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</svg> Method via LMI Optimization

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td align="left">Properties </td><td align="center"> Value </td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td align="left">Size</td><td align="center"><svg height="11.125" id="M89" style="vertical-align:-0.1638pt" version="1.1" viewbox="0 0 67.824997 11.125" width="67.824997" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>
						4.5 cm </td></tr><tr><td align="left"> Mass </td><td align="center"> 10 gr </td></tr><tr><td align="left"> Accuracy </td><td align="center"> 1 arcseg</td></tr><tr><td align="left"> Angular velocity </td><td align="center">
						above 10°/s
					</td></tr><tr><td align="left"> Reliability </td><td align="center">99.99% </td></tr><tr><td align="left"> Rate of actualization </td><td align="center"> 8 Hz </td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

Mathematical Problems in Engineering

tab1

Table 1

Table 1: Design of the Microsatellite Attitude Control System Using the Mixed <svg     style="vertical-align:-4.47127pt;width:73.462502px;" id="M1" height="21.450001" version="1.1" viewBox="0 0 73.462502 21.450001" width="73.462502"  xmlns:xlink="http://www.w3.org/1999/xlink" xmlns="http://www.w3.org/2000/svg">
	
		
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</svg> Method via LMI Optimization 

Mathematical Problems in Engineering

Design of the Microsatellite Attitude Control System Using the Mixed Method via LMI Optimization

Table 1