Optimization of Coaxial Rotor System for a Gun-Launched Micro Air Vehicle
In-Flight Measurements and Validation of Electric Powertrain Models
Biomimetic Adaptive Airframe Technology (BAAT) for Rotorcraft Design and Optimization
Design, Development, and Flight Testing of a 25-Kilogram Quad-Cyclocopter
Flow-Field and Force Measurements on a Cycloidal Rotor Blade in Forward Flight
Design, Development, and Flight Testing of a 70-Gram Micro Quad-Cyclocopter
A Model-Based Design Framework for Electric VTOL Aircraft
DEVELOPMENT OF ``ARIA'', A COMPACT, ULTRA-QUIET PERSONAL ELECTRIC HELICOPTER
DEVELOPMENT OF A BRUSHLESS DC MOTOR SIZING ALGORITHM FOR A SMALL UAS DESIGN FRAMEWORK
Development of an Air-Launched Tail-Sitter Unmanned Aerial Vehicle
Investigation of Coaxial Rotor Performance for a Gun-Launched Micro Air Vehicle
DESIGN, DEVELOPMENT AND FLIGHT TESTING OF A GUN-LAUNCHED ROTARY-WING MICRO AIR VEHICLE