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https://hdl.handle.net/2445/191494Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.advisor | Gómez Muntané, Gerardo | - |
| dc.contributor.author | Martin Graells, Eduard | - |
| dc.date.accessioned | 2022-12-13T09:43:03Z | - |
| dc.date.available | 2022-12-13T09:43:03Z | - |
| dc.date.issued | 2022-06-13 | - |
| dc.identifier.uri | https://hdl.handle.net/2445/191494 | - |
| dc.description | Treballs Finals de Grau d'Enginyeria Informàtica, Facultat de Matemàtiques, Universitat de Barcelona, Any: 2022, Director: Gerardo Gómez Muntané | ca |
| dc.description.abstract | [en] In the modern world, artificial satellites orbiting around the Earth are used in a wide variety of areas. The tracking and modeling of their orbits is of utmost importance. In the following text, a mathematical framework for their study as well as a software implementation and the use of a software suite, GMAT, are presented. | ca |
| dc.format.extent | 58 p. | - |
| dc.format.mimetype | application/pdf | - |
| dc.language.iso | eng | ca |
| dc.rights | memòria: cc-nc-nd (c) Eduard Martin Graells, 2022 | - |
| dc.rights | codi: GPL (c) Eduard Martin Graells, 2022 | - |
| dc.rights.uri | http://www.gnu.org/licenses/gpl-3.0.ca.html | - |
| dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/3.0/es/ | * |
| dc.source | Treballs Finals de Grau (TFG) - Enginyeria Informàtica | - |
| dc.subject.classification | Mecànica orbital | ca |
| dc.subject.classification | Òrbites | ca |
| dc.subject.classification | Programari | ca |
| dc.subject.classification | Treballs de fi de grau | ca |
| dc.subject.classification | Sistemes dinàmics diferenciables | ca |
| dc.subject.classification | Satèl·lits artificials | ca |
| dc.subject.other | Orbital mechanics | en |
| dc.subject.other | Orbits | en |
| dc.subject.other | Computer software | en |
| dc.subject.other | Differentiable dynamical systems | en |
| dc.subject.other | Artificial satellites | en |
| dc.subject.other | Bachelor's theses | en |
| dc.title | Moviment d’un satèl·lit artificial en presència de frenat atmosfèric | ca |
| dc.type | info:eu-repo/semantics/bachelorThesis | ca |
| dc.rights.accessRights | info:eu-repo/semantics/openAccess | ca |
| Appears in Collections: | Programari - Treballs de l'alumnat Treballs Finals de Grau (TFG) - Matemàtiques Treballs Finals de Grau (TFG) - Enginyeria Informàtica | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| tfg_martin_graells_eduard.pdf | Memòria | 1.1 MB | Adobe PDF | View/Open |
| codi.zip | Codi font | 229.03 kB | zip | View/Open |
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