Applied nonsingular astrodynamics optimal low-thrust orbit transfer / (Record no. 84244)
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000 -LEADER | |
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fixed length control field | 02322nam a2200373 i 4500 |
001 - CONTROL NUMBER | |
control field | CR9781108560061 |
005 - DATE AND TIME OF LATEST TRANSACTION | |
control field | 20240730160805.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 180102s2018||||enk o ||1 0|eng|d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
ISBN | 9781108560061 (ebook) |
082 00 - CLASSIFICATION NUMBER | |
Call Number | 629.4/113 |
100 1# - AUTHOR NAME | |
Author | Kéchichian, Jean Albert, |
245 10 - TITLE STATEMENT | |
Title | Applied nonsingular astrodynamics optimal low-thrust orbit transfer / |
300 ## - PHYSICAL DESCRIPTION | |
Number of Pages | 1 online resource (xvii, 461 pages) : |
490 1# - SERIES STATEMENT | |
Series statement | Cambridge aerospace series ; |
500 ## - GENERAL NOTE | |
Remark 1 | Title from publisher's bibliographic system (viewed on 31 Aug 2018). |
520 ## - SUMMARY, ETC. | |
Summary, etc | 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. |
856 40 - ELECTRONIC LOCATION AND ACCESS | |
Uniform Resource Identifier | https://doi.org/10.1017/9781108560061 |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Koha item type | eBooks |
264 #1 - | |
-- | Cambridge : |
-- | Cambridge University Press, |
-- | 2018. |
336 ## - | |
-- | text |
-- | txt |
-- | rdacontent |
337 ## - | |
-- | computer |
-- | c |
-- | rdamedia |
338 ## - | |
-- | online resource |
-- | cr |
-- | rdacarrier |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Orbital transfer (Space flight) |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Trajectory optimization. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Space trajectories. |
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