int
main( int argc, char **argv )
{
int arg; /* command-line argument counter */
BOOLEAN xyz = 0; /* whether -x, -y, or -z options were given */
INT4 verbosity = 0; /* verbosity level */
REAL8 x_1 = 0.0, x_2 = 0.0, dx; /* range and increment in x */
REAL8 y_1 = 0.0, y_2 = 0.0, dy; /* range and increment in y */
REAL8 z_1 = 0.0, z_2 = 0.0, dz; /* range and increment in z */
INT4 nx = 1, ny = 1, nz = 1; /* number of steps in each direction */
INT4 i, j, k; /* index in each direction */
REAL8 x, y, z, ddx, ddy, ddz; /* position and error in each direction */
REAL8 ddr, ddmax = 0.0; /* overall and maximum position error */
static LALStatus stat; /* status structure */
EarthPosition earth; /* terrestrial coordinates */
/*******************************************************************
* PARSE ARGUMENTS (arg stores the current position) *
*******************************************************************/
arg = 1;
while ( arg < argc ) {
/* Parse range options. */
if ( !strcmp( argv[arg], "-x" ) ) {
if ( argc > arg + 3 ) {
arg++;
xyz = 1;
x_1 = atof( argv[arg++] );
x_2 = atof( argv[arg++] );
nx = atoi( argv[arg++] );
} else {
ERROR( GEOCENTRICGEODETICTESTC_EARG,
GEOCENTRICGEODETICTESTC_MSGEARG, 0 );
LALPrintError( USAGE, *argv );
return GEOCENTRICGEODETICTESTC_EARG;
}
} else if ( !strcmp( argv[arg], "-y" ) ) {
if ( argc > arg + 3 ) {
arg++;
xyz = 1;
y_1 = atof( argv[arg++] );
y_2 = atof( argv[arg++] );
ny = atoi( argv[arg++] );
} else {
ERROR( GEOCENTRICGEODETICTESTC_EARG,
GEOCENTRICGEODETICTESTC_MSGEARG, 0 );
LALPrintError( USAGE, *argv );
return GEOCENTRICGEODETICTESTC_EARG;
}
} else if ( !strcmp( argv[arg], "-z" ) ) {
if ( argc > arg + 3 ) {
arg++;
xyz = 1;
z_1 = atof( argv[arg++] );
z_2 = atof( argv[arg++] );
nz = atoi( argv[arg++] );
} else {
ERROR( GEOCENTRICGEODETICTESTC_EARG,
GEOCENTRICGEODETICTESTC_MSGEARG, 0 );
LALPrintError( USAGE, *argv );
return GEOCENTRICGEODETICTESTC_EARG;
}
}
/* Parse verbosity option. */
else if ( !strcmp( argv[arg], "-v" ) ) {
if ( argc > arg + 1 ) {
arg++;
verbosity = atoi( argv[arg++] );
} else {
ERROR( GEOCENTRICGEODETICTESTC_EARG,
GEOCENTRICGEODETICTESTC_MSGEARG, 0 );
LALPrintError( USAGE, *argv );
return GEOCENTRICGEODETICTESTC_EARG;
}
}
/* Parse debug level option. */
else if ( !strcmp( argv[arg], "-d" ) ) {
if ( argc > arg + 1 ) {
arg++;
} else {
ERROR( GEOCENTRICGEODETICTESTC_EARG,
GEOCENTRICGEODETICTESTC_MSGEARG, 0 );
LALPrintError( USAGE, *argv );
return GEOCENTRICGEODETICTESTC_EARG;
}
}
/* Check for unrecognized options. */
else if ( argv[arg][0] == '-' ) {
ERROR( GEOCENTRICGEODETICTESTC_EARG,
GEOCENTRICGEODETICTESTC_MSGEARG, 0 );
LALPrintError( USAGE, *argv );
return GEOCENTRICGEODETICTESTC_EARG;
}
} /* End of argument parsing loop. */
/*******************************************************************
* SET PARAMETERS *
*******************************************************************/
/* If none of -x, -y, -z were given, generate a random position. */
if ( !xyz ) {
REAL4 lon, coslat, sinlat, rad; /* polar coordinates */
RandomParams *rparams = NULL; /* pseudorandom sequence parameters */
SUB( LALCreateRandomParams( &stat, &rparams, 0 ), &stat );
