Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="302982.fig.0013a" src="https://static.hindawi.com/articles/aaa/volume-2014/302982/figures/302982.fig.0013a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>The whole response</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="302982.fig.0013b" src="https://static.hindawi.com/articles/aaa/volume-2014/302982/figures/302982.fig.0013b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>The steady-state behavior</td></tr></table></td></tr></table>

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</svg> with different disturbance and uncertain inertia.</table>

Abstract and Applied Analysis

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Figure 13

Figure 13: Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite 