Generalization of Active In-Flight Tracking Control to the N-Bladed Helicopter Rotor
暂无分享,去创建一个
[1] Peretz P. Friedmann,et al. Simultaneous blade-vortex interaction noise and vibration reduction in rotorcraft using microflaps, including the effect of actuator saturation , 2015 .
[2] Kourosh Danai,et al. Adaptive Method of Helicopter Track and Balance , 2005 .
[3] Peretz P. Friedmann,et al. On-blade control of rotor vibration, noise, and performance: Just around the corner? The 33rd Alexander Nikolsky honorary lecture , 2014 .
[4] Walter Fichter,et al. In-Flight Tracking Control for Helicopters using Active Trailing Edge Flaps , 2012 .
[5] Ch. Kessler,et al. Active rotor control for helicopters: individual blade control and swashplateless rotor designs , 2011 .
[6] Inderjit Chopra,et al. An Integrated Three-Dimensional Aeromechanics Analysis of the NASA Tilt Rotor Aeroacoustic Model , 2018, Journal of the American Helicopter Society.
[7] Uwe T.P. Arnold,et al. Closed loop IBC results from CH-53G flight tests , 2005 .
[8] Walter Fichter,et al. In-Flight Rotorblade Tracking Control for Helicopters Using Active Trailing-Edge Flaps , 2014 .
[9] W. Fichter,et al. Linear Analysis of Vibration Reduction Using an Active N-Bladed Helicopter Rotor , 2019, Journal of Guidance, Control, and Dynamics.