NASA NTRS · 19710000086
Performance evaluation system for inertial navigation equipment
Abstract
Testing system studies inertial characteristics of gyroscopic devices. System consisting of instrument support package, dynamic test table, torque control electronics, and real-time computer evaluates performance of prototype gyroscopic strapdown units in inertial-grade attitude-reference systems. System is applicable to commercial aircraft.
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Mc Kern, R. A.. 1971-04-01. Performance evaluation system for inertial navigation equipment. https://ntrs.nasa.gov/citations/19710000086
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