Affiliation:
1. University of Stuttgart, 70569 Stuttgart, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Reference15 articles.
1. Active rotor control for helicopters: individual blade control and swashplateless rotor designs
2. On-Blade Control of Rotor Vibration, Noise, and Performance: Just Around the Corner? The 33rd Alexander Nikolsky Honorary Lecture
3. ReberD. “Modellbildung und Regelung zur Reduktion von Vibrationen und ‘Dynamic Stall’ bei Hubschrauberrotoren,” Fortschritt-Berichte VDI, Vol. 8, No. 1142, VDI Verlag, Düsseldorf, Germany, 2008, pp. 29–70.
4. In-Flight Rotorblade Tracking Control for Helicopters Using Active Trailing-Edge Flaps
5. Simultaneous Blade–Vortex Interaction Noise and Vibration Reduction in Rotorcraft Using Microflaps, Including the Effect of Actuator Saturation