Design and Testing of a Flight Control System for Unstable Subscale Aircraft
The primary objective of this thesis was to study, implement, and test low-cost electronic flight control systems (FCS) in remotely piloted subscale research aircraft with relaxed static longitudinal stability. Even though this implementation was carried out in small, simplified test-bed aircraft, i...
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| Format: | Others |
| Language: | English |
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Linköpings universitet, Fluida och mekatroniska system
2015
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-121819 |