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15.4 Performance Specification
Proper selection and integration of sensors and transducers are crucial in “instrumenting” a vibrating
system. The response variable that is being measured (for example, acceleration) is termed the
measurand. A measuring device passes through two stages in making a measurement. First, the
measurand is sensed. Then, the measured signal is transduced (converted) into a form that is particularly
suitable for signal conditioning, processing, or recording. Often, the output from the transducer stage is
an electrical signal. It is common practice to identify the combined sensor– transducer unit as either a
sensor or a transducer.
The measuring device itself might contain some of the signal-conditioning circuitry and recording (or
display) devices or meters. These are components of an overall measuring system. For our purposes, we
shall consider these components separately.
In most applications, the following four variables are particularly useful in determining the response
and structural integrity of a vibrating system (in each case the usual measuring devices are indicated in
parentheses):
1. Displacement (potentiometer or LVDT)
2. Velocity (tachometer)
3. Acceleration (accelerometer)
4. Stress and strain (strain gage)
It is somewhat common practice to measure acceleration first and then determine velocity and
displacement by direct integration. Any noise and DC components in the measurement, however, could
give rise to erroneous results in such cases. Consequently, it is good practice to measure displacement,
velocity, and acceleration by using separate sensors, particularly when the measurements are employed
in feedback control of the vibratory system. It is not recommended to differentiate a displacement
(or velocity) signal to obtain velocity (or acceleration), because this process would amplify any noise
present in the measured signal. Consider, for example, a sinusoidal signal give by A sin vt: Since
d=dtðA sin vtÞ ¼ Av cos vt; it follows that any high-frequency noise would be amplified by a factor
proportional to its frequency. Also, any discontinuities in noise components would produce large
deviations in the results. Using the same argument, it may be concluded that the acceleration
measurements are desirable for high-frequency signals and the displacement measurements are desirable
for low-frequency signals. It follows that the selection of a particular measurement transducer should
depend on the frequency content of the useful portion of the measured signal.
Transducers are divided into two broad categories: active transducers and passive transducers. Passive
transducers do not require an external electric source for activation. Some examples are electromagnetic,
piezoelectric, and photovoltaic transducers. Active transducers, however, do not possess selfcontained
energy sources and thus need external activation. A good example is a resistive transducer, such as a
potentiometer.
In selecting a particular transducer (measuring device) for a specific vibration application, special
attention should be give to its ratings, which usually are provided by the manufacturer, and the required
performance specifications as provided by the customer (or developed by the system designer).
Vibration Instrumentation 15-21
© 2005 by Taylor & Francis Group, LLC
15.4.1 Parameters for Performance Specification
A perfect measuring device can be defined as one that possesses the following characteristics:
1. Output instantly reaches the measured value (fast response).
2. Transducer output is sufficiently large (high gain, low output impedance, high sensitivity).
3. Output remains at the measured value (without drifting or being affected by environmental effects
and other undesirable disturbances and noise) unless the measurand itself changes (stability and
robustness).
4. The output signal level of the transducer varies in proportion to the signal level of the measurand
(static linearity).
5. Connection of a measuring device does not distort the measurand itself (loading effects are absent
and impedances are matched).
6. Power consumption is small (high input impedance).
All these properties are based on dynamic characteristics and therefore can be explained in terms
of dynamic behavior of the measuring device. In particular, items 1 to 4 can be specified in terms of the
device (response), either in the time domain or in the frequency domain. Items 2, 5, and 6 can be specified
using the impedance characteristics of a device. First, we shall discuss response characteristics that are
important in performance specification of a sensor/transducer unit.
15.4.1.1 Time-Domain Specifications
Several parameters that are useful for the time-domain performance specification of a device are as
follows:
1. Rise time ðTrÞ: This is the time taken to pass the steady-state value of the response for the first time.
In overdamped systems, the response is nonoscillatory; consequently, there is no overshoot. So
that the definition is valid for all systems, rise time is often defined as the time taken to pass 90% of
the steady-state value for the first time. Rise time is often measured from 10% of the steady-state
value in order to leave out irregularities occurring at start-up and time lags that might be present
in a system. Rise time represents the speed of response of a device: a small rise time indicates a fast
response.
2. Delay time (Td): This is usually defined as the time taken to reach 50% of the steady-state value for
the first time. This parameter is also a measure of the speed of response.
