Immersion and Invariance Adaptive Control for Spacecraft Pose Tracking via Dual Quaternions

<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">Orbit 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">26553.4</td></tr><tr><td class="align_left">Eccentricity</td><td class="align_center">0.73</td></tr><tr><td class="align_left">Inclination</td><td class="align_center">63.4</td></tr><tr><td class="align_left">Argument of perigee (deg)</td><td class="align_center">270</td></tr><tr><td class="align_left">RAAN (deg)</td><td class="align_center">329.6</td></tr><tr><td class="align_left">True anomaly (deg)</td><td class="align_center">100.5</td></tr><tr class="table-tr"><td colspan="2"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Orbit elements of the target spacecraft.</div>

Complexity

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Table 1

Table 1: Immersion and Invariance Adaptive Control for Spacecraft Pose Tracking via Dual Quaternions 