On Bounded Satellite Motion under Constant Radial Propulsive Acceleration

<table>Allowed region for bounded motion in the <svg height="16.625" id="M91" style="vertical-align:-2.21957pt" version="1.1" viewbox="0 0 46.849998 16.625" width="46.849998" xmlns="http://www.w3.org/2000/svg">
<g transform="matrix(1.25,0,0,-1.25,0,16.625)">
<g transform="translate(72,-58.7)">
<text transform="matrix(1,0,0,-1,-71.95,60.96)">
<tspan style="font-size: 12.50px; " x="0" y="0">(</tspan>
<tspan style="font-size: 12.50px; " x="4.1634989" y="0">Φ</tspan>
<tspan style="font-size: 12.50px; " x="13.703288" y="0">,</tspan>
<tspan style="font-size: 12.50px; " x="18.904535" y="0">𝐺</tspan>
</text>
<text transform="matrix(1,0,0,-1,-43.61,66.03)">
<tspan style="font-size: 8.75px; " x="0" y="0">2</tspan>
</text>
<text transform="matrix(1,0,0,-1,-38.74,60.96)">
<tspan style="font-size: 12.50px; " x="0" y="0">)</tspan>
</text>
</g>
</g>
</svg>-plane.</table>

Mathematical Problems in Engineering

fig3

Figure 3

Figure 3: On Bounded Satellite Motion under Constant Radial Propulsive Acceleration 