Designing a Robust Nonlinear Dynamic Inversion Controller for Spacecraft Formation Flying

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="471352.fig.0010a" src="https://static.hindawi.com/articles/mpe/volume-2014/471352/figures/471352.fig.0010a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Control inputs generated by NDI</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="471352.fig.0010b" src="https://static.hindawi.com/articles/mpe/volume-2014/471352/figures/471352.fig.0010b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Control inputs generated by RNDI</td></tr></table></td></tr></table>

<table>Control inputs generated by NDI and RNDI.</table>

Mathematical Problems in Engineering

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Figure 10

Figure 10: Designing a Robust Nonlinear Dynamic Inversion Controller for Spacecraft Formation Flying 