Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros

<div>Desired <svg height="9.51299pt" id="M191" style="vertical-align:-3.29111pt" version="1.1" viewbox="-0.0498162 -6.22188 13.396 9.51299" width="13.396pt" 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="M570 456L546 470C529 452 514 445 490 445C451 445 409 450 346 450C134 450 21 324 21 171C21 59 80 -12 197 -12C343 -12 453 99 453 227C453 286 433 327 375 370L376 373C409 368 450 363 487 363C521 363 548 377 570 456ZM340 272C340 210 304 31 214 31C166 31 150 87 150 140C150 249 198 377 285 377C298 377 312 369 322 356C339 333 340 304 340 272Z" id="g5-240"></path><glyph.data ascent="3481" descent="-2878" horiz-adv-x="586" vert-adv-y="586"></glyph.data></g><g transform="matrix(.0091,0,0,-0.0091,7.647,3.132)"><path d="M538 684C542 703 539 710 529 710C512 710 455 682 363 674L361 644H396C444 644 448 642 438 594L405 438C373 450 347 451 336 451C288 451 200 416 147 374C69 312 24 207 24 113C24 29 60 -12 94 -12C126 -12 156 4 196 30C231 53 296 100 346 166H348L328 81C311 10 325 -12 348 -12C380 -12 450 24 512 98L495 125C466 97 431 70 417 70C408 70 408 80 411 98L538 684ZM390 373L361 240C336 196 210 56 145 56C132 56 113 73 113 131C113 216 156 338 220 379C243 394 266 402 303 402C331 402 375 388 390 373Z" id="g50-101"></path><glyph.data ascent="3443" descent="-2856" horiz-adv-x="564" vert-adv-y="564"></glyph.data></g></svg> profile.</div>

International Journal of Aerospace Engineering

fig1

Figure 1

Figure 1: Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros 

Figure 1 | Integrated Power and Attitude Control Design of Satellites Based on a Fuzzy Adaptive Disturbance Observer Using Variable-Speed Control Moment Gyros 