Satellite/Inertial Navigation Integrated Navigation Method Based on Improved Kalman Filtering Algorithm

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/misy/volume-2022/4627111/figures/4627111.fig.006a.svgz" name="4627111.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>North position and velocity error</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/misy/volume-2022/4627111/figures/4627111.fig.006b.svgz" name="4627111.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>West position and velocity error</td></tr></table>

<div>Velocity and position errors within 30 s of navigation for east and west systems.</div>

Mobile Information Systems

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Figure 6

Figure 6: Satellite/Inertial Navigation Integrated Navigation Method Based on Improved Kalman Filtering Algorithm 