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.

• Type: Conference
• Year: 2007
• Where: WCE
• Authors: L. Derafa, A. Ouldali, Tarek Madani, Abdelaziz Benallegue
• Keywords: Control Law, Nonlinear Dynamic Model, Rotors Helicopter, WCE 2007, WCE 2008