Hamiltonian perturbation solutions for spacecraft orbit prediction: the method of lie transforms
Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems ar...
Gespeichert in:
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| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Berlin ; Boston
De Gruyter
[2021]
|
| Schriftenreihe: | De Gruyter Studies in Mathematical Physics
54 |
| Schlagworte: | |
| Online-Zugang: | FAB01 FAW01 FCO01 FHA01 FKE01 FLA01 UBR01 UPA01 URL des Erstveröffentlichers |
| Zusammenfassung: | Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations |
| Beschreibung: | Description based on online resource; title from PDF title page (publisher's Web site, viewed 26. Mai 2021) |
| Beschreibung: | 1 Online-Ressource (XVI, 378 Seiten) |
| ISBN: | 9783110668513 |
| DOI: | 10.1515/9783110668513 |
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| spelling | Lara, Martín Verfasser aut Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms Martín Lara Berlin ; Boston De Gruyter [2021] © 2021 1 Online-Ressource (XVI, 378 Seiten) txt rdacontent c rdamedia cr rdacarrier De Gruyter Studies in Mathematical Physics 54 Description based on online resource; title from PDF title page (publisher's Web site, viewed 26. Mai 2021) Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations In English Hamilton-Jacobi-Differentialgleichung Störungstheorie Umlaufbahn SCIENCE / Space Science bisacsh Erscheint auch als Druck-Ausgabe 9783110667226 https://doi.org/10.1515/9783110668513 Verlag URL des Erstveröffentlichers Volltext |
| spellingShingle | Lara, Martín Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms Hamilton-Jacobi-Differentialgleichung Störungstheorie Umlaufbahn SCIENCE / Space Science bisacsh |
| title | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms |
| title_auth | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms |
| title_exact_search | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms |
| title_exact_search_txtP | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms |
| title_full | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms Martín Lara |
| title_fullStr | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms Martín Lara |
| title_full_unstemmed | Hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms Martín Lara |
| title_short | Hamiltonian perturbation solutions for spacecraft orbit prediction |
| title_sort | hamiltonian perturbation solutions for spacecraft orbit prediction the method of lie transforms |
| title_sub | the method of lie transforms |
| topic | Hamilton-Jacobi-Differentialgleichung Störungstheorie Umlaufbahn SCIENCE / Space Science bisacsh |
| topic_facet | Hamilton-Jacobi-Differentialgleichung Störungstheorie Umlaufbahn SCIENCE / Space Science |
| url | https://doi.org/10.1515/9783110668513 |
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