Stepwise fusion algorithm with dual correction for multi-sensor navigation
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DOI: 10.1177/1729881418779931
Abstract: In high-altitude, long-endurance unmanned aerial vehicles, a celestial attitude determination system is used to enhance the inertial navigation system (INS)/global positioning system (GPS) to achieve the required attitude performance. The traditional federal filter is not… read more here.
Keywords: system; error; attitude determination; navigation ... See more keywords