3. Peak time (Tp): This is the time at the first peak. This parameter also represents the speed of
response of the device.
4. Settling time (Ts): This is the time taken for the device response to settle down within a certain
percentage (e.g., ^2%) of the steady-state value. This parameter is related to the degree of
damping present in the device as well as the degree of stability.
5. Percentage overshoot (PO): This is defined as
PO ¼ 100ðMp 2 1Þ% ð15:30Þ
using the normalized-to-unity step response curve, where Mp is the peak value. Percentage
overshoot is a measure of damping or relative stability in the device.
6. Steady-state error: This is the deviation of the actual steady-state value from the desired value.
Steady-state error may be expressed as a percentage with respect to the (desired) steady-state
value. In a measuring device, steady-state error manifests itself as an offset. This is a systematic
(deterministic) error that normally can be corrected by recalibration. In servo-controlled
devices, steady-state error can be reduced by increasing the loop gain or by introducing a lag
compensation. Steady-state error can be completely eliminated using the integral control (reset)
action.
15-22 Vibration and Shock Handbook
© 2005 by Taylor & Francis Group, LLC
For the best performance of a measuring device, we wish to have the values of all the foregoing
parameters as small as possible. In actual practice, however, it might be difficult to meet all specifications,
particularly under conflicting requirements. For instance, Tr can be decreased by increasing the dominant
natural frequency vn of the device. This, however, increases the PO and sometimes the Ts. On the other
hand, the PO and Ts can be decreased by increasing device damping, but this has the undesirable effect of
increasing Tr.
15.4.1.2 Frequency-Domain Specifications
Since any time signal can be decomposed into sinusoidal components through Fourier transformation, it
is clear that the response of a system to an arbitrary input excitation also can be determined using
transfer-function (frequency response-function) information for that system. For this reason, one could
argue that it is redundant to use both time-domain specifications and frequency-domain specifications,
as they carry the same information. Often, however, both specifications are used simultaneously, because
this can provide a better understanding of the system performance. Frequency-domain parameters are
more suitable in representing some characteristics of a system under some types of excitation.
Consider a device with the frequency-response function (transfer function) Gð jvÞ: Some useful
parameters for performance specification of the device in the frequency domain are:
1. Useful frequency range (operating interval): This is given by the flat region of the frequency
response magnitude, lGð jvÞl; of the device.
2. Bandwidth (speed of response): This may be represented by the primary natural frequency (or
resonant frequency) of the device.
3. Static gain (steady-state performance): Since static conditions correspond to zero frequencies; this
is given by Gð0Þ:
4. Resonant frequency (speed and critical frequency region) vr: This corresponds to the lowest
frequency at which lGð jvÞl peaks.
5. Magnitude at resonance (stability): This is given by lGðjvr Þl:
6. Input impedance (loading, efficiency, interconnectability): This represents the dynamic resistance
as felt at the input terminals of the device. This parameter will be discussed in more detail under
component interconnection and matching.
7. Output impedance (loading, efficiency, interconnectability): This represents the dynamic
resistance as felt at the output terminals of the device.
8. Gain margin (stability): This is the amount by which the device gain could be increased before the
system becomes unstable.
9. Phase margin (stability): This is the amount by which the device phase lead could be decreased
(i.e., phase lag increased) before the system becomes unstable.
15.4.2 Linearity
A device is considered linear if it can be modeled by linear differential equations, with time t as the
independent variable. Nonlinear devices are often analyzed using linear techniques by considering small
excursions about an operating point. This linearization is accomplished by introducing incremental
variables for the excitations (inputs) and responses (outputs). If one increment can cover the entire
operating range of a device with sufficient accuracy, it is an indication that the device is linear. If the
input/output relations are nonlinear algebraic equations, that represents a static nonlinearity. Such a
situation can be handled simply by using nonlinear calibration curves, which linearize the device without
introducing nonlinearity errors. If, on the other hand, the input/output relations are nonlinear
differential equations, analysis usually becomes quite complex. This situation represents a dynamic
nonlinearity.
Transfer-function representation is a “linear” model of an instrument. Hence, it implicitly assumes
linearity. According to industrial terminology, a linear measuring instrument provides a measured value
that varies linearly with the value of the measurand. This is consistent with the definition of static linearity.
