Sciweavers

Share
WCE
2007

Four Rotors Helicopter Yaw and Altitude Stabilization

11 years 24 days ago
Four Rotors Helicopter Yaw and Altitude Stabilization
— In this paper an appropriate four rotors helicopter nonlinear dynamic model for identi cation and control law synthesis is obtained via modelization procedure where several phenomena are included like gyroscopic effects and aerodynamic friction. The numerical simulations of the model obtained show that the control law stabilizes the four rotors helicopter with good tracking.
L. Derafa, A. Ouldali, Tarek Madani, Abdelaziz Ben
Added 07 Nov 2010
Updated 07 Nov 2010
Type Conference
Year 2007
Where WCE
Authors L. Derafa, A. Ouldali, Tarek Madani, Abdelaziz Benallegue
Comments (0)
books