NASA NTRS ยท 19720000091
Control of acceleration in sine/random vibration tests
Abstract
Sampling output levels of accelerometers using largest output or any combination of outputs provide control of shaker for spacecraft vibration qualification tests.
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Woodbury, R. C.. 1972-01-01. Control of acceleration in sine/random vibration tests. https://ntrs.nasa.gov/citations/19720000091
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