Vibration Instrumentation 15-23
© 2005 by Taylor & Francis Group, LLC
All physical devices are nonlinear to some degree. This stems from any deviation from the ideal behavior,
due to causes such as saturation, deviation from Hooke’s Law in elastic elements, Coulomb friction, creep
at joints, aerodynamic damping, backlash in gears and other loose components, and component wearout.
Nonlinearities in devices are often manifested as some peculiar characteristics. In particular, the following
properties are important in detecting nonlinear behavior in dynamic systems:
1. Saturation: The response does not increase when the excitation is increased beyond some level.
This may result from such causes as magnetic saturation, which is common in transformer devices
such as differential transformers, plasticity in mechanical components, or nonlinear deformation
in springs.
2. Hysteresis: In this case, the input/output curve changes depending on the direction of motion,
resulting in a hysteresis loop. This is common in: loose components such as gears, which have
backlash; in components with nonlinear damping, such as Coulomb friction; and in magnetic
devices with ferromagnetic media and various dissipative mechanisms (e.g., eddy current
dissipation).
3. The jump phenomenon: Some nonlinear devices exhibit an instability known as the jump
phenomenon (or fold catastrophe). Here, the frequency response (transfer) function curve suddenly
jumps in magnitude at a particular frequency, while the excitation frequency is increased
or decreased. A device with this nonlinearity will exhibit a characteristic “tilt” of its resonant
peak either to the left (softening nonlinearity) or to the right (hardening nonlinearity).
Furthermore, the transfer function itself may change with the level of input excitation in the case
of nonlinear devices.
4. Limit cycles: A limit cycle is a closed trajectory in the state space that corresponds to sustained
oscillations without decay or growth. The amplitude of these oscillations is independent of the
location at which the response began. In the case of a stable limit cycle, the response will return to the
limit cycle irrespective of the location near the limit cycle from which the response was initiated. In
the case of an unstable limit cycle, the response will steadily move away from the location with the
slightest disturbance.
5. Frequency creation: At steady state, nonlinear devices can create frequencies that are not present in
the excitation signals. These frequencies might be harmonics (integer multiples of the excitation
frequency), subharmonics (integer fractions of the excitation frequency), or nonharmonics (usually
rational fractions of the excitation frequency).
Several methods are available to reduce or eliminate nonlinear behavior in vibrating systems. They
include calibration (in the static case), use of linearizing elements, such as resistors and amplifiers to
neutralize the nonlinear effects, and the use of nonlinear feedback. It is also good practice to take the
following precautions:
1. Avoid operating the device over a wide range of signal levels.
2. Avoid operation over a wide frequency band.
3. Use devices that do not generate large mechanical motions.
4. Minimize Coulomb friction.
5. Avoid loose joints and gear coupling (i.e., use direct-drive mechanisms).
15.4.3 Instrument Ratings
Instrument manufacturers do not usually provide complete dynamic information for their products. In
most cases, it is unrealistic to expect complete dynamic models (in the time or the frequency domain)
and associated parameter values for complex instruments. Performance characteristics provided by
manufacturers and vendors are primarily static parameters. Known as instrument ratings, these are
available as parameter values, tables, charts, calibration curves, and empirical equations. Dynamic
characteristics such as transfer functions (e.g., transmissibility curves expressed with respect to excitation
15-24 Vibration and Shock Handbook
© 2005 by Taylor & Francis Group, LLC
frequency) might also be provided for more sophisticated instruments, but the available dynamic
information is never complete. Furthermore, the definitions of rating parameters used by manufacturers
and vendors of instruments are in some cases not the same as analytical definitions used in textbooks.
This is particularly true in relation to the term linearity. Nevertheless, instrument ratings provided by
manufacturers and vendors are very useful in the selection, installation, operation, and maintenance of
instruments. Some of these performance parameters are indicated below.
15.4.3.1 Rating Parameters
Typical rating parameters supplied by instrument manufacturers are:
1. Sensitivity
2. Dynamic range
3. Resolution
4. Linearity
5. Zero drift and full-scale drift
6. Useful frequency range
7. Bandwidth
8. Input and output impedances
The conventional definitions given by instrument manufacturers and vendors are summarized below.
Sensitivity of a transducer is measured by the magnitude (peak, root-mean-square [RMS] value, etc.)
of the output signals corresponding to a unit input of the measurand. This may be expressed as the ratio
of (incremental output)/(incremental input) or, analytically, as the corresponding partial derivative. In
the case of vectorial or tensorial signals (e.g., displacement, velocity, acceleration, strain, force), the
direction of sensitivity should be specified.
