A team of researchers from the Army Research Laboratory, NASA Langley Research Center (LaRC), and Bell Helicopter-Textron, Inc. have completed hover-cell and wind-tunnel testing of a 1/5-size aeroelastically-scaled tiltrotor model using a new active control system for stability augmentation. The active system is based on a generalized predictive control (GPC) algorithm originally developed at NASA LaRC in 1997 for un-known disturbance rejection. Results of these investigations show that GPC combined with an active swashplate can significantly augment the damping and stability of tiltrotors in both hover and high-speed flight.
Experimental Investigations of Generalized Predictive Control for Tiltrotor Stability Augmentation
2001 CEAS/AIAA/AIAE International Forum of Aeroelasticity and Structural Dynamics ; 2001 ; Madrid, Spain
2001-01-01
Conference paper
No indication
English
British Library Conference Proceedings | 2023
|British Library Conference Proceedings | 2001
|