Research Article
Thermal Analysis and Rigid-Flexible Coupling Dynamics of a Satellite with Membrane Antenna
Figure 14
Dynamic response of the satellite-membrane-antenna system during the attitude maneuver with CSVS control: (a) attitude angle; (b) angular velocity in the x1 direction; (c) angular velocity in the y1 direction; (d) angular velocity in the z1 direction; (e) first-order modal coordinate; (f) second-order modal coordinate; (g) third-order modal coordinate; (h) fourth-order modal coordinate.
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