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

Figure 15

The roll and pitch angles and -axis acceleration of both the rigid wing and FMW model at 7 Hz longitudinal gusts. Rigid wing behavior is shown in (a), (c), and (e), while those from FMW are shown in (b), (d), and (f).

(a)

(b)

(c)

(d)

(e)

(f)