Cross-sensitivity is the sensitivity along directions that are orthogonal to the direction of primary
sensitivity; it is expressed as a percentage of the direct sensitivity. High sensitivity and low crosssensitivity
are desirable for measuring instruments. Sensitivity to parameter changes, disturbances, and
noise has to be small in any device, however; this is an indication of its robustness. Often, sensitivity
and robustness are conflicting requirements.
Dynamic range of an instrument is determined by the allowed lower and upper limits of its input or
output (response) so as to maintain a required level of measurement accuracy. This range is usually
expressed as a ratio, in decibels. In many situations, the lower limit of the dynamic range is equal to
the resolution of the device. Hence, the dynamic range is usually expressed as the ratio (range of
operation)/(resolution), in decibels.
Resolution is the smallest change in a signal that can be detected and accurately indicated by a
transducer, a display unit, or other instrument. It is usually expressed as a percentage of the maximum
range of the instrument or as the inverse of the dynamic range ratio, as defined above. It follows that
dynamic range and resolution are very closely related.
Linearity is determined by the calibration curve of an instrument. The curve of output amplitude
(a peak or rms value) vs. input amplitude under static conditions within the dynamic range of an
instrument is known as the static calibration curve. Its closeness to a straight line measures the degree of
linearity. Manufacturers provide this information either as the maximum deviation of the calibration
curve from the least squares straight-line fit of the calibration curve or from some other reference straight
line. If the least squares fit is used as the reference straight line, the maximum deviation is called
independent linearity (or more correctly, the independent nonlinearity, because the larger the deviation,
the greater the nonlinearity). Nonlinearity may be expressed as a percentage of either the actual reading at
an operating point or the full-scale reading.
Zero drift is defined as the drift from the null reading of the instrument when the measurand is
maintained steady for a long period. Note that in this case, the measurand is kept at zero or any other
level that corresponds to null reading of the instrument. Similarly, full-scale drift is defined with respect to
the full-scale reading (the measurand is maintained at the full-scale value). Usual causes of drift include
Vibration Instrumentation 15-25
© 2005 by Taylor & Francis Group, LLC
instrument instability (e.g., instability in amplifiers), ambient changes (e.g., changes in temperature,
pressure, humidity, and vibration level), changes in power supply (e.g., changes in reference DC voltage
or alternating current [AC] line voltage), and parameter changes in an instrument (due to aging,
wearout, nonlinearities, etc.). Drift due to parameter changes that are caused by instrument
nonlinearities is known as parametric drift, sensitivity drift, or scale-factor drift. For example, a change
in spring stiffness or electrical resistance due to changes in ambient temperature results in a parametric
drift. Note that the parametric drift depends on the measurand level. Zero drift, however, is assumed to
be the same at any measurand level if the other conditions are kept constant. For example, a change in
reading caused by thermal expansion of the readout mechanism due to changes in the ambient
temperature is considered a zero drift. In electronic devices, drift can be reduced by using AC circuitry
rather than direct current (DC) circuitry. For example, AC-coupled amplifiers have fewer drift problems
than DC amplifiers. Intermittent checking for the instrument response level for zero input is a popular
way to calibrate for zero drift. In digital devices, this can be done automatically and intermittently,
between sample points, when the input signal can be bypassed without affecting the system operation.
Useful frequency range corresponds to the interval of both flat gain and zero phase in the frequency
response characteristics of an instrument. The maximum frequency in this band is typically less than half
(say, one fifth of) the dominant resonant frequency of the instrument. This is a measure of instrument
bandwidth.
Bandwidth of an instrument determines the maximum speed or frequency at which the instrument is
capable of operating. High bandwidth implies faster speed of response. Bandwidth is determined by the
dominant natural frequency, vn; or the dominant resonant frequency, vr; of the transducer. (Note: For
low damping, vr is approximately equal to vn.) It is inversely proportional to the rise time and the
dominant time constant. Half-power bandwidth is also a useful parameter. Instrument bandwidth must
be several times greater than the maximum frequency of interest in the measured signal. The bandwidth
of a measuring device is important, particularly when measuring transient signals. Note that the
bandwidth is directly related to the useful frequency range.
