Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques

<table class="table-group" id="tab6"><tr><td><table class="table"><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr class="thead"><td align="left">Time Simulation (days)</td><td align="center">11</td><td align="center">8</td><td align="center">3</td><td align="center">2</td></tr><tr><td class="thead-hr" colspan="5"><hr/></td></tr><tr><td align="left"><svg height="16.174999" id="M137" style="vertical-align:-4.68872pt" version="1.1" viewbox="0 0 87.175003 16.174999" width="87.175003" xmlns="http://www.w3.org/2000/svg">
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<tspan style="font-size: 12.50px; " x="0" y="0">𝑊</tspan>
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<text transform="matrix(1,0,0,-1,-60.5,60.66)">
<tspan style="font-size: 8.75px; " x="0" y="0">S</tspan>
<tspan style="font-size: 8.75px; " x="4.8661122" y="0">C</tspan>
<tspan style="font-size: 8.75px; " x="10.703696" y="0">C</tspan>
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<tspan style="font-size: 12.50px; " x="0" y="0">−</tspan>
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<tspan style="font-size: 8.75px; " x="0" y="0">Q</tspan>
<tspan style="font-size: 8.75px; " x="6.318944" y="0">C</tspan>
<tspan style="font-size: 8.75px; " x="12.156528" y="0">I</tspan>
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</svg> (rpm)</td><td align="center">−0.1475</td><td align="center">−0.1091</td><td align="center">−0.0312</td><td align="center">−0.0144</td></tr><tr class="table-tr"><td colspan="5"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mean deviations for different time simulations for spin velocity and SCD1 (in degrees).

Mathematical Problems in Engineering

tab6

Table 6

Table 6: Spin-Stabilized Spacecrafts: Analytical Attitude Propagation Using Magnetic Torques 