Parra, Camille and Su, Bingwei and Bordeneuve-Guibé, Joël
and Brière, Yves
Development of a MAV from theory to implementation.
(2002)
In: UVS-TECH 2002, 5 December 2002 - 6 December 2002 (Brussells, Belgium).
(Unpublished)
|
(Document in English)
PDF (Author's version) - Requires a PDF viewer such as GSview, Xpdf or Adobe Acrobat Reader 693kB |
Abstract
A nonlinear model of Pégase, a mini aerial vehicle, is established from the data of wind tunnel test. The interpolation of the force and moment coefficients is introduced. After that, a level straight flight linearization equation is obtained. According to this equation, based on the idea of dynamic inversion, an attitude control law is devised and verified by nonlinear simulation. Later on, the 2-D guidance loop is designed. It includes the altitude control loop and heading control loop. Then a simple attitude determination algorithm is presented. Finally we introduce our experimental setup.
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Audience (conference): | International conference without published proceedings |
| Uncontrolled Keywords: | |
| Institution: | Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE-SUPAERO (FRANCE) |
| Laboratory name: | Département de Mathématiques, Informatique, Automatique - DMIA (Toulouse, France) - Automatique, Dynamique et Interface des Systèmes - ADIS |
| Statistics: | download |
| Deposited On: | 21 Mar 2008 14:38 |
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