Separation Analysis with OpenModelica
When launching a satellite a separation system is used to keep the satellite attached to a launch vehicle during ascent and to separate it from the launch vehicle while in space. In separation analysis the separation is studied by simulations to see if requirements on the system can be fulfilled. Th...
Main Author: | Källdahl, Malin |
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Format: | Others |
Language: | English |
Published: |
Linköpings universitet, Institutionen för systemteknik
2007
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Subjects: | |
Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-10399 |
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