/**
* Extract multi detector-info from a given multi SFTCatalog view
*/
int
XLALMultiLALDetectorFromMultiSFTCatalogView ( MultiLALDetector *multiIFO, //!< [out] list of detectors found in catalog
const MultiSFTCatalogView *multiView //!< [in] multi-IFO view of SFT catalog
)
{
// check input consistency
XLAL_CHECK ( multiIFO != NULL, XLAL_EINVAL );
XLAL_CHECK ( multiView != NULL, XLAL_EINVAL );
UINT4 numIFOs = multiView->length;
XLAL_CHECK ( (numIFOs > 0) && (numIFOs <= PULSAR_MAX_DETECTORS), XLAL_EINVAL );
multiIFO->length = numIFOs;
for ( UINT4 X=0; X < numIFOs; X ++ )
{
LALDetector *site;
XLAL_CHECK ( (site = XLALGetSiteInfo ( multiView->data[X].data->header.name )) != NULL, XLAL_EFUNC );
multiIFO->sites[X] = (*site); // struct-copy
XLALFree ( site );
} /* for X < numIFOs */
return XLAL_SUCCESS;
} /* XLALMultiLALDetectorFromMultiSFTCatalogView() */
/**
* Parse string-vectors (typically input by user) of N detector-names
* for detectors \f$X=1\ldots N\f$, returns a MultiLALDetector struct
*
*/
int
XLALParseMultiLALDetector ( MultiLALDetector *detInfo, /**< [out] parsed detector-info struct */
const LALStringVector *detNames /**< [in] list of detector names */
)
{
XLAL_CHECK ( detInfo != NULL, XLAL_EINVAL );
XLAL_CHECK ( detNames != NULL, XLAL_EINVAL );
UINT4 numDet = detNames->length;
XLAL_CHECK ( (numDet > 0) && (numDet <= PULSAR_MAX_DETECTORS), XLAL_EINVAL );
detInfo->length = numDet;
/* parse input strings and fill detInfo */
for ( UINT4 X = 0; X < numDet; X ++ )
{
LALDetector *ifo;
/* first parse detector name */
XLAL_CHECK ( (ifo = XLALGetSiteInfo ( detNames->data[X] ) ) != NULL, XLAL_EINVAL, "Failed to parse detector-name '%s'\n", detNames->data[X] );
detInfo->sites[X] = (*ifo); // struct copy
XLALFree ( ifo );
} /* for X < numDet */
return XLAL_SUCCESS;
} /* XLALParseMultiLALDetector() */
/**
* basic initializations: deal with user input and return standardized 'ConfigVariables'
*/
int
XLALInitCode ( ConfigVariables *cfg, const UserVariables_t *uvar, const char *app_name)
{
if ( !cfg || !uvar || !app_name ) {
XLALPrintError ("%s: illegal NULL pointer input.\n\n", __func__ );
XLAL_ERROR ( XLAL_EINVAL );
}
/* init ephemeris data */
XLAL_CHECK ( (cfg->edat = XLALInitBarycenter ( uvar->ephemEarth, uvar->ephemSun )) != NULL, XLAL_EFUNC );
/* convert input REAL8 time into LIGOTimeGPS */
if ( XLALGPSSetREAL8( &cfg->timeGPS, uvar->timeGPS ) == NULL ) {
XLALPrintError ("%s: failed to convert input GPS %g into LIGOTimeGPS\n", __func__, uvar->timeGPS );
XLAL_ERROR ( XLAL_EFUNC );
}
/* set up dummy timestamps vector containing just this one timestamps
* (used to interface with LALComputeAM(), LALGetAMCoeffs() and LALNewGetAMCoeffs())
*/
if ( (cfg->timestamps = XLALCreateTimestampVector( 1 )) == NULL ) {
XLALPrintError ("%s: XLALCreateTimestampVector( 1 ) failed.", __func__ );
XLAL_ERROR ( XLAL_EFUNC );
}
