Dynamics and Control of Morphing Aircraft
The following work is directed towards an evaluation of aircraft that undergo structural shape change for the purpose of optimized flight and maneuvering control authority. Dynamical equations are derived for a morphing aircraft based on two primary representations; a general non-rigid model and a m...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/28681 http://scholar.lib.vt.edu/theses/available/etd-08162005-134143/ |