micro air vehicle

Structural Technology Evaluation and Analysis Program (STEAP). Delivery Order 0035: Dynamics and Control and Computational Design of Flapping Wing Micro Air Vehicles

Computation of Inertial Forces and Torques Associated with Flapping Wings

Typically, inertial loads associated with flapping wing micro air vehicles are ignored for analysis and control law development purposes. The goal of this work is to compute the inertial loads associated with flapping a wing and compare those loads …

Flapping Wing Technology for Micro Air Vehicles Incorporating a Lead Zirconate Titanate (PZT) Bimorph Actuator