Applied nonsingular astrodynamics (Record no. 560651)
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000 -LEADER | |
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fixed length control field | 01619 a2200229 4500 |
005 - DATE AND TIME OF LATEST TRANSACTION | |
control field | 20190819122050.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 190814b xxu||||| |||| 00| 0 eng d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
ISBN | 9781108472364 |
040 ## - CATALOGING SOURCE | |
Transcribing agency | IIT Kanpur |
041 ## - LANGUAGE CODE | |
Language code of text/sound track or separate title | eng |
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
Classification number | 629.4113 |
Item number | K233a |
100 ## - MAIN ENTRY--AUTHOR NAME | |
Personal name | Kechichian, Jean Albert |
245 ## - TITLE STATEMENT | |
Title | Applied nonsingular astrodynamics |
Remainder of title | optimal low-thrust orbit transfer |
Statement of responsibility, etc | Jean Albert Kechichian |
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
Name of publisher | Cambridge University Press |
Place of publication | Cambridge |
Year of publication | 2018 |
300 ## - PHYSICAL DESCRIPTION | |
Number of Pages | xvii, 461p |
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
Title | Cambridge aerospace series |
490 ## - SERIES STATEMENT | |
Series statement | / edited by Wei Shyy |
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. |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
Topical Term | Space trajectories |
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
Topical Term | Trajectory optimization |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Koha item type | Books |
Withdrawn status | Lost status | Damaged status | Not for loan | Collection code | Home library | Current library | Date acquired | Source of acquisition | Cost, normal purchase price | Full call number | Accession Number | Cost, replacement price | Koha item type |
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General Stacks | PK Kelkar Library, IIT Kanpur | PK Kelkar Library, IIT Kanpur | 26/08/2019 | 2 | 6207.15 | 629.4113 K233a | A184618 | 7758.94 | Books |