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Reliable Force Predictions for a Flapping-Wing Micro Air Vehicle: A “Vortex-Lift” Approach
Free accessSAGE Publications | 2011| -
Energy Absorption Behavior of a Hyperelastic Membrane for Micro Air Vehicle Wings: Experimental and Finite Element Approaches
Free accessSAGE Publications | 2011| -
Reviewing and Investigating the Use of Co-Axial Rotor Systems in Small UAVs
Free accessSAGE Publications | 2010| -
Simulator Development for Transition Flight Dynamics of a VTOL MAV
Free accessSAGE Publications | 2010| -
Performance Flight Testing of Small, Electric Powered Unmanned Aerial Vehicles
Free accessSAGE Publications | 2009| -
Development of a Kinematical Model to Study the Aerodynamics of Flapping-Wings
Free accessSAGE Publications | 2011| -
Biomimetic Analysis of Insect Wing Kinematics for Flapping MAVs
Free accessSAGE Publications | 2011| -
Optical Flow for Heading Estimation of a Quadrotor Helicopter
Free accessSAGE Publications | 2009| -
Computation vs. Experiment for High-Frequency Low-Reynolds Number Airfoil Plunge
Free accessSAGE Publications | 2009| -
Multi-Objective Topology Optimization of Wing Skeletons for Aeroelastic Membrane Structures
Free accessSAGE Publications | 2009| -
Experimental Characterization of Actuators for Micro Air Vehicles
Free accessSAGE Publications | 2011| -
Force Measurements and Flow Visualization for a Flexible Flapping Wing Mechanism
Free accessSAGE Publications | 2009| -
Experimental Analysis of a Fixed-Wing VTOL MAV in Ground Effect
Free accessSAGE Publications | 2010|
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