Robust <i>H</i><sub>∞</sub> Control for the Spacecraft with Flexible Appendages

<div>Bode diagram of the weighting function <span class="nowrap"><svg height="11.8174pt" id="M29" style="vertical-align:-3.1815pt" version="1.1" viewbox="-0.0498162 -8.6359 15.8635 11.8174" width="15.8635pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M962 650H739L732 622L760 619C812 613 819 604 798 552C760 457 671 267 606 131H604L511 638H480L237 131H233L183 554C177 607 183 614 226 619L248 622L257 650H24L17 622C88 615 92 611 103 524L173 -11H203L450 491H453L543 -11H575L839 529C882 609 886 613 953 622L962 650Z"></path></g><g transform="matrix(.0091,0,0,-0.0091,10.777,3.132)"><path d="M389 0V32C297 38 291 46 291 118V635C234 613 175 595 109 583V556L161 554C203 552 207 547 207 497V118C207 46 201 38 110 32V0H389Z"></path></g></svg>.</span></div>

Complexity

fig5

Figure 5

Figure 5: Robust <i>H</i><sub>∞</sub> Control for the Spacecraft with Flexible Appendages 

Complexity

Robust H∞ Control for the Spacecraft with Flexible Appendages

Figure 5

Robust H_∞ Control for the Spacecraft with Flexible Appendages