Estimation of Aerodynamic Parameters in Real-Time : Implementation and Comparison of a Sequential Frequency Domain Method and a Batch Method
The flight testing and evaluation of collected data must be efficient during intensive flight-test programs such as the ones conducted during development of new aircraft. The aim of this thesis has thus been to produce a first version of an aerodynamic derivative estimation program that is to be use...
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| Format: | Others |
| Language: | English |
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Linköpings universitet, Fluida och mekatroniska system
2016
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-132807 |