Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure

<table>Time dependence of angles <svg height="11.05" id="M251" style="vertical-align:-3.2316pt" version="1.1" viewbox="0 0 12.3375 11.05" width="12.3375" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,11.05)">
<g transform="translate(72,-63.16)">
<text transform="matrix(1,0,0,-1,-71.95,66.44)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝛼</tspan>
</text>
<text transform="matrix(1,0,0,-1,-65.4,63.31)">
<tspan style="font-size: 8.75px; " x="0" y="0">𝑖</tspan>
</text>
</g>
</g>
</svg>. </table>

Modelling and Simulation in Engineering

fig12

Figure 12

Figure 12: Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure 