Attitude Analysis and Robust Adaptive Backstepping Sliding Mode Control of Spacecrafts Orbiting Irregular Asteroids

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="367163.fig.0032a" src="https://static.hindawi.com/articles/mpe/volume-2014/367163/figures/367163.fig.0032a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Control of pitch</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="367163.fig.0032b" src="https://static.hindawi.com/articles/mpe/volume-2014/367163/figures/367163.fig.0032b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Partial enlargement of control</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="367163.fig.0032c" src="https://static.hindawi.com/articles/mpe/volume-2014/367163/figures/367163.fig.0032c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Partial enlargement of control</td></tr></table></td></tr></table>

Mathematical Problems in Engineering

fig32

Figure 32

Figure 32: Attitude Analysis and Robust Adaptive Backstepping Sliding Mode Control of Spacecrafts Orbiting Irregular Asteroids 