cfg->timestamps->data[0] = cfg->timeGPS;
/* convert detector name into site-info */
if ( ( cfg->det = XLALGetSiteInfo ( uvar->detector )) == NULL )
{
XLALPrintError ("%s: XLALGetSiteInfo('%s') failed.\n", __func__, uvar->detector );
XLAL_ERROR ( XLAL_EFUNC );
}
/* NOTE: contrary to ComputeAM() and LALGetAMCoffs(), the new function LALNewGetAMCoeffs()
* computes 'a * sinzeta' and 'b * sinzeta': for the comparison we therefore need to correct
* for GEO's opening-angle of 94.33degrees [JKS98]: */
if ( ! strcmp ( cfg->det->frDetector.name, "GEO_600" ) )
cfg->sinzeta = 0.997146;
else
cfg->sinzeta = 1;
/* convert input skyposition to radians Alpha/Delta [trivial here] */
cfg->skypos.system = COORDINATESYSTEM_EQUATORIAL;
cfg->skypos.longitude = uvar->Alpha;
cfg->skypos.latitude = uvar->Delta;
return XLAL_SUCCESS;
} /* XLALInitCode() */
/**
* Extract multi detector-info from a given multi SFTCatalog view
*/
int
XLALMultiLALDetectorFromMultiSFTs ( MultiLALDetector *multiIFO, //!< [out] list of detectors found in catalog
const MultiSFTVector *multiSFTs //!< [in] multi-IFO SFT vector
)
{
// check input consistency
XLAL_CHECK ( multiIFO != NULL, XLAL_EINVAL );
XLAL_CHECK ( multiSFTs != NULL, XLAL_EINVAL );
XLAL_CHECK ( multiSFTs->length > 0, XLAL_EINVAL );
UINT4 numIFOs = multiSFTs->length;
multiIFO->length = numIFOs;
for ( UINT4 X=0; X < numIFOs; X ++ )
{
LALDetector *site;
XLAL_CHECK ( (site = XLALGetSiteInfo ( multiSFTs->data[X]->data[0].name )) != NULL, XLAL_EFUNC );
multiIFO->sites[X] = (*site); // struct-copy
XLALFree ( site );
} /* for X < numIFOs */
return XLAL_SUCCESS;
} /* XLALMultiLALDetectorFromMultiSFTVector() */
/* ----- function definitions ---------- */
int
main ( int argc, char *argv[] )
{
LALStatus status;
UserInput_t uvar_s;
UserInput_t *uvar = &uvar_s;
INIT_MEM ( status );
INIT_MEM ( uvar_s );
struct tms buf;
uvar->randSeed = times(&buf);
// ---------- register all our user-variable ----------
XLALregBOOLUserStruct ( help, 'h', UVAR_HELP , "Print this help/usage message");
XLALregINTUserStruct ( randSeed, 's', UVAR_OPTIONAL, "Specify random-number seed for reproducible noise.");
/* read cmdline & cfgfile */
XLAL_CHECK ( XLALUserVarReadAllInput ( argc, argv ) == XLAL_SUCCESS, XLAL_EFUNC );
if ( uvar->help ) { /* if help was requested, we're done */
exit (0);
}
srand ( uvar->randSeed );
REAL8 startTimeREAL8 = 714180733;
REAL8 duration = 180000; /* 50 hours */
REAL8 Tsft = 1800; /* assume 30min SFTs */
char earthEphem[] = TEST_DATA_DIR "earth00-19-DE200.dat.gz";
char sunEphem[] = TEST_DATA_DIR "sun00-19-DE200.dat.gz";
//REAL8 tolerance = 2e-10; /* same algorithm, should be basically identical results */
LIGOTimeGPS startTime, refTime;
XLALGPSSetREAL8 ( &startTime, startTimeREAL8 );
refTime = startTime;
// pick skyposition at random ----- */
SkyPosition skypos;
skypos.longitude = LAL_TWOPI * (1.0 * rand() / ( RAND_MAX + 1.0 ) ); // alpha uniform in [0, 2pi)
