Flight Dynamics Modelling and Application to SatelliteDeorbitation Strategy
In this paper a study to determine the best strategic choice to deorbit satellites incase of system failures is conducted. An orbital mechanic analysis of the deorbitationis done and a matlab code based on Lagrange’s interplanetary equations is developed.The effects of the atmospheric drag and the s...
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| Format: | Others |
| Language: | English |
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KTH, Flygdynamik
2011
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-30613 |