Applied nonsingular astrodynamics optimal low-thrust orbit transfer:
This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research...
Gespeichert in:
| Beteilige Person: | |
|---|---|
| Format: | E-Book |
| Sprache: | Englisch |
| Veröffentlicht: |
Cambridge
Cambridge University Press
2018
|
| Schriftenreihe: | Cambridge aerospace series
45 |
| Links: | https://doi.org/10.1017/9781108560061 |
| Zusammenfassung: | This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses. |
| Umfang: | 1 Online-Ressource (xvii, 461 Seiten) |
| ISBN: | 9781108560061 |
Internformat
MARC
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Datensatz im Suchindex
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| id | ZDB-20-CTM-CR9781108560061 |
| illustrated | Not Illustrated |
| indexdate | 2025-01-17T11:17:12Z |
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| isbn | 9781108560061 |
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| spelling | Kéchichian, Jean Albert 1945- Applied nonsingular astrodynamics optimal low-thrust orbit transfer Jean Albert Kéchichian (The Aerospace Corporation (retired)) Cambridge Cambridge University Press 2018 1 Online-Ressource (xvii, 461 Seiten) txt c cr Cambridge aerospace series 45 This essential book describes the mathematical formulations and subsequent computer simulations required to accurately project the trajectory of spacecraft and rockets in space, using the formalism of optimal control for minimum-time transfer in general elliptic orbit. The material will aid research students in aerospace engineering, as well as practitioners in the field of spaceflight dynamics, in developing simulation software to carry out trade studies useful in vehicle and mission design. It will teach readers to develop flight software for operational applications in autonomous mode, so to actually transfer space vehicles from one orbit to another. The practical, real-life applications discussed will give readers a clear understanding of the mathematics of orbit transfer, allow them to develop their own operational software to fly missions, and to use the contents as a research tool to carry out even more complex analyses. Erscheint auch als Druck-Ausgabe 9781108472364 |
| spellingShingle | Kéchichian, Jean Albert 1945- Applied nonsingular astrodynamics optimal low-thrust orbit transfer |
| title | Applied nonsingular astrodynamics optimal low-thrust orbit transfer |
| title_auth | Applied nonsingular astrodynamics optimal low-thrust orbit transfer |
| title_exact_search | Applied nonsingular astrodynamics optimal low-thrust orbit transfer |
| title_full | Applied nonsingular astrodynamics optimal low-thrust orbit transfer Jean Albert Kéchichian (The Aerospace Corporation (retired)) |
| title_fullStr | Applied nonsingular astrodynamics optimal low-thrust orbit transfer Jean Albert Kéchichian (The Aerospace Corporation (retired)) |
| title_full_unstemmed | Applied nonsingular astrodynamics optimal low-thrust orbit transfer Jean Albert Kéchichian (The Aerospace Corporation (retired)) |
| title_short | Applied nonsingular astrodynamics optimal low-thrust orbit transfer |
| title_sort | applied nonsingular astrodynamics optimal low thrust orbit transfer |
| work_keys_str_mv | AT kechichianjeanalbert appliednonsingularastrodynamicsoptimallowthrustorbittransfer |