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Communication Dans Un Congrès Année : 2007

Attitude Stabilization in Hover Flight of a Mini Tail-Sitter UAV with Variable Pitch Propeller

Résumé

In this paper, the modeling and control design of a vertical flight attitude control for a mini tail-sitter with variable pitch propeller is discussed. Tail-sitters VTOL-UAVs have operational flexibility of typical helicopters while having the cruise performance of fixed wing airplanes. The configuration proposed in this work is highly unstable in its natural flight state in vertical mode. A dynamic model is developed and a linear control strategy has been developed to stabilize the platform. The results are supported by experimental tests.

Domaines

Automatique
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Dates et versions

hal-00448754 , version 1 (20-01-2010)

Identifiants

  • HAL Id : hal-00448754 , version 1

Citer

K.C. Wong, Jose Alfredo Guerrero, David Lara, Rogelio Lozano. Attitude Stabilization in Hover Flight of a Mini Tail-Sitter UAV with Variable Pitch Propeller. 2007 IEEE/RSJ International Conference on Intelligent Robots and Systems, Oct 2007, San Diego, United States. ⟨hal-00448754⟩
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