NASA NTRS · 19750010237
Multiple IMU system development, volume 1
Abstract
A redundant gimballed inertial system is described. System requirements and mechanization methods are defined and hardware and software development is described. Failure detection and isolation algorithms are presented and technology achievements described. Application of the system as a test tool for shuttle avionics concepts is outlined.
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Landey, M., Mckern, R.. 1974-12-01. Multiple IMU system development, volume 1. https://ntrs.nasa.gov/citations/19750010237
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