Thermal Analysis and Rigid-Flexible Coupling Dynamics of a Satellite with Membrane Antenna

Figure 15

Dynamic response of the satellite-membrane-antenna system during the attitude maneuver with modeling disturbance under CSVS control: (a) attitude angle; (b) angular velocity in the direction; (c) angular velocity in the direction; (d) angular velocity in the direction; (e) first-order modal coordinate; (f) second-order modal coordinate; (g) third-order modal coordinate; (h) fourth-order modal coordinate.

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)