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RealWave Pocket Analyser

RealWave Pocket Analyser
The Realwave Pocket Analyser is a handheld, PDA-based analyser that addresses many applications including realtime FFT analysis, spectrograms, octave analysis, vibration level meter with human vibration filter, sound level meter & FFT based RPM meter. And prices start from just £1385. Click here to find out more.

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DATS : Capture, Analyze, Report

DATS is one of the leading software packages for the capture, analysis and reporting of technical and scientific data of all types. It includes time and frequency domain analyses as well as special solution packs to address specific applications such as NVH testing, rotating machinery analysis, acoustic measurement, human response to vibration and so on.

Software NVH Rotating Machinery Noise Vibration Capture Analyze report

DATS Flight Test Analysis Software (01-55-889)

Noise Vibration Harshness NVH
  • Flutter Analysis
  • Acoustic & Vibration Analysis
  • Stability Analysis
  • In-flight & Post-flight Options
  • Fully Automated & Scripted

The Prosig Flight Test Software covers standard vibration and acoustic analysis as well as specific analyses for modal flutter analysis and stability analysis. The software is designed to operate either in real-time (in-flight) mode taking data from a telemetry server, or in off-line (post-flight) mode taking input data from stored media.

Flutter Analysis

Flutter Analysis is primarily concerned with measuring the damped vibrations at the major resonance frequencies while the aircraft is in flight and tracking the changes in behavior with increasing speed. Essentially this is a form of modal analysis and can be performed either in the frequency domain (Potter method) or time domain (Eigen Realisation of Direct Correlations). The frequency-based method is completely automated in the sense that it is the software that decides which are the dominant modes of interest, whereas with time-based method the user chooses the main modes based on results presented in the form of a stability plot.

 





Stability Analysis

The structural behavior at a response point on an aircraft when subjected to a forced excitation can be analyzed as a Transfer Function in the frequency domain. When this data is displayed as a Nyquist plot (real versus imaginary) it gives clear insight into the stability of the response characteristics close to resonances.


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DATS Flight Test Analysis Software
01-55-889 Flight Test Analysis Software (requires 01-55-622 DATS Professional)