skypos.latitude = LAL_PI_2 - acos ( 1 - 2.0 * rand()/RAND_MAX ); // sin(delta) uniform in [-1,1]
skypos.system = COORDINATESYSTEM_EQUATORIAL;
// pick binary orbital parameters:
// somewhat inspired by Sco-X1 parameters from S2-paper (PRD76, 082001 (2007), gr-qc/0605028)
// but with a more extreme eccentricity, and random argp
REAL8 argp = LAL_TWOPI * (1.0 * rand() / ( RAND_MAX + 1.0 ) ); // uniform in [0, 2pi)
BinaryOrbitParams orbit;
XLALGPSSetREAL8 ( &orbit.tp, 731163327 ); // time of observed periapsis passage (in SSB)
orbit.argp = argp; // argument of periapsis (radians)
orbit.asini = 1.44; // projected, normalized orbital semi-major axis (s) */
orbit.ecc = 1e-2; // relatively large value, for better testing
orbit.period = 68023; // period (s) : about ~18.9h
// ----- step 0: prepare test-case input for calling the BinarySSB-functions
// setup detectors
const char *sites[3] = { "H1", "L1", "V1" };
UINT4 numDetectors = sizeof( sites ) / sizeof ( sites[0] );
MultiLALDetector multiIFO;
multiIFO.length = numDetectors;
for ( UINT4 X = 0; X < numDetectors; X ++ )
{
LALDetector *det = XLALGetSiteInfo ( sites[X] );
XLAL_CHECK ( det != NULL, XLAL_EFUNC, "XLALGetSiteInfo ('%s') failed for detector X=%d\n", sites[X], X );
multiIFO.sites[X] = (*det); // struct copy
XLALFree ( det );
}
// load ephemeris
EphemerisData *edat = XLALInitBarycenter ( earthEphem, sunEphem );
XLAL_CHECK ( edat != NULL, XLAL_EFUNC, "XLALInitBarycenter('%s','%s') failed\n", earthEphem, sunEphem );
// setup multi-timeseries
MultiLIGOTimeGPSVector *multiTS;
XLAL_CHECK ( (multiTS = XLALCalloc ( 1, sizeof(*multiTS))) != NULL, XLAL_ENOMEM );
XLAL_CHECK ( (multiTS->data = XLALCalloc (numDetectors, sizeof(*multiTS->data))) != NULL, XLAL_ENOMEM );
multiTS->length = numDetectors;
for ( UINT4 X = 0; X < numDetectors; X ++ )
{
multiTS->data[X] = XLALMakeTimestamps ( startTime, duration, Tsft, 0 );
XLAL_CHECK ( multiTS->data[X] != NULL, XLAL_EFUNC, "XLALMakeTimestamps() failed.\n");
} /* for X < numIFOs */
// generate detector-states
MultiDetectorStateSeries *multiDetStates = XLALGetMultiDetectorStates ( multiTS, &multiIFO, edat, 0 );
XLAL_CHECK ( multiDetStates != NULL, XLAL_EFUNC, "XLALGetMultiDetectorStates() failed.\n");
// generate isolated-NS SSB times
MultiSSBtimes *multiSSBIn = XLALGetMultiSSBtimes ( multiDetStates, skypos, refTime, SSBPREC_RELATIVISTICOPT );
XLAL_CHECK ( multiSSBIn != NULL, XLAL_EFUNC, "XLALGetMultiSSBtimes() failed.\n");
// ----- step 1: compute reference-result using old LALGetMultiBinarytimes()
MultiSSBtimes *multiBinary_ref = NULL;
LALGetMultiBinarytimes (&status, &(multiBinary_ref), multiSSBIn, multiDetStates, &orbit, refTime );
XLAL_CHECK ( status.statusCode == 0, XLAL_EFAILED, "LALGetMultiBinarytimes() failed with status = %d : '%s'\n", status.statusCode, status.statusDescription );
