Guidance Navigation and Control for Autonomous Multiple Spacecraft Assembly: Analysis and Experimentation

<table>Relative vectors used in the alignment and assembly logic. All vectors are in the LVLH <svg height="12.175" id="M57" style="vertical-align:-3.56265pt" version="1.1" viewbox="0 0 19.475 12.175" width="19.475" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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q0 16 13.5 31.5t28.5 15.5q12 0 17 -11q5 -10 25 -10q22 0 57.5 36t89.5 111l-40 108q-22 58 -36 58q-21 0 -67 -57l-19 20q81 107 125 107q17 0 30 -22t39 -88l22 -55q68 92 108.5 128.5t74.5 36.5q20 0 32.5 -14t12.5 -30z" id="x1D465"></path></g><g transform="matrix(.017,-0,0,-.017,9.565,7.675)"><path d="M556 393q0 -39 -36 -106q-42 -78 -185 -279q-47 -66 -81 -108t-117 -135l-112 -26l-8 22q150 90 251 219q-6 136 -39 340q-8 53 -21 53q-6 0 -27 -19.5t-38 -42.5l-16 26q80 111 127 111q23 0 35 -28t20 -90q18 -137 27 -263h2q142 200 142 279q0 24 -14 48q-4 7 5 26
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International Journal of Aerospace Engineering

fig7

Figure 7

Figure 7: Guidance Navigation and Control for Autonomous Multiple Spacecraft Assembly: Analysis and Experimentation 