Nonlinear control of aerial vehicles subjected to aerodynamic forces
Résumé
The paper contributes towards the development of a unified control approach for longitudinal aircraft dynamics. It states conditions that allow to adapt the control strategies developed for orientation-independent external forces to the orientation-dependent case. The control strategy presented here is a step to the automatic monitoring of the flight transitions between hovering and cruising for convertible aerial vehicles.
| Origine | Fichiers produits par l'(les) auteur(s) |
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