SUB( LALUniformDeviate( &stat, &lon, rparams ), &stat );
lon *= LAL_TWOPI;
SUB( LALUniformDeviate( &stat, &sinlat, rparams ), &stat );
coslat = sqrt( 1.0 - sinlat*sinlat );
SUB( LALUniformDeviate( &stat, &rad, rparams ), &stat );
rad = 1.5*rad + 0.5;
x_1 = x_2 = rad*coslat*cos( lon );
y_1 = y_2 = rad*coslat*sin( lon );
z_1 = z_2 = rad*sinlat;
SUB( LALDestroyRandomParams( &stat, &rparams ), &stat );
}
/* Compute stepsizes. */
dx = dy = dz = 0.0;
if ( nx > 1 )
dx = ( x_2 - x_1 )/( nx - 1.0 );
if ( ny > 1 )
dy = ( y_2 - y_1 )/( ny - 1.0 );
if ( nz > 1 )
dz = ( z_2 - z_1 )/( nz - 1.0 );
/*******************************************************************
* PERFORM TEST *
*******************************************************************/
/* Loop over each direction. */
for ( i = 0; i < nx; i++ ) {
x = LAL_REARTH_SI*( x_1 + i*dx );
for ( j = 0; j < ny; j++ ) {
y = LAL_REARTH_SI*( y_1 + j*dy );
for ( k = 0; k < nz; k++ ) {
z = LAL_REARTH_SI*( z_1 + k*dz );
/* Do transformation. */
earth.x = x;
earth.y = y;
earth.z = z;
SUB( LALGeocentricToGeodetic( &stat, &earth ), &stat );
SUB( LALGeodeticToGeocentric( &stat, &earth ), &stat );
/* Compute difference. */
ddx = x - earth.x;
ddy = y - earth.y;
ddz = z - earth.z;
ddr = sqrt( ddx*ddx + ddy*ddy + ddz*ddz );
if ( ddr > ddmax )
ddmax = ddr;
if ( verbosity == 1 )
fprintf( stdout, "%+23.16e\n", ddr );
else if ( verbosity == 2 )
fprintf( stdout, "%+23.16e %+23.16e\n", earth.elevation, ddr );
else if ( verbosity == 3 )
fprintf( stdout, "%+23.16e %+23.16e %+23.16e %+23.16e\n",
x, y, z, ddr );
else if ( verbosity == 4 )
fprintf( stdout, "%+23.16e %+23.16e %+23.16e"
" %+23.16e %+23.16e %+23.16e %+23.16e\n", x, y, z,
earth.elevation, LAL_180_PI*earth.geodetic.latitude,
LAL_180_PI*earth.geodetic.longitude, ddr );
}
}
}
/* Print maximum. */
fprintf( stdout, "Maximum error: %.16em\n", ddmax );
if ( !xyz && ddmax > 1.0e-6 ) {
ERROR( GEOCENTRICGEODETICTESTC_ETEST,
GEOCENTRICGEODETICTESTC_MSGETEST, 0 );
return GEOCENTRICGEODETICTESTC_ETEST;
}
LALCheckMemoryLeaks();
INFO( GEOCENTRICGEODETICTESTC_MSGENORM );
return GEOCENTRICGEODETICTESTC_ENORM;
}
/**
* \author Creighton, T. D.
*
* \brief Computes the response of a detector to a coherent gravitational wave.
*
* This function takes a quasiperiodic gravitational waveform given in
* <tt>*signal</tt>, and estimates the corresponding response of the
* detector whose position, orientation, and transfer function are
* specified in <tt>*detector</tt>. The result is stored in
* <tt>*output</tt>.
*
* The fields <tt>output-\>epoch</tt>, <tt>output->deltaT</tt>, and
* <tt>output-\>data</tt> must already be set, in order to specify the time
* period and sampling rate for which the response is required. If
* <tt>output-\>f0</tt> is nonzero, idealized heterodyning is performed (an
* amount \f$2\pi f_0(t-t_0)\f$ is subtracted from the phase before computing
* the sinusoid, where \f$t_0\f$ is the heterodyning epoch defined in
* \c detector). For the input signal, <tt>signal-\>h</tt> is ignored,
* and the signal is treated as zero at any time for which either
* <tt>signal-\>a</tt> or <tt>signal-\>phi</tt> is not defined.
