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

<table>The mixed <svg height="16.299999" id="M144" style="vertical-align:-3.3907pt" version="1.1" viewbox="0 0 56.037498 16.299999" width="56.037498" 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,-.012,43.212,16.088)"><path d="M983 225q0 -112 -67 -174.5t-150 -62.5q-91 0 -154.5 43.5t-113.5 129.5q-49 -85 -104 -129t-138 -44q-98 0 -158.5 66t-60.5 154q0 59 21 106.5t54.5 75.5t70.5 43t73 15q90 0 152.5 -43.5t112.5 -128.5q48 84 104.5 128t140.5 44q93 0 155 -65t62 -158zM478 196
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</svg> controller response to external torques for the pitch axis.</table>

Mathematical Problems in Engineering

fig13

Figure 13

Figure 13: 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

Figure 13