Path Formation Time in the Noise-Limited Fractionated Spacecraft Network with FDMA

<div>The geometry of two identical orbits with a different RAAN, <span class="nowrap"><svg height="8.68572pt" id="M154" style="vertical-align:-0.0498209pt" version="1.1" viewbox="-0.0498162 -8.6359 18.3418 8.68572" width="18.3418pt" 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" id="g113-133"></path></g><g transform="matrix(.013,0,0,-0.013,8.327,0)"><path d="M719 146L691 147C666 77 657 72 612 72H528C572 125 688 224 688 364C688 546 558 665 384 665C212 665 77 541 77 361C77 221 188 124 239 72H150C110 72 97 80 73 147L46 146L63 0H307L314 18C284 71 178 203 178 360C178 529 256 631 383 631C509 631 588 523 588 363C588 197 485 67 453 18L458 0H701L719 146Z" id="g113-153"></path></g></svg>,</span> shown in the inertial reference frame.</div>

International Journal of Aerospace Engineering

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Figure 2

Figure 2: Path Formation Time in the Noise-Limited Fractionated Spacecraft Network with FDMA 