Long-term monitoring of the STS-2 self-noise

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Long-term monitoring of the STS-2 self-noise an experiment in the Conrad Observatory, Austria Reinoud Sleeman (1) , Peter Melichar (2) KNMI, Netherlands, sleeman@knmi.nl ZAMG, Austria, melichar@zamg.ac.at

Introduction and motivation Outline Introduction and motivation Side-by-side correlation technique (2 channels, 3 channels) PSD estimate and representation Synthetic experiments: exploring the triplet technique Potential source of error: sensor mis-alignment Initial real experiments, choice of digitizer Conrad experiment Results Conclusions and recommendations Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Seismic background noise (m/s2) power spectral density Introduction and motivation Seismic background noise (m/s2) power spectral density measured at seismic station Heimansgroeve (HGN), Netherlands during 2002: 302- 309 and 2003: 029 - 043 STS-2 STS-1 N-S E-W Z Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Low noise model STS-2 noise level from: STS-2 manual Introduction and motivation from: STS-2 manual Low noise model STS-2 noise level Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Johnson-Mathiesen seismometer > 1 Hz STS-1 < 0.01 Hz STS-2 noise (Wielandt, 1991)

Motivation for determining instrumental noise: bias of data by the recording system selection of instrumentation improving installation conditions

How to determine instrumental noise of digitizers or seismic sensors ? Side-by-side correlation technique How to determine instrumental noise of digitizers or seismic sensors ? digitizer: shorted input recording ( e.g. 50 ohm resistor ) sensor: common input recording ( side by side test ) coherency analysis of 2 channels ( Holcomb, 1989 ) coherency analysis of 3 channels - triplet ( Sleeman et. al., 2006 ) Holcomb, L. G., A direct method for calculating instrument noise levels in side-by-side seismometer evaluations. U.S. Geol. Surv., Open-File Report 89-214 (1989) Sleeman, R., A. van Wettum and J. Trampert. Three-channel correlation analysis: a new technique to measure instrumental noise of digitizers and seismic sensors. Bull. Seism. Soc. Am., 96, 1, 258-271 (2006) Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Conventional 2-channel correlation Side-by-side correlation technique Conventional 2-channel correlation time domain frequency domain Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

a better approach: 3-channel correlation Side-by-side correlation technique a better approach: 3-channel correlation Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Side-by-side correlation technique Model equations Relative gains (transfer functions) can be estimated from output cross spectra only ! Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Self-noise PSD can be estimated from output recordings only ! Side-by-side correlation technique Model equations Self-noise PSD can be estimated from output recordings only ! Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

3-channel correlation method (triplet method): Side-by-side correlation technique 3-channel correlation method (triplet method): direct method for estimating system noise and relative transfer functions based on the recordings only no a-priori information required about transfer functions or their accuracy; method is not sensitive for errors in gain reliable technique, up to 120 dB SNR no quiet site required (in theory) ! Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Powers Spectrum Density (PSD) estimation (Welch, 1978) PSD estimate and representation Instrumental self noise is non-deterministic, stochastic signal  Power Spectral Density Powers Spectrum Density (PSD) estimation (Welch, 1978) 50 % overlapping time sections tapering (Hanning window) autocorrelation Fourier transform averaging over the number of time sections one-sided PSD (USGS noise models) instrument response deconvolution (to acceleration) PSD smoothing over 1/10-th of a decade Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

A=1e3 A=1e4 A=1e5 A=1e6 120 dB common input: seismic recording Synthetic experiments common input: seismic recording self noise: white noise (rms = 1) sampling rate: 1 sps  theoretical self noise: 3 dB output gain self noise common input A=1e3 A=1e4 A=1e5 A=1e6 120 dB output extracted “self-noise” 3 dB Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Self noise extraction possible up to about 120 dB SNR ! Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

3-channel coherency analysis requires identical alignment and Sensor misalignment 3-channel coherency analysis requires identical alignment and levelling of the 3 sensors STS-2 sensor Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Synthetic experiment sensors with alignment and/or levelling errors Sensor misalignment Synthetic experiment sensors with alignment and/or levelling errors Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

for small alignment/tilting errors: Sensor misalignment for small alignment/tilting errors: self noise extraction possible only up to about ~40-60 dB SNR ! output PSD PSD self-noise - - alignment or tilting error (~10 ) theoretical self-noise Initial experiments in De Bilt (KNMI) showed that sites with high background noise levels are not suitable for self-noise measurements, using the 3-channel technique. Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Which datalogger is suitable for measuring the STS-2 self-noise ? Initial experiment with STS-2 + Q330 dataloggers Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Initial experiments PSD in dB ( rel. to V 2 / Hz ) extracted noise

Initial experiments PSD in dB ( rel. to V 2 / Hz ) extracted noise

Initial experiments PSD in dB ( rel. to V 2 / Hz ) extracted noise

Initial experiments PSD in dB ( rel. to V 2 / Hz ) extracted noise

Initial experiments PSD in dB ( rel. to V 2 / Hz ) extracted noise Q330HR STS-2 self noise measurement needs Q330HR !

The Conrad Observatory Experiment Conrad experiment The Conrad Observatory Experiment NERIES framework (TA5) - funding Conrad Observatory - quiet conditions 4 STS-2 (same generation) 3 aligned, 1 mis-aligned (2, 4, 8 degrees) 4 Q330-HR, enabled pre-amplifier Antelope acquisition

Conrad experiment Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Conrad experiment Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Conrad experiment Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Conrad experiment Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Seismic PSD LNM Wielandt (STS-2) Triplet (STS-2) 12 dB ! Results Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

use vertical component ! Results Z comp N comp E comp use vertical component !

Results 3 Z components differences up to 5 dB

Seismic PSD Triplet (STS-2) Results Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Results Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Q330-HR with enabled pre-amplifier required for estimating Conclusions Q330-HR with enabled pre-amplifier required for estimating the self-noise of the STS-2. Quiet site required, only vertical components. STS-2 self-noise is ~12 dB below previous estimates (> 1 Hz ) and is in agreement with Wielandt between 0.01 and 1 Hz. Coherency is lost below 0.05 Hz ( in present installation ) Long-term analysis required instead of window shopping. Relatively large differences between individual sensors High and low frequency spurious signals. Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Possible contributing sources: Barometric pressure variations (ground tilt, elastic response ) Temperature variations Humidity (corrosion) Installation conditions (mechanical strees in the pier) Quantization noise of digitizer Sensor self-noise (instrumental noise) Brownian motion of the mass (thermal noise) Displacement transducer noise Integrator noise (semi-conductors) Electromagnetic noise of the displacement sensor (LVDT) : Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements

Effects of temperature variations Thermal expansion of leaf spring (and other components) Temperature dependence of elasic moduli of leaf spring Thermal stresses due to uneven heating Thermal stresses due to differing expansion coefficients of different metalic components Convection of enclosed air due to dissipated heat from feedback electronics Tilting due to uneven heating and expansion of foot screws Thermal stresses in pier => Privide additional thermal shielding and increase thermal inertia. Reinoud Sleeman, Peter Melichar IASPEI, 2009, Cape Town STS-2 self-noise measurements