*
* This routine will convert <tt>signal-\>position</tt> to equatorial
* coordinates, if necessary.
*
* ### Algorithm ###
*
* The routine first accounts for the time delay between the detector and
* the solar system barycentre, based on the detector position
* information stored in <tt>*detector</tt> and the propagation direction
* specified in <tt>*signal</tt>. Values of the propagation delay are
* precomuted at fixed intervals and stored in a table, with the
* intervals \f$\Delta T_\mathrm{delay}\f$ chosen such that the value
* interpolated from adjacent table entries will never differ from the
* true value by more than some timing error \f$\sigma_T\f$. This implies
* that:
* \f[
* \Delta T_\mathrm{delay} \leq \sqrt{
* \frac{8\sigma_T}{\max\{a/c\}} } \; ,
* \f]
* where \f$\max\{a/c\}=1.32\times10^{-10}\mathrm{s}^{-1}\f$ is the maximum
* acceleration of an Earth-based detector in the barycentric frame. The
* total propagation delay also includes Einstein and Shapiro delay, but
* these are more slowly varying and thus do not constrain the table
* spacing. At present, a 400s table spacing is hardwired into the code,
* implying \f$\sigma_T\approx3\mu\f$s, comparable to the stated accuracy of
* <tt>LALBarycenter()</tt>.
*
* Next, the polarization response functions of the detector
* \f$F_{+,\times}(\alpha,\delta)\f$ are computed for every 10 minutes of the
* signal's duration, using the position of the source in <tt>*signal</tt>,
* the detector information in <tt>*detector</tt>, and the function
* <tt>LALComputeDetAMResponseSeries()</tt>. Subsequently, the
* polarization functions are estimated for each output sample by
* interpolating these precomputed values. This guarantees that the
* interpolated value is accurate to \f$\sim0.1\%\f$.
*
* Next, the frequency response of the detector is estimated in the
* quasiperiodic limit as follows:
* <ul>
* <li> At each sample point in <tt>*output</tt>, the propagation delay is
* computed and added to the sample time, and the instantaneous
* amplitudes \f$A_1\f$, \f$A_2\f$, frequency \f$f\f$, phase \f$\phi\f$, and polarization
* shift \f$\Phi\f$ are found by interpolating the nearest values in
* <tt>signal-\>a</tt>, <tt>signal-\>f</tt>, <tt>signal-\>phi</tt>, and
* <tt>signal-\>shift</tt>, respectively. If <tt>signal-\>f</tt> is not
* defined at that point in time, then \f$f\f$ is estimated by differencing
* the two nearest values of \f$\phi\f$, as \f$f\approx\Delta\phi/2\pi\Delta
* t\f$. If <tt>signal-\>shift</tt> is not defined, then \f$\Phi\f$ is treated as
* zero.</li>
* <li> The complex transfer function of the detector the frequency \f$f\f$
* is found by interpolating <tt>detector-\>transfer</tt>. The amplitude of
* the transfer function is multiplied with \f$A_1\f$ and \f$A_2\f$, and the
* phase of the transfer function is added to \f$\phi\f$,</li>
* <li> The plus and cross contributions \f$o_+\f$, \f$o_\times\f$ to the
* detector output are computed as in \eqref{eq_quasiperiodic_hpluscross}
* of \ref PulsarSimulateCoherentGW_h, but
* using the response-adjusted amplitudes and phase.</li>
* <li> The final detector response \f$o\f$ is computed as
* \f$o=(o_+F_+)+(o_\times F_\times)\f$.</li>
* </ul>
*
* ### A note on interpolation: ###
*
* Much of the computational work in this routine involves interpolating
* various time series to find their values at specific output times.
* The algorithm is summarized below.
*
* Let \f$A_j = A( t_A + j\Delta t_A )\f$ be a sampled time series, which we
* want to resample at new (output) time intervals \f$t_k = t_0 + k\Delta
* t\f$. We first precompute the following quantities:
* \f{eqnarray}{
* t_\mathrm{off} & = & \frac{t_0-t_A}{\Delta t_A} \; , \\
* dt & = & \frac{\Delta t}{\Delta t_A} \; .
