Helicopter Vibration Reduction Using Active Twist Control of Composite Rotor Blades
Enabling Operational Autonomy for UAVs with Robustness (AIAA 2013-4652)
Increasing Operational and Fuel Efficiency for Multi-UAV Missions (AIAA 2013-4732)
A Refined Structural Dynamics Model for Composite Rotor Blades
Genetic Algorithm for the Time-Dependent Vehicle Routing Problem
AIAA-2003-3938 Investigation of Plume Effects on Longitudinal Aerodynamics of Missile at M=1.2
Absolute Orientation for a UAV using Celestial Objects (AIAA 2013-5145)