Finite-Time Stabilization Control for a Rigid Spacecraft under Parameter Uncertainties

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<g transform="matrix(.017,-0,0,-.017,.062,7.9)"><path d="M538 43v-23l-63 -7q-80 -9 -132 -26v65q-39 -37 -71.5 -51.5t-73.5 -14.5q-63 0 -98 38t-35 107v241q0 35 -9 47t-40 18v24h188v-334q0 -76 56 -76q38 0 82 47v276q0 34 -12.5 47t-48.5 16v24h200v-356q0 -34 12.5 -47.5t44.5 -14.5z" id="x1D42E"></path></g>
</svg> without disturbs.</table>

Journal of Applied Mathematics

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Figure 3

Figure 3: Finite-Time Stabilization Control for a Rigid Spacecraft under Parameter Uncertainties 