Flight Vibration Survey

Use when you must reduce an in-flight vibration survey: extract the per-rev order amplitudes from measured accelerometer time histories with a synchronous DFT over integer-revolution windows, compute the windowed total RMS survey level, combine the order components by root-sum-square, and gate each survey point against the declared vibration limit and the 1P trim limit. Produces the per-order amplitudes, the total level, the RSS check, and the pass or needs-trim verdicts for rotorcraft main-rotor track-and-balance and airframe vibration limits, and for fixed-wing vibration or buzz surveys. Trigger: vibration survey, track and balance, per-rev order, order analysis, synchronous DFT, rotor balance survey, 1P trim.

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