Itasse, Maxime and Moschetta, Jean-Marc Hybrid micro air vehicle for complex environment missions. (2012) In: Workshop Micro-Drones du Micro Air Vehicle Research Center, 27 Jan 2012, Toulouse, France. (Unpublished)
![[img]](http://oatao.univ-toulouse.fr/style/images/fileicons/application_pdf.png)
| (Document in English) PDF (Author's version) - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader 7Mb |
Abstract
Modern urban reconnaissance missions dictate the need for a Micro Air Vehicle (MAV) platform capable of performing a complex mission : rapid and efficient ingress to a target location followed by slow loiter for quality image capture. This may be achieved using a tilt-body fixed-wing vehicle which combines the speed, range, and gust-hardiness of a fixed wing with the loiter and precision capability of a rotorcraft vehicle.
| Item Type: | Conference or Workshop Item (Poster) |
|---|---|
| Audience (conference): | National conference without published proceedings |
| Uncontrolled Keywords: | Transition - MAV - Experimental - Numerical - Low Reynolds - Wind Tunnel - Fixed-wing - Tilt-body - Propeller - Wheel |
| Institution: | Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE |
| Laboratory name: | |
| Statistics: | download |
| Deposited By: | Maxime ITASSE |
Repository Staff Only: item control page
