Averaging Methods for Design of Spacecraft Hysteresis Damper

Figure 1

A typical trajectory for 𝜖=0.25, 𝜅=0.1, 𝜔=0.949.

(a) Phase plot of 𝑏 versus 𝑎

(b) Time evolution of amplitude 𝑎²+𝑏² of pitch oscillations (29)