* \f}
* Then, for each output sample time \f$t_k\f$, we compute:
* \f{eqnarray}{
* t & = & t_\mathrm{off} + k \times dt \; , \\
* j & = & \lfloor t \rfloor \; , \\
* f & = & t - j \; ,
* \f}
* where \f$\lfloor x\rfloor\f$ is the "floor" function; i.e.\ the largest
* integer \f$\leq x\f$. The time series sampled at the new time is then:
* \f[
* A(t_k) = f \times A_{j+1} + (1-f) \times A_j \; .
* \f]
*
* ### Notes ###
*
* The major computational hit in this routine comes from computing the
* sine and cosine of the phase angle in
* \eqref{eq_quasiperiodic_hpluscross} of
* \ref PulsarSimulateCoherentGW_h. For better online performance, these can
* be replaced by other (approximate) trig functions. Presently the code
* uses the native \c libm functions by default, or the function
* <tt>sincosp()</tt> in \c libsunmath \e if this function is
* available \e and the constant \c ONLINE is defined.
* Differences at the level of 0.01 begin to appear only for phase
* arguments greater than \f$10^{14}\f$ or so (corresponding to over 500
* years between phase epoch and observation time for frequencies of
* around 1kHz).
*
* To activate this feature, be sure that <tt>sunmath.h</tt> and
* \c libsunmath are on your system, and add <tt>-DONLINE</tt> to the
* <tt>--with-extra-cppflags</tt> configuration argument. In future this
* flag may be used to turn on other efficient trig algorithms on other
* (non-Solaris) platforms.
*
*/
void
LALPulsarSimulateCoherentGW( LALStatus *stat,
REAL4TimeSeries *output,
PulsarCoherentGW *CWsignal,
PulsarDetectorResponse *detector )
{
INT4 i, n; /* index over output->data, and its final value */
INT4 nMax; /* used to store limits on index ranges */
INT4 fInit, fFinal; /* index range for which CWsignal->f is defined */
INT4 shiftInit, shiftFinal; /* ditto for CWsignal->shift */
UINT4 dtDelayBy2; /* delay table half-interval (s) */
UINT4 dtPolBy2; /* polarization table half-interval (s) */
REAL4 *outData; /* pointer to output data */
REAL8 delayMin, delayMax; /* min and max values of time delay */
SkyPosition source; /* source sky position */
BOOLEAN transfer; /* 1 if transfer function is specified */
BOOLEAN fFlag = 0; /* 1 if frequency left detector->transfer range */
BOOLEAN pFlag = 0; /* 1 if frequency was estimated from phase */
/* get delay table and polaristion tables half intervals if defined (>0) in
the PulsarCoherentGW structure otherwise default to 400s for dtDelatBy2 and 300s
for dtPolBy2 */
dtDelayBy2 = CWsignal->dtDelayBy2 > 0 ? CWsignal->dtDelayBy2 : 400;
dtPolBy2 = CWsignal->dtPolBy2 > 0 ? CWsignal->dtPolBy2 : 300;
/* The amplitude, frequency, phase, polarization shift, polarization
response, and propagation delay are stored in arrays that must be
interpolated. For a quantity x, we define a pointer xData to the
data array. At some time t measured in units of output->deltaT,
the interpolation point in xData is given by ( xOff + t*xDt ),
where xOff is an offset and xDt is a relative sampling rate. */
LALDetAMResponseSeries polResponse;
REAL8Vector *delay = NULL;
REAL4 *aData, *fData, *shiftData, *plusData, *crossData;
REAL8 *phiData, *delayData;
REAL8 aOff, fOff, phiOff, shiftOff, polOff, delayOff;
REAL8 aDt, fDt, phiDt, shiftDt, polDt, delayDt;
/* Frequencies in the detector transfer function are interpolated
similarly, except everything is normalized with respect to
detector->transfer->deltaF. */
REAL4Vector *aTransfer = NULL;
REAL4Vector *phiTransfer = NULL;
REAL4Vector *phiTemp = NULL;
REAL4 *aTransData = NULL, *phiTransData = NULL;
REAL8 f0 = 1.0;
REAL8 phiFac = 1.0, fFac = 1.0;
/* Heterodyning phase factor LAL_TWOPI*output->f0*output->deltaT,
and phase offset at the start of the series
