Mechanism and experiments of asymmetrical pitch system for MAV

Abstract

In view of problem for miniaturizing Micro Air Vehicles (MAV), a novel asymmetrical pitch system faced to rotary wing MAV is introduced. The pitch mechanism and control characteristics are studied and analyzed. Because the deformation of elasticity link is key to generate the blade pitch, it is analyzed and calculated by elasticity finite element method… (More)

Topics

  • Presentations referencing similar topics