Itasse, Maxime and Moschetta, Jean-Marc and Ameho, Yann and Carr, Ryan Equilibrium transition study for a hybrid MAV. (2011) In: Inernational Micro Air Vehicle Conference and Flight Competition, 12-15 Sep 2011, 't Harde, the Netherlands .
(Document in English)
PDF (Author's version) - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader
Official URL: http://dx.doi.org/10.1260/1756-8222.214.171.124
Wind tunnel testing was performed on a VTOL aircraft in order to characterize longitudinal flight behavior during a transition between vertical and horizontal flight modes. Trim values for airspeed, pitch, motor speed and elevator position were determined. Data was collected by independently varying the trim parameters, and stability and control derivatives were identified as functions of the trim pitch angle. A linear fractional representation model was then proposed, along with several methods to improve longitudinal control of the aircraft.
|Item Type:||Conference or Workshop Item (Paper)|
|Additional Information:||Article publié dans la revue International Journal of Micro Air Vehicles, volume 3, n° 4, december 2011, éditeur : Multi-Science Publishing : http://multi-science.metapress.com/content/82lk15621n785376/?referencesMode=Show|
|Audience (conference):||International conference proceedings|
|Institution:||Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE (FRANCE)|
French research institutions > Office National d'Etudes et Recherches Aérospatiales - ONERA (FRANCE)
|Deposited By:||Maxime ITASSE|
|Deposited On:||02 Mar 2012 13:22|
Repository Staff Only: item control page