A Miniature Integrated Navigation System for Rotary-Wing Unmanned Aerial Vehicles

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="748940.fig.0013a" src="https://static.hindawi.com/articles/ijae/volume-2014/748940/figures/748940.fig.0013a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>Flight trajectory</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="748940.fig.0013b" src="https://static.hindawi.com/articles/ijae/volume-2014/748940/figures/748940.fig.0013b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Estimated velocity</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="748940.fig.0013c" src="https://static.hindawi.com/articles/ijae/volume-2014/748940/figures/748940.fig.0013c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>Estimated attitude</td></tr></table></td></tr></table>

<table>Estimated flight states of quadrotor in hovering flight.</table>

International Journal of Aerospace Engineering

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Figure 13

Figure 13: A Miniature Integrated Navigation System for Rotary-Wing Unmanned Aerial Vehicles 