solar radiation pressure arising from unequal area-to-mass ratios, as well as the secular and long-periodic gravitational perturbations due to the Sun and the Moon. The extended relative motion model is validated using several typical formation geometries against a reference generated by numerical integration of the absolute orbits of the two spacecraft. The results of this work can find application in future on-orbit servicing and formation flying missions in near-geostationary orbit.</description><identifier>ISSN: 0923-2958</identifier><identifier>EISSN: 1572-9478</identifier><identifier>DOI: 10.1007/s10569-016-9693-0</identifier><language>eng</language><publisher>Dordrecht: Springer Netherlands</publisher><subject>Aerospace Technology and Astronautics ; Astrophysics and Astroparticles ; Classical Mechanics ; Dynamical Systems and Ergodic Theory ; Formations ; Geophysics/Geodesy ; Geostatistics ; Gravitation ; Mathematical models ; Missions ; Orbits ; Original Article ; Perturbation methods ; Physics ; Physics and Astronomy ; Solar radiation ; Space environment ; Spacecraft ; Star & galaxy formation ; Time & motion studies</subject><ispartof>Celestial mechanics and dynamical astronomy, 2016-08, Vol.125 (4), p.485-500</ispartof><rights>Springer Science+Business Media Dordrecht 2016</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c382t-513a251b551b336879fb523a76d401005516bc9feffddcd2395a69db5c4d78153</citedby><cites>FETCH-LOGICAL-c382t-513a251b551b336879fb523a76d401005516bc9feffddcd2395a69db5c4d78153</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s10569-016-9693-0$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s10569-016-9693-0$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,41488,42557,51319</link.rule.ids></links><search><creatorcontrib>Spiridonova, Sofya</creatorcontrib><title>Formation dynamics in geostationary ring</title><title>Celestial mechanics and dynamical astronomy</title><addtitle>Celest Mech Dyn Astr</addtitle><description>A relative motion model for a satellite formation composed of two Earth-orbiting spacecraft located in the geostationary ring is developed taking into account major gravitational and non-gravitational forces. A previously existing model featuring perturbation due to
J
2
is enhanced by the perturbations due to solar radiation pressure arising from unequal area-to-mass ratios, as well as the secular and long-periodic gravitational perturbations due to the Sun and the Moon. The extended relative motion model is validated using several typical formation geometries against a reference generated by numerical integration of the absolute orbits of the two spacecraft. 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J
2
is enhanced by the perturbations due to solar radiation pressure arising from unequal area-to-mass ratios, as well as the secular and long-periodic gravitational perturbations due to the Sun and the Moon. The extended relative motion model is validated using several typical formation geometries against a reference generated by numerical integration of the absolute orbits of the two spacecraft. The results of this work can find application in future on-orbit servicing and formation flying missions in near-geostationary orbit.</abstract><cop>Dordrecht</cop><pub>Springer Netherlands</pub><doi>10.1007/s10569-016-9693-0</doi><tpages>16</tpages></addata></record> |
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| ispartof | Celestial mechanics and dynamical astronomy, 2016-08, Vol.125 (4), p.485-500 |
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| language | eng |
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| subjects | Aerospace Technology and Astronautics Astrophysics and Astroparticles Classical Mechanics Dynamical Systems and Ergodic Theory Formations Geophysics/Geodesy Geostatistics Gravitation Mathematical models Missions Orbits Original Article Perturbation methods Physics Physics and Astronomy Solar radiation Space environment Spacecraft Star & galaxy formation Time & motion studies |
| title | Formation dynamics in geostationary ring |
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