Allocation Optimization Strategy for High-Precision Control of Picosatellites and Nanosatellites

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/6239725/figures/6239725.fig.0017a.svgz" name="6239725.fig.0017a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>The variation of attitude angles</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/6239725/figures/6239725.fig.0017b.svgz" name="6239725.fig.0017b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>The variation of attitude angular velocities</td></tr></table>

<div>Control results of SPMA using AECF.</div>

International Journal of Aerospace Engineering

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Figure 17

Figure 17: Allocation Optimization Strategy for High-Precision Control of Picosatellites and Nanosatellites 