Mechanism and Application of Attitude and Orbit Coupling Dynamics for Spacecraft Proximity Relative Motion

<div>Relative velocity when navigation error is <span class="nowrap"><svg height="8.68572pt" id="M209" style="vertical-align:-0.0498209pt" version="1.1" viewbox="-0.0498162 -8.6359 13.7356 8.68572" width="13.7356pt" 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="M600 0V24L339 665L311 657L43 24V0H600ZM497 50H107L303 539L497 50Z"></path></g><g transform="matrix(.013,0,0,-0.013,8.327,0)"><path d="M220 349V455C158 436 98 425 38 417V389C85 378 92 374 92 323V104C92 43 83 38 28 32V0H302V32C225 38 220 43 220 104V291C237 330 257 343 276 343C292 343 305 336 322 322C329 316 339 313 353 318C379 328 402 356 402 392C402 426 374 454 335 454C297 454 259 411 222 349H220Z"></path></g></svg>.</span></div>

International Journal of Aerospace Engineering

fig13

Figure 13

Figure 13: Mechanism and Application of Attitude and Orbit Coupling Dynamics for Spacecraft Proximity Relative Motion 