Antidisturbance Fault Tolerant Control of Attitude Control Systems for Microsatellite with Unknown Input Delay

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="804754.fig.003a" src="https://static.hindawi.com/articles/mpe/volume-2013/804754/figures/804754.fig.003a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Time responses of vibration and vibration observed</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="804754.fig.003b" src="https://static.hindawi.com/articles/mpe/volume-2013/804754/figures/804754.fig.003b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Partial amplification of (a)</td></tr></table></td></tr></table>

<table>Curves of vibration estimation of disturbance observer.</table>

Mathematical Problems in Engineering

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Figure 3

Figure 3: Antidisturbance Fault Tolerant Control of Attitude Control Systems for Microsatellite with Unknown Input Delay 