NASA NTRS · 19680056561
Design approach for reducing gyro-induced errors in strapdown inertial systems.
Abstract
Single degree of freedom integrating gyro in strapdown inertial systems, discussing error reduction
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Gelb, A., Sutherland, A. A., Jr.. 1968-08-01. Design approach for reducing gyro-induced errors in strapdown inertial systems.. https://ntrs.nasa.gov/citations/19680056561
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