Finite-Time Anti-Disturbance Inverse Optimal Attitude Tracking Control of Flexible Spacecraft

<table>Angular velocity tracking errors—controller <svg height="15.0875" id="M356" style="vertical-align:-2.3205pt" version="1.1" viewbox="0 0 28.2125 15.0875" width="28.2125" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> in [<a href="/journals/mpe/2013/967574/#B38">37</a>].</table>

Mathematical Problems in Engineering

fig12

Figure 12

Figure 12: Finite-Time Anti-Disturbance Inverse Optimal Attitude Tracking Control of Flexible Spacecraft 