Reconfigurability Analysis Method for Spacecraft Autonomous Control

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr class="thead"><td align="left">MRU</td><td align="center"><span style="width: 8.6374998px;"><svg height="12.175" id="M137" style="vertical-align:-2.34499pt" version="1.1" viewbox="0 0 8.6374998 12.175" width="8.6374998" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg></span></td><td align="center"><i>I </i></td></tr><tr><td class="thead-hr" colspan="3"><hr/></td></tr><tr><td align="left">ESPower</td><td align="center">0</td><td align="center">1</td></tr><tr><td align="left"> ES1</td><td align="center">1</td><td align="center">0.5</td></tr><tr><td align="left"> ES2</td><td align="center">1</td><td align="center">0.5</td></tr><tr><td align="left">GPower</td><td align="center">1</td><td align="center">0</td></tr><tr><td align="left"> <svg height="15.6875" id="M138" style="vertical-align:-3.21404pt" version="1.1" viewbox="0 0 19.700001 15.6875" width="19.700001" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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<g transform="matrix(.012,-0,0,-.012,12.375,15.475)"><path d="M536 404q0 -17 -13.5 -31.5t-26.5 -14.5q-8 0 -15 10q-11 14 -25 14q-22 0 -67 -50q-47 -52 -68 -82l37 -102q31 -88 55 -88t78 59l16 -23q-32 -48 -68.5 -78t-65.5 -30q-19 0 -37.5 20t-29.5 53l-41 116q-72 -106 -114.5 -147.5t-79.5 -41.5q-21 0 -34.5 14t-13.5 37
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</svg></td><td align="center">1</td><td align="center">0</td></tr><tr><td align="left"> <svg height="18.65" id="M139" style="vertical-align:-4.74141pt" version="1.1" viewbox="0 0 19.950001 18.65" width="19.950001" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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<g transform="matrix(.012,-0,0,-.012,12.375,15.475)"><path d="M556 393q0 -39 -36 -106q-42 -78 -185 -279q-47 -66 -81 -108t-117 -135l-112 -26l-8 22q150 90 251 219q-6 136 -39 340q-8 53 -21 53q-6 0 -27 -19.5t-38 -42.5l-16 26q80 111 127 111q23 0 35 -28t20 -90q18 -137 27 -263h2q142 200 142 279q0 24 -14 48q-4 7 5 26
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</svg></td><td align="center">1</td><td align="center">0</td></tr><tr><td align="left"> <svg height="15.775" id="M140" style="vertical-align:-3.25793pt" version="1.1" viewbox="0 0 18.975 15.775" width="18.975" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,.062,11.4)"><path d="M713 296l-5 -25q-47 -7 -59 -20t-23 -72l-15 -79q-9 -48 -3 -74q-15 -3 -55 -13t-63 -15t-59.5 -10t-70.5 -5q-149 0 -243 80t-94 220q0 169 127.5 276.5t336.5 107.5q91 0 206 -36l-10 -165l-29 -1q1 85 -47.5 126t-146.5 41q-153 0 -243.5 -97t-90.5 -242
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</svg></td><td align="center">1</td><td align="center">0</td></tr><tr class="table-tr"><td colspan="3"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

tab5

Table 5

Table 5: Reconfigurability Analysis Method for Spacecraft Autonomous Control 