En indirekt metod för adaptiv reglering av en helikopter
When a helicopter is flying, the dynamics vary depending on, for example, speed and position. Hence, a time-invariant linear model cannot describe its properties under all flight conditions. It is therefore desirable to update the linear helicopter model continuously during the flight. In this thesi...
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| Format: | Others |
| Language: | Swedish |
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Linköpings universitet, Tekniska högskolan
2009
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17637 |