Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure

<table>General coordinates <svg height="11.1875" id="M255" style="vertical-align:-3.2316pt" version="1.1" viewbox="0 0 11.95 11.1875" width="11.95" xmlns="http://www.w3.org/2000/svg">
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<g transform="translate(72,-63.05)">
<text transform="matrix(1,0,0,-1,-71.95,66.32)">
<tspan style="font-size: 12.50px; " x="0" y="0">𝑧</tspan>
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<text transform="matrix(1,0,0,-1,-65.71,63.2)">
<tspan style="font-size: 8.75px; " x="0" y="0">𝑖</tspan>
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</svg> versus time at optimal deployment law. </table>

Modelling and Simulation in Engineering

fig14

Figure 14

Figure 14: Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure 