Originally Posted by D H
Another way to express that 15 microns/second/sqrt(second) requirement from post #1 is 15 microns/second2*sqrt(second). In terms of g (9.80665 m/s2), that is about 1.5 micro-g*sqrt(sec). You need an extremely sensitive and noise-free accelerometer here! This is verging on nano-g accelerometer territory.
Per Honeywell's specs (see http://www.inertialsensor.com/qa3000.shtml), the intrinsic noise from a QA 3000 is 7 micro-g*sqrt(sec) at low frequencies, 70 micro-g*sqrt(sec) at midlevel frequencies, and 1500 micro-g*sqrt(sec) at high frequencies. Not even close to the < 2 micro-g*sqrt(sec) your application needs, even if you can reliably filter out the high frequency components.
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That was the initial way I went about looking at this once the units made sense to me. But, I happen to know this spec was written such that the QA3000 passes, so that drove me to keep researching.
I came across an IEEE standard (IEEE 952-1997, annex C.1.1, "angle random walk" -- it was written for gyros). It associates rate noise PSD (S(f)) with random walk (N) by the equation: S(f) = N
2. We're filtering out everything above 300Hz (and the PSD happens to have a zero-slope portion, ie white noise), so I found N like this: N = sqrt(S(f)) = sqrt(S(300Hz)) = 12.58 (micro-m/s)/sqrt(s).
It still doesn't entirely make sense why exactly it would work that way, but that's what I get from the IEEE standard... any ideas?