[PDF][PDF] A Flight Dynamics Helicopter UAV Model For A Single Pitch-Lag-Flap Main Rotor: Modeling & Simulations
S Taamallah - 2010 - reports.nlr.nl
We present a UAV helicopter flight dynamics nonlinear model for a flybarless articulated
Pitch-Lag-Flap (PLF) main rotor with rigid blades, applicable for high bandwidth control …
Pitch-Lag-Flap (PLF) main rotor with rigid blades, applicable for high bandwidth control …