USAF Developmental Test and Evaluation Summit : 16 - 18 November 2004, Woodland Hills, California
Comprehensive approach for noise reduction in helicopter cabins
Active cabin vibration reduction for jet-smooth helicopter ride
The Development of Spoonbill UAV and LPV modeling of Longitudinal dynamics
Development of EC 135 turbulence models via system identification
Load transportation system based on autonomous small size helicopters
Vibration reduction of a rotorcraft UAV using PZT patches
Parameter identification by free-flight wind tunnel tests