Extended-State-Observer-Based Terminal Sliding Mode Tracking Control for Synchronous Fly-Around with Space Tumbling Target

<table class="table-group" id="tab1"><tr><td><table class="table"><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr class="thead"><td class="align_left">Orbital elements</td><td class="align_center">Values</td></tr><tr><td class="thead-hr" colspan="2"><hr/></td></tr><tr><td class="align_left">Semimajor axis (km)</td><td class="align_center">6778</td></tr><tr><td class="align_left">Eccentricity</td><td class="align_center">0.02</td></tr><tr><td class="align_left">Inclination (deg)</td><td class="align_center">45</td></tr><tr><td class="align_left">Right ascension of the ascending node (deg)</td><td class="align_center">30</td></tr><tr><td class="align_left">Argument of perigee (deg)</td><td class="align_center">25</td></tr><tr><td class="align_left">True anomaly (deg)</td><td class="align_center">30</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Simulation experiment parameters.</div>

Mathematical Problems in Engineering

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Table 1

Table 1: Extended-State-Observer-Based Terminal Sliding Mode Tracking Control for Synchronous Fly-Around with Space Tumbling Target 