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Priority to JP13411084UpriorityCriticalpatent/JPS6151600U/ja
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Error of an inertial navigation system designed on the basis of an azimuth gyrocompass(Error analysis for inertial navigation system using azimuth gyrocompass and directional gyroscope)
Tests of aircraft navigation for small area mapping using minimum local aids to navigation(Flight tests of air navigation equipment to determine accuracy of position location for small area mapping and aerial reconnaissance in Arctic regions)[Final Report]
Strapdown platforms using redundant two-degree-of-freedom gyros(Characteristics of strapdown inertial platforms using redundant two degree of freedom gyros)