15.4.4 Accuracy and Precision
The instrument ratings mentioned above affect the overall accuracy of an instrument. Accuracy can be
assigned either to a particular reading or to an instrument. Note that instrument accuracy depends not
only on the physical hardware of the instrument but also on the operating conditions (e.g., design
conditions that are the normal, steady operating conditions or extreme transient conditions, such
as emergency start-up and shutdown). Measurement accuracy determines the closeness of the
measured value to the true value. Instrument accuracy is related to the worst accuracy obtainable
within the dynamic range of the instrument in a specific operating environment. Measurement error is
defined as
Error ¼ ðmeasured valueÞ 2 ðtrue valueÞ ð15:31Þ
Correction, which is the negative of error, is defined as
Correction ¼ ðtrue valueÞ 2 ðmeasured valueÞ ð15:32Þ
Each of these can also be expressed as a percentage of the true value. The accuracy of an instrument may
be determined by measuring a parameter whose true value is known, and is near the extremes of the
dynamic range of the instrument, under certain operating conditions. For this purpose, standard
parameters or signals that can be generated at very high levels of accuracy would be needed. The National
Institute for Standards and Testing (NIST) is usually responsible for the generation of these standards.
Nevertheless, accuracy and error values cannot be determined to 100% exactness in typical applications,
because the true value is not known. In a given situation, we can only make estimates for accuracy,
by using ratings provided by the instrument manufacturer or by analyzing data from previous
measurements and models.
15-26 Vibration and Shock Handbook
© 2005 by Taylor & Francis Group, LLC
Causes of error include instrument instability, external noise (disturbances), poor calibration,
inaccurate information (e.g., poor analytical models, inaccurate control), parameter changes (e.g., due
to environmental changes, aging, and wearout), unknown nonlinearities, and improper use of the
instrument.
Errors can be classified as deterministic (or systematic) and random (or stochastic). Deterministic errors
are those caused by well-defined factors, including nonlinearities and offsets in readings. These usually
can be removed by applying proper calibration and analytical practices. Error ratings and calibration
charts are used to remove systematic errors from instrument readings. Random errors are caused by
uncertain factors entering into the instrument response. These include device noise, line noise, and the
effects of unknown random variations in the operating environment. A statistical analysis using
sufficiently large amounts of data is necessary to estimate random errors. The results are usually
expressed as a mean error, which is the systematic part of random error, and a standard deviation or
confidence interval for instrument response.
Precision is not synonymous with accuracy. Reproducibility (or repeatability) of an instrument reading
determines the precision of an instrument. Two or more identical instruments that have the same high
offset error might be able to generate responses at high precision, even though these readings are clearly
inaccurate. For example, consider a timing device (clock) that very accurately indicates time increments
(say, up to the nearest microsecond). If the reference time (starting time) is set incorrectly, the time
readings will be in error, even though the clock has a very high precision.
Instrument error may be represented by a random variable that has a mean value me and a
standard deviation se. If the standard deviation is zero, the variable is considered deterministic. In
that case, the error is said to be deterministic or repeatable. Otherwise, the error is said to be random.
The precision of an instrument is determined by the standard deviation of error in the instrument
response. Readings of an instrument may have a large mean value of error (e.g., large offset), but if
the standard deviation is small, the instrument has a high precision. Hence, a quantitative definition
for precision is
Precision ¼ ðmeasurement rangeÞ=se ð15:33Þ
Lack of precision originates from random causes and poor construction practices. It cannot be
compensated for by recalibration, just as the precision of a clock cannot be improved by resetting the
time. On the other hand, accuracy can be improved by recalibration. Repeatable (deterministic)
accuracy is inversely proportional to the magnitude of the mean error me.
In selecting instruments for a particular application, in addition to matching instrument ratings with
specifications, several additional features should be considered. These include geometric limitations
(size, shape, etc.); environmental conditions (e.g., chemical reactions including corrosion, extreme
temperatures, light, dirt accumulation, electromagnetic fields, radioactive environments, shock and
vibration); power requirements; operational simplicity; availability; the past record and reputation
of the manufacturer and of the particular instrument; and cost-related economic aspects (initial cost,
maintenance cost, cost of supplementary components such as signal-conditioning and processing
devices, design life and associated frequency of replacement, and cost of disposal and replacement).
Often, these considerations become the ultimate deciding factors in the selection process.
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