Fault Reconstruction Approach for Distributed Coordinated Spacecraft Attitude Control System

<div>The reconstruction error <svg height="9.71953pt" id="M252" style="vertical-align:-3.42779pt" version="1.1" viewbox="-0.0498162 -6.29174 11.1764 9.71953" width="11.1764pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.0135,0,0,-0.0135,0,0)"><path d="M400 123C365 93 327 80 288 80C216 80 157 134 153 241C251 245 374 254 392 257C414 260 420 273 421 293C421 375 351 454 258 454H257C203 454 148 427 104 383C62 341 30 278 30 202C30 87 103 -12 237 -12C279 -12 357 8 417 99L400 123ZM237 414C276 414 299 362 298 311C298 294 292 291 277 291C236 290 199 289 157 288C164 367 198 414 237 414Z" id="g13-99"></path><glyph.data ascent="1024" descent="-360" horiz-adv-x="437" vert-adv-y="437"></glyph.data></g><g transform="matrix(.0095,0,0,-0.0095,5.921,3.264)"><path d="M290 377C321 398 342 415 358 430C378 450 389 473 389 502C389 578 329 635 238 635H237C184 635 137 610 109 578L64 515L88 493C112 529 154 573 208 573S303 542 303 482C303 409 233 370 141 341L149 308C165 313 190 319 215 319C272 319 341 283 341 193C342 98 292 43 222 43C163 43 122 72 96 94C88 101 79 100 70 94C61 87 47 73 46 60C44 47 48 37 62 23C76 10 118 -12 165 -12C238 -12 430 62 430 223C430 297 379 359 290 375V377Z" id="g50-52"></path><glyph.data ascent="3443" descent="-2856" horiz-adv-x="487" vert-adv-y="487"></glyph.data></g></svg> for the third spacecraft.</div>

Mathematical Problems in Engineering

fig4

Figure 4

Figure 4: Fault Reconstruction Approach for Distributed Coordinated Spacecraft Attitude Control System 