LAL_TWOPI*output->f0*(time offset). */
REAL8 heteroFac, phi0;
/* Variables required by the TCENTRE() macro, above. */
REAL8 realIndex;
INT4 intIndex;
REAL8 indexFrac;
INITSTATUS(stat);
ATTATCHSTATUSPTR( stat );
/* Make sure parameter structures and their fields exist. */
ASSERT( CWsignal, stat, SIMULATECOHERENTGWH_ENUL,
SIMULATECOHERENTGWH_MSGENUL );
if ( !( CWsignal->a ) ) {
ABORT( stat, SIMULATECOHERENTGWH_ESIG,
SIMULATECOHERENTGWH_MSGESIG );
}
ASSERT( CWsignal->a->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( CWsignal->a->data->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
if ( !( CWsignal->phi ) ) {
ABORT( stat, SIMULATECOHERENTGWH_ESIG,
SIMULATECOHERENTGWH_MSGESIG );
}
ASSERT( CWsignal->phi->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( CWsignal->phi->data->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
if ( CWsignal->f ) {
ASSERT( CWsignal->f->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( CWsignal->f->data->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
}
if ( CWsignal->shift ) {
ASSERT( CWsignal->shift->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( CWsignal->shift->data->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
}
ASSERT( detector, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
if ( ( transfer = ( detector->transfer != NULL ) ) ) {
ASSERT( detector->transfer->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( detector->transfer->data->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
}
ASSERT( output, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( output->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
ASSERT( output->data->data, stat,
SIMULATECOHERENTGWH_ENUL, SIMULATECOHERENTGWH_MSGENUL );
/* Check dimensions of amplitude array. */
ASSERT( CWsignal->a->data->vectorLength == 2, stat,
SIMULATECOHERENTGWH_EDIM, SIMULATECOHERENTGWH_MSGEDIM );
/* Make sure we never divide by zero. */
ASSERT( CWsignal->a->deltaT != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
ASSERT( CWsignal->phi->deltaT != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
aDt = output->deltaT / CWsignal->a->deltaT;
phiDt = output->deltaT / CWsignal->phi->deltaT;
ASSERT( aDt != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
ASSERT( phiDt != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
if ( CWsignal->f ) {
ASSERT( CWsignal->f->deltaT != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
fDt = output->deltaT / CWsignal->f->deltaT;
ASSERT( fDt != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
} else
fDt = 0.0;
if ( CWsignal->shift ) {
ASSERT( CWsignal->shift->deltaT != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
shiftDt = output->deltaT / CWsignal->shift->deltaT;
ASSERT( shiftDt != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
} else
shiftDt = 0.0;
if ( transfer ) {
ASSERT( detector->transfer->deltaF != 0.0, stat,
SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
fFac = 1.0 / detector->transfer->deltaF;
phiFac = fFac / ( LAL_TWOPI*CWsignal->phi->deltaT );
f0 = detector->transfer->f0/detector->transfer->deltaF;
}
heteroFac = LAL_TWOPI*output->f0*output->deltaT;
phi0 = (REAL8)( output->epoch.gpsSeconds -
detector->heterodyneEpoch.gpsSeconds );
phi0 += 0.000000001*(REAL8)( output->epoch.gpsNanoSeconds -
detector->heterodyneEpoch.gpsNanoSeconds );
phi0 *= LAL_TWOPI*output->f0;
if ( phi0 > 1.0/LAL_REAL8_EPS ) {
LALWarning( stat, "REAL8 arithmetic is not sufficient to maintain"
" heterodyne phase to within a radian." );
}
/* Check units on input, and set units on output. */
{
ASSERT( XLALUnitCompare( &(CWsignal->f->sampleUnits), &lalHertzUnit ) == 0, stat, SIMULATECOHERENTGWH_EUNIT, SIMULATECOHERENTGWH_MSGEUNIT );