// ----- step 2: compute test-result using new XLALAddMultiBinaryTimes()
MultiSSBtimes *multiBinary_test = NULL;
PulsarDopplerParams doppler;
memset(&doppler, 0, sizeof(doppler));
doppler.tp = orbit.tp;
doppler.argp = orbit.argp;
doppler.asini = orbit.asini;
doppler.ecc = orbit.ecc;
doppler.period = orbit.period;
XLAL_CHECK ( XLALAddMultiBinaryTimes ( &multiBinary_test, multiSSBIn, &doppler ) == XLAL_SUCCESS, XLAL_EFUNC );
// ----- step 3: compare results
REAL8 err_DeltaT, err_Tdot;
REAL8 tolerance = 1e-10;
int ret = XLALCompareMultiSSBtimes ( &err_DeltaT, &err_Tdot, multiBinary_ref, multiBinary_test );
XLAL_CHECK ( ret == XLAL_SUCCESS, XLAL_EFUNC, "XLALCompareMultiSSBtimes() failed.\n");
XLALPrintWarning ( "INFO: err(DeltaT) = %g, err(Tdot) = %g\n", err_DeltaT, err_Tdot );
XLAL_CHECK ( err_DeltaT < tolerance, XLAL_ETOL, "error(DeltaT) = %g exceeds tolerance of %g\n", err_DeltaT, tolerance );
XLAL_CHECK ( err_Tdot < tolerance, XLAL_ETOL, "error(Tdot) = %g exceeds tolerance of %g\n", err_Tdot, tolerance );
// ---- step 4: clean-up memory
XLALDestroyUserVars();
XLALDestroyEphemerisData ( edat );
XLALDestroyMultiSSBtimes ( multiBinary_test );
XLALDestroyMultiSSBtimes ( multiBinary_ref );
XLALDestroyMultiSSBtimes ( multiSSBIn );
XLALDestroyMultiTimestamps ( multiTS );
XLALDestroyMultiDetectorStateSeries ( multiDetStates );
// check for memory-leaks
LALCheckMemoryLeaks();
return XLAL_SUCCESS;
} // main()
int main(int argc, char *argv[]){
static LALStatus status;
static LALDetector *detector;
static LIGOTimeGPSVector timeV;
static REAL8Cart3CoorVector velV;
static REAL8Vector timeDiffV;
static REAL8 foft;
static HoughPulsarTemplate pulsarTemplate;
EphemerisData *edat = NULL;
CHAR *uvar_earthEphemeris = NULL;
CHAR *uvar_sunEphemeris = NULL;
SFTVector *inputSFTs = NULL;
REAL8 *alphaVec=NULL;
REAL8 *deltaVec=NULL;
REAL8 *freqVec=NULL;
REAL8 *spndnVec=NULL;
/* pgV is vector of peakgrams and pg1 is onepeakgram */
static UCHARPeakGram *pg1, **pgV;
UINT4 msp; /*number of spin-down parameters */
CHAR *uvar_ifo = NULL;
CHAR *uvar_sftDir = NULL; /* the directory where the SFT could be */
CHAR *uvar_fnameOut = NULL; /* The output prefix filename */
CHAR *uvar_fnameIn = NULL;
INT4 numberCount, ind;
UINT8 nTemplates;
UINT4 mObsCoh;
REAL8 uvar_peakThreshold;
REAL8 f_min, f_max, fWings, timeBase;
INT4 uvar_blocksRngMed;
UINT4 sftlength;
INT4 sftFminBin;
UINT4 loopId, tempLoopId;
FILE *fpOut = NULL;
CHAR *fnameLog=NULL;
FILE *fpLog = NULL;
CHAR *logstr=NULL;
/*REAL8 asq, bsq;*/ /* square of amplitude modulation functions a and b */
/******************************************************************/
/* Set up the default parameters. */
/* ****************************************************************/
/* LAL error-handler */
lal_errhandler = LAL_ERR_EXIT;
msp = 1; /*only one spin-down */
/* memory allocation for spindown */
