NASA NTRS · 19730008985
General test plan redundant sensor strapdown IMU evaluation program
Abstract
The general test plan for a redundant sensor strapdown inertial measuring unit evaluation program is presented. The inertial unit contains six gyros and three orthogonal accelerometers. The software incorporates failure detection and correction logic and a land vehicle navigation program. The principal objective of the test is a demonstration of the practicability, reliability, and performance of the inertial measuring unit with failure detection and correction in operational environments.
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Hartwell, T., Irwin, H. A., Miyatake, Y., Wedekind, D. E.. 1971-11-08. General test plan redundant sensor strapdown IMU evaluation program. https://ntrs.nasa.gov/citations/19730008985
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