ASSERT( XLALUnitCompare( &(CWsignal->phi->sampleUnits), &lalDimensionlessUnit ) == 0, stat, SIMULATECOHERENTGWH_EUNIT, SIMULATECOHERENTGWH_MSGEUNIT );
if( CWsignal->shift ) {
ASSERT( XLALUnitCompare( &(CWsignal->shift->sampleUnits), &lalDimensionlessUnit ) == 0, stat, SIMULATECOHERENTGWH_EUNIT, SIMULATECOHERENTGWH_MSGEUNIT );
}
if ( transfer ) {
if ( XLALUnitMultiply( &(output->sampleUnits), &(CWsignal->a->sampleUnits), &(detector->transfer->sampleUnits) ) == NULL ) {
ABORT( stat, SIMULATECOHERENTGWH_EUNIT, SIMULATECOHERENTGWH_MSGEUNIT );
}
} else {
output->sampleUnits = CWsignal->a->sampleUnits;
}
snprintf( output->name, LALNameLength, "response to %s", CWsignal->a->name );
}
/* Define temporary variables to access the data of CWsignal->a,
CWsignal->f, and CWsignal->phi. */
aData = CWsignal->a->data->data;
INT4 aLen = CWsignal->a->data->length * CWsignal->a->data->vectorLength;
phiData = CWsignal->phi->data->data;
INT4 phiLen = CWsignal->phi->data->length;
outData = output->data->data;
INT4 fLen=0, shiftLen=0;
if ( CWsignal->f )
{
fData = CWsignal->f->data->data;
fLen = CWsignal->f->data->length;
}
else
{
fData = NULL;
}
if ( CWsignal->shift )
{
shiftData = CWsignal->shift->data->data;
shiftLen = CWsignal->shift->data->length;
}
else
{
shiftData = NULL;
}
/* Convert source position to equatorial coordinates, if
required. */
if ( detector->site ) {
source = CWsignal->position;
if ( source.system != COORDINATESYSTEM_EQUATORIAL ) {
ConvertSkyParams params; /* parameters for conversion */
EarthPosition location; /* location of detector */
params.gpsTime = &( output->epoch );
params.system = COORDINATESYSTEM_EQUATORIAL;
if ( source.system == COORDINATESYSTEM_HORIZON ) {
params.zenith = &( location.geodetic );
location.x = detector->site->location[0];
location.y = detector->site->location[1];
location.z = detector->site->location[2];
TRY( LALGeocentricToGeodetic( stat->statusPtr, &location ),
stat );
}
TRY( LALConvertSkyCoordinates( stat->statusPtr, &source,
&source, ¶ms ), stat );
}
}
/* Generate the table of propagation delays.
dtDelayBy2 = (UINT4)( 38924.9/sqrt( output->f0 +
1.0/output->deltaT ) ); */
delayDt = output->deltaT/( 2.0*dtDelayBy2 );
nMax = (UINT4)( output->data->length*delayDt ) + 3;
TRY( LALDCreateVector( stat->statusPtr, &delay, nMax ), stat );
delayData = delay->data;
/* Compute delay from solar system barycentre. */
if ( detector->site && detector->ephemerides ) {
LIGOTimeGPS gpsTime; /* detector time when we compute delay */
EarthState state; /* Earth position info at that time */
BarycenterInput input; /* input structure to LALBarycenter() */
EmissionTime emit; /* output structure from LALBarycenter() */
/* Arrange nested pointers, and set initial values. */
gpsTime = input.tgps = output->epoch;
gpsTime.gpsSeconds -= dtDelayBy2;
input.tgps.gpsSeconds -= dtDelayBy2;
input.site = *(detector->site);
for ( i = 0; i < 3; i++ )
input.site.location[i] /= LAL_C_SI;
input.alpha = source.longitude;
input.delta = source.latitude;
input.dInv = 0.0;
delayMin = delayMax = 1.1*LAL_AU_SI/( LAL_C_SI*output->deltaT );
delayMax *= -1;
/* Compute table. */
for ( i = 0; i < nMax; i++ ) {
REAL8 tDelay; /* propagation time */
LALBarycenterEarth( stat->statusPtr, &state, &gpsTime,
detector->ephemerides );
BEGINFAIL( stat )
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
ENDFAIL( stat );
LALBarycenter( stat->statusPtr, &emit, &input, &state );
BEGINFAIL( stat )
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
ENDFAIL( stat );
delayData[i] = tDelay = emit.deltaT/output->deltaT;
if ( tDelay < delayMin )
delayMin = tDelay;
if ( tDelay > delayMax )
delayMax = tDelay;
gpsTime.gpsSeconds += 2*dtDelayBy2;
input.tgps.gpsSeconds += 2*dtDelayBy2;
}
}
