Tendon-Sheath Mechanisms in Flexible Membrane Wing Mini-UAVs: Control and Performance

Figure 3

Design of the FMW mini-UAV and the final prototype: (a) 3D CAD model of the FMW mini-UAV; (b) 3D printed fuselage of the FMW mini-UAV. Carbon fiber rod is used for the tail boom.

(a)

(b)