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:
| 1. Verfasser: | |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
Cambridge
Cambridge University Press
2018
|
| Schriftenreihe: | Cambridge aerospace series
45 |
| Schlagworte: | |
| Online-Zugang: | BSB01 FHN01 UBA01 Volltext |
| 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 |
| Beschreibung: | Title from publisher's bibliographic system (viewed on 31 Aug 2018) |
| Beschreibung: | 1 Online-Ressource (xvii, 461 Seiten) |
| ISBN: | 9781108560061 |
| DOI: | 10.1017/9781108560061 |
Internformat
MARC
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| 245 | 1 | 0 | |a Applied nonsingular astrodynamics |b optimal low-thrust orbit transfer |c Jean Albert Kéchichian (The Aerospace Corporation (retired)) |
| 264 | 1 | |a Cambridge |b Cambridge University Press |c 2018 | |
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| 490 | 0 | |a Cambridge aerospace series |v 45 | |
| 500 | |a Title from publisher's bibliographic system (viewed on 31 Aug 2018) | ||
| 520 | |a 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 | ||
| 650 | 4 | |a Orbital transfer (Space flight) | |
| 650 | 4 | |a Trajectory optimization | |
| 650 | 4 | |a Space trajectories | |
| 650 | 0 | 7 | |a Astrodynamik |0 (DE-588)4143246-0 |2 gnd |9 rswk-swf |
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Datensatz im Suchindex
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| any_adam_object | |
| author | Kéchichian, Jean Albert 1945- |
| author_GND | (DE-588)1169456901 |
| author_facet | Kéchichian, Jean Albert 1945- |
| author_role | aut |
| author_sort | Kéchichian, Jean Albert 1945- |
| author_variant | j a k ja jak |
| building | Verbundindex |
| bvnumber | BV045242660 |
| classification_rvk | ZO 8000 |
| collection | ZDB-20-CBO |
| ctrlnum | (ZDB-20-CBO)CR9781108560061 (OCoLC)1057789912 (DE-599)BVBBV045242660 |
| dewey-full | 629.4/113 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.4/113 |
| dewey-search | 629.4/113 |
| dewey-sort | 3629.4 3113 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| doi_str_mv | 10.1017/9781108560061 |
| format | Electronic eBook |
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| id | DE-604.BV045242660 |
| illustrated | Not Illustrated |
| indexdate | 2024-07-10T08:12:35Z |
| institution | BVB |
| isbn | 9781108560061 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-030630836 |
| oclc_num | 1057789912 |
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| owner_facet | DE-12 DE-92 DE-384 |
| physical | 1 Online-Ressource (xvii, 461 Seiten) |
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| publishDate | 2018 |
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| publisher | Cambridge University Press |
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| spelling | Kéchichian, Jean Albert 1945- Verfasser (DE-588)1169456901 aut 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 rdacontent c rdamedia cr rdacarrier Cambridge aerospace series 45 Title from publisher's bibliographic system (viewed on 31 Aug 2018) 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 Orbital transfer (Space flight) Trajectory optimization Space trajectories Astrodynamik (DE-588)4143246-0 gnd rswk-swf Astrodynamik (DE-588)4143246-0 s 1\p DE-604 Erscheint auch als Druck-Ausgabe 978-1-108-47236-4 https://doi.org/10.1017/9781108560061 Verlag URL des Erstveröffentlichers Volltext 1\p cgwrk 20201028 DE-101 https://d-nb.info/provenance/plan#cgwrk |
| spellingShingle | Kéchichian, Jean Albert 1945- Applied nonsingular astrodynamics optimal low-thrust orbit transfer Orbital transfer (Space flight) Trajectory optimization Space trajectories Astrodynamik (DE-588)4143246-0 gnd |
| subject_GND | (DE-588)4143246-0 |
| 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 |
| title_sort | applied nonsingular astrodynamics optimal low thrust orbit transfer |
| title_sub | optimal low-thrust orbit transfer |
| topic | Orbital transfer (Space flight) Trajectory optimization Space trajectories Astrodynamik (DE-588)4143246-0 gnd |
| topic_facet | Orbital transfer (Space flight) Trajectory optimization Space trajectories Astrodynamik |
| url | https://doi.org/10.1017/9781108560061 |
| work_keys_str_mv | AT kechichianjeanalbert appliednonsingularastrodynamicsoptimallowthrustorbittransfer |