Mathematical Problems in Engineering / 2014 / Article / Fig 3

Research Article

Satellite Attitude Control System Design Taking into Account the Fuel Slosh and Flexible Dynamics

Figure 3

The angular and sloshing control by the LQR and LQG controller.
820586.fig.003a
(a)
820586.fig.003b
(b)
820586.fig.003c
(c)
820586.fig.003d
(d)

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