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DSpace at Transilvania University >
Mechanical Engineering >
COMEC 2009 >
Please use this identifier to cite or link to this item:
http://hdl.handle.net/123456789/1127
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| Title: | MODIFICATIONS OF SPACECRAFT ORBITS |
| Authors: | BENCZE, A
NICULITA, C
CONSTANTIN, A
ZELENYAK, E
BORITU, A
TANASE, D |
| Keywords: | spacecraft, trajectory,
transfer orbit, energy, optimization |
| Issue Date: | 2009 |
| Publisher: | Transilvania University Press of Braşov |
| Citation: | Google Scholar |
| Series/Report no.: | COMEC 2009;463-464 |
| Abstract: | The paper present a basic methods for the preliminary calculation of the parameters needed to modify the orbit of a
spacecraft. The modifications and corrections of the orbit can be related to the orbit radius, eccentricity, speed and inclination. The
methods presented make use of the classical space mechanics in order to address the important problems of optimization for fuel
consumption, energy, time and costs. |
| URI: | http://hdl.handle.net/123456789/1127 |
| ISBN: | 978-973-598-572-1 |
| Appears in Collections: | COMEC 2009
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