/* No information from which to compute delays. */
else {
LALInfo( stat, "Detector site and ephemerides absent; simulating hplus with no"
" propagation delays" );
memset( delayData, 0, nMax*sizeof(REAL8) );
delayMin = delayMax = 0.0;
}
/* Generate the table of polarization response functions. */
polDt = output->deltaT/( 2.0*dtPolBy2 );
nMax = (UINT4)( output->data->length*polDt ) + 3;
memset( &polResponse, 0, sizeof( LALDetAMResponseSeries ) );
polResponse.pPlus = (REAL4TimeSeries *)
LALMalloc( sizeof(REAL4TimeSeries) );
polResponse.pCross = (REAL4TimeSeries *)
LALMalloc( sizeof(REAL4TimeSeries) );
polResponse.pScalar = (REAL4TimeSeries *)
LALMalloc( sizeof(REAL4TimeSeries) );
if ( !polResponse.pPlus || !polResponse.pCross ||
!polResponse.pScalar ) {
if ( polResponse.pPlus )
LALFree( polResponse.pPlus );
if ( polResponse.pCross )
LALFree( polResponse.pCross );
if ( polResponse.pScalar )
LALFree( polResponse.pScalar );
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
ABORT( stat, SIMULATECOHERENTGWH_EMEM,
SIMULATECOHERENTGWH_MSGEMEM );
}
memset( polResponse.pPlus, 0, sizeof(REAL4TimeSeries) );
memset( polResponse.pCross, 0, sizeof(REAL4TimeSeries) );
memset( polResponse.pScalar, 0, sizeof(REAL4TimeSeries) );
LALSCreateVector( stat->statusPtr, &( polResponse.pPlus->data ),
nMax );
BEGINFAIL( stat ) {
LALFree( polResponse.pPlus );
LALFree( polResponse.pCross );
LALFree( polResponse.pScalar );
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
} ENDFAIL( stat );
LALSCreateVector( stat->statusPtr, &( polResponse.pCross->data ),
nMax );
BEGINFAIL( stat ) {
TRY( LALSDestroyVector( stat->statusPtr,
&( polResponse.pPlus->data ) ), stat );
LALFree( polResponse.pPlus );
LALFree( polResponse.pCross );
LALFree( polResponse.pScalar );
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
} ENDFAIL( stat );
LALSCreateVector( stat->statusPtr, &( polResponse.pScalar->data ),
nMax );
BEGINFAIL( stat ) {
TRY( LALSDestroyVector( stat->statusPtr,
&( polResponse.pPlus->data ) ), stat );
TRY( LALSDestroyVector( stat->statusPtr,
&( polResponse.pCross->data ) ), stat );
LALFree( polResponse.pPlus );
LALFree( polResponse.pCross );
LALFree( polResponse.pScalar );
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
} ENDFAIL( stat );
plusData = polResponse.pPlus->data->data;
crossData = polResponse.pCross->data->data;
INT4 plusLen = polResponse.pPlus->data->length;
INT4 crossLen = polResponse.pCross->data->length;
if ( plusLen != crossLen ) {
XLALPrintError ("plusLen = %d != crossLen = %d\n", plusLen, crossLen );
ABORT ( stat, SIMULATECOHERENTGWH_EBAD, SIMULATECOHERENTGWH_MSGEBAD );
}
if ( detector->site ) {
LALSource polSource; /* position and polarization angle */
LALDetAndSource input; /* response input structure */
LALTimeIntervalAndNSample params; /* response parameter structure */
/* Arrange nested pointers, and set initial values. */
polSource.equatorialCoords = source;
polSource.orientation = (REAL8)( CWsignal->psi );
input.pSource = &polSource;
input.pDetector = detector->site;
params.epoch = output->epoch;
params.epoch.gpsSeconds -= dtPolBy2;
params.deltaT = 2.0*dtPolBy2;
params.nSample = nMax;
/* Compute table of responses. */
LALComputeDetAMResponseSeries( stat->statusPtr, &polResponse,
&input, ¶ms );
BEGINFAIL( stat ) {
TRY( LALSDestroyVector( stat->statusPtr,
&( polResponse.pPlus->data ) ), stat );
TRY( LALSDestroyVector( stat->statusPtr,
&( polResponse.pCross->data ) ), stat );
TRY( LALSDestroyVector( stat->statusPtr,
&( polResponse.pScalar->data ) ), stat );
LALFree( polResponse.pPlus );
LALFree( polResponse.pCross );
LALFree( polResponse.pScalar );
TRY( LALDDestroyVector( stat->statusPtr, &delay ), stat );
} ENDFAIL( stat );
} else {
