Your Equation

Library / Structural dynamics and vibration testing / SDY-31

Structural dynamics and vibration testing

H1 transfer estimate

Frequency response estimate from the cross-spectrum Syx of input and output divided by the input autospectrum Sxx.

Ref
SDY-31
Rev
v1
Field
Structural dynamics and vibration testing
Result
|H1| [m/N]

The H1 estimate is the cross-spectrum of output against input divided by the input autospectrum, H₁ = Syx/Sxx. It is unbiased when there is no noise on the input and the output noise is uncorrelated with the input, and it is biased low where noise enters the force channel. This entry gives its magnitude; the derived values give its real and imaginary parts and phase.

Frequency response estimate from the cross-spectrum Syx of input and output divided by the input autospectrum Sxx. It is the right choice when the input is clean and the output carries the noise. This entry returns its magnitude.

Calculator

Solve for
m/N
m·N/Hz
−55
m·N/Hz
−55
N²/Hz
0.15
  • Real part of H12 m/N
  • Imaginary part of H12 m/N
  • Phase angle45 °

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Magnitude of the H1 estimate (m/N) current value 2.828 m/N
SxxInput autospectrumKey driver
0.56628.3
Re SyxReal part of the cross-spectrum
25.39
Im SyxImaginary part of the cross-spectrum
25.39
  • The estimate has magnitude 2.828 m/N and phase 45°.
  • Pair H1 with the coherence: where the coherence drops, treat the value as unreliable.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (m/N)Local stepChange in result
Sxx Input autospectrum0.1 to 5 N²/Hz0.565728.2827.72+10%−9.09 %
Re Syx Real part of the cross-spectrum−5 to 5 m·N/Hz25.3853.385+0.2 m·N/Hz+5.12 %
Im Syx Imaginary part of the cross-spectrum−5 to 5 m·N/Hz25.3853.385+0.2 m·N/Hz+5.12 %

Sweep of Input autospectrum

Input autospectrum (N²/Hz)Magnitude of the H1 estimate (m/N)
0.128.28
0.71253.97
1.3252.135
1.9381.46
2.551.109
3.1630.8944
3.7750.7493
4.3880.6447
50.5657

Sweep one variable

Magnitude of the H1 estimate (m/N)Hover, touch, or use the arrow keys on the chart
051015202530 12345 Input autospectrum (N²/Hz) now 2.828

Variables and how each one contributes

|H1|

Magnitude of the H1 estimate

Result · m/N

What the equation gives you. Everything else feeds it.

Re Syx

Real part of the cross-spectrum

m·N/Hz · typical −5 to 5

The real part of the averaged cross-spectrum of output against input at one frequency, in m·N/Hz. Raises the magnitude of the estimate. Raising it by 0.5 (to 2.5) moves the result by +13.2 %, from 2.828 to 3.202 m/N.

Im Syx

Imaginary part of the cross-spectrum

m·N/Hz · typical −5 to 5

The imaginary part of the cross-spectrum, in m·N/Hz. It sets the phase of the estimate. Raises the magnitude of the estimate. Raising it by 0.5 (to 2.5) moves the result by +13.2 %, from 2.828 to 3.202 m/N.

Sxx

Input autospectrum

N²/Hz · typical 0.1 to 5

The averaged input autospectrum, in N²/Hz. It must be positive. A larger input spectrum lowers the estimate. Raising it by 10 % (to 1.1) moves the result by −9.09 %, from 2.828 to 2.571 m/N.

Worked example with the values above

  1. Cross-spectrum magnitude: |Sᵧₓ| = √(2² + 2²) = 2.8284.
  2. Divide by the input autospectrum 1.
  3. |H₁| = 2.8284 m/N.

Assumptions and limits

  • Averaged spectra from the same records, windows and frequency bin, with a stationary, linear system.
  • At least several averages are used, because a single unaveraged record gives a coherence of one at every frequency.

Common mistakes

  • Using H1 where the force channel is noisy, which biases the peak low, or H2 where the output is noisy.
  • Reading frequency response values where the coherence is low.
  • Forgetting the 90° and 180° phase changes when converting between receptance, mobility and accelerance.

Statistics and uncertainty

Spectral estimates carry random error that falls as the square root of the number of averages and bias that depends on leakage and noise. Quote the number of averages, and read the coherence before relying on any frequency response value.

Where it is used

  • Estimating frequency response functions from impact hammer and shaker tests.
  • Converting between displacement, velocity and acceleration responses for modal fitting and coupling.

Maths you need

  • Cross-spectrum: the averaged product of one signal and the conjugate of another
  • Complex numbers: real and imaginary parts, magnitude and phase
  • Frequency response function: output per unit input at each frequency

Related formulas

Practise this formula