Hardware-in-the-Loop Simulation for Spacecraft Formation Flying

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="572526.fig.0010a" src="https://static.hindawi.com/articles/jcse/volume-2010/572526/figures/572526.fig.0010a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Burkert valve at 60 psi</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="572526.fig.0010b" src="https://static.hindawi.com/articles/jcse/volume-2010/572526/figures/572526.fig.0010b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>SMC valve at 28 psi</td></tr></table></td></tr></table>

<table>Thruster characterization test.</table>

Journal of Control Science and Engineering

fig10

Figure 10

Figure 10: Hardware-in-the-Loop Simulation for Spacecraft Formation Flying 