In order to detect signals we search for threshold crossings of the -statistic over the intrinsic parameter
space. Once we have a threshold crossing we need to find the precise location of the maximum of
in order to estimate accurately the parameters of the signal. A satisfactory procedure is the
two-step procedure. The first step is a coarse search where we evaluate
on a coarse grid in
parameter space and locate threshold crossings. The second step, called fine search, is a refinement
around the region of parameter space where the maximum identified by the coarse search is
located.
There are two methods to perform the fine search. One is to refine the grid around the threshold
crossing found by the coarse search [70, 68, 91, 88], and the other is to use an optimization routine to find
the maximum of [49
, 60
]. As initial value to the optimization routine we input the values of the
parameters found by the coarse search. There are many maximization algorithms available. One useful
method is the Nelder–Mead algorithm [61] which does not require computation of the derivatives of the
function being maximized.
Usually the grid in parameter space is very large and it is important to calculate the optimum statistic as
efficiently as possible. In special cases the -statistic given by Equation (35
) can be further simplified.
For example, in the case of coalescing binaries
can be expressed in terms of convolutions
that depend on the difference between the time-of-arrival (TOA) of the signal and the TOA
parameter of the filter. Such convolutions can be efficiently computed using Fast Fourier Transforms
(FFTs). For continuous sources, like gravitational waves from rotating neutron stars observed
by ground-based detectors [49
] or gravitational waves form stellar mass binaries observed by
space-borne detectors [60
], the detection statistic
involves integrals of the general form
In order to test the performance of the maximization method of the statistic it is useful to perform
Monte Carlo simulations of the parameter estimation and compare the variances of the estimators with
the variances calculated from the Fisher matrix. Such simulations were performed for various
gravitational-wave signals [55, 19, 49
]. In these simulations we observe that above a certain
signal-to-noise ratio, that we call the threshold signal-to-noise ratio, the results of the Monte Carlo
simulations agree very well with the calculations of the rms errors from the inverse of the Fisher
matrix. However, below the threshold signal-to-noise ratio they differ by a large factor. This
threshold effect is well-known in signal processing [96]. There exist more refined theoretical bounds
on the rms errors that explain this effect, and they were also studied in the context of the
gravitational-wave signal from a coalescing binary [72
]. Use of the Fisher matrix in the assessment
of the parameter estimators has been critically examined in [95
] where a criterion has been
established for signal-to-noise ratio above which the inverse of the Fisher matrix approximates well
covariance of the estimators of the parameters. Update
Here we present a simple model that explains the deviations from the covariance matrix and reproduces well the results of the Monte Carlo simulations. The model makes use of the concept of the elementary cell of the parameter space that we introduced in Section 4.5.2. The calculation given below is a generalization of the calculation of the rms error for the case of a monochromatic signal given by Rife and Boorstyn [81].
When the values of parameters of the template that correspond to the maximum of the functional
fall within the cell in the parameter space where the signal is present, the rms error is satisfactorily
approximated by the inverse of the Fisher matrix. However, sometimes as a result of noise
the global maximum is in the cell where there is no signal. We then say that an outlier has
occurred. In the simplest case we can assume that the probability density of the values of the
outliers is uniform over the search interval of a parameter, and then the rms error is given by
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