A Simplified Kalman Filter for Integrated Navigation System with Low-Dynamic Movement

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/mpe/volume-2016/3528146/figures/3528146.fig.007a.svgz" name="3528146.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Pitch</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/mpe/volume-2016/3528146/figures/3528146.fig.007b.svgz" name="3528146.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Roll</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/mpe/volume-2016/3528146/figures/3528146.fig.007c.svgz" name="3528146.fig.007c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Yaw</td></tr></table>

<div>The attitude error curves of turntable experiment.</div>

Mathematical Problems in Engineering

fig7

Figure 7

Figure 7: A Simplified Kalman Filter for Integrated Navigation System with Low-Dynamic Movement 