pulsarTemplate.spindown.length = msp;
pulsarTemplate.spindown.data = NULL;
pulsarTemplate.spindown.data = (REAL8 *)LALMalloc(msp*sizeof(REAL8));
uvar_peakThreshold = THRESHOLD;
uvar_earthEphemeris = (CHAR *)LALMalloc(1024*sizeof(CHAR));
strcpy(uvar_earthEphemeris,EARTHEPHEMERIS);
uvar_sunEphemeris = (CHAR *)LALMalloc(1024*sizeof(CHAR));
strcpy(uvar_sunEphemeris,SUNEPHEMERIS);
uvar_sftDir = (CHAR *)LALMalloc(1024*sizeof(CHAR));
strcpy(uvar_sftDir,SFTDIRECTORY);
uvar_fnameOut = (CHAR *)LALMalloc(1024*sizeof(CHAR));
strcpy(uvar_fnameOut,VALIDATEOUT);
uvar_fnameIn = (CHAR *)LALMalloc(1024*sizeof(CHAR));
strcpy(uvar_fnameIn,VALIDATEIN);
uvar_blocksRngMed = BLOCKSRNGMED;
/* register user input variables */
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_ifo, "ifo", STRING, 'i', OPTIONAL, "Detector GEO(1) LLO(2) LHO(3)" ) == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_earthEphemeris, "earthEphemeris", STRING, 'E', OPTIONAL, "Earth Ephemeris file") == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_sunEphemeris, "sunEphemeris", STRING, 'S', OPTIONAL, "Sun Ephemeris file") == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_sftDir, "sftDir", STRING, 'D', OPTIONAL, "SFT Directory") == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_fnameIn, "fnameIn", STRING, 'T', OPTIONAL, "Input template file") == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_fnameOut, "fnameOut", STRING, 'o', OPTIONAL, "Output filename") == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_blocksRngMed, "blocksRngMed", INT4, 'w', OPTIONAL, "RngMed block size") == XLAL_SUCCESS, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALRegisterNamedUvar( &uvar_peakThreshold, "peakThreshold", REAL8, 't', OPTIONAL, "Peak selection threshold") == XLAL_SUCCESS, XLAL_EFUNC);
/* read all command line variables */
BOOLEAN should_exit = 0;
XLAL_CHECK_MAIN( XLALUserVarReadAllInput(&should_exit, argc, argv, lalAppsVCSInfoList) == XLAL_SUCCESS, XLAL_EFUNC);
if (should_exit)
exit(1);
/* open log file for writing */
fnameLog = LALCalloc( (strlen(uvar_fnameOut) + strlen(".log") + 10),1);
strcpy(fnameLog,uvar_fnameOut);
strcat(fnameLog,".log");
if ((fpLog = fopen(fnameLog, "w")) == NULL) {
fprintf(stderr, "Unable to open file %s for writing\n", fnameLog);
LALFree(fnameLog);
exit(1);
}
/* get the log string */
XLAL_CHECK_MAIN( ( logstr = XLALUserVarGetLog(UVAR_LOGFMT_CFGFILE) ) != NULL, XLAL_EFUNC);
fprintf( fpLog, "## Log file for HoughValidate\n\n");
fprintf( fpLog, "# User Input:\n");
fprintf( fpLog, "#-------------------------------------------\n");
fprintf( fpLog, "%s", logstr);
LALFree(logstr);
/* append an ident-string defining the exact CVS-version of the code used */
{
CHAR command[1024] = "";
fprintf (fpLog, "\n\n# CVS-versions of executable:\n");
fprintf (fpLog, "# -----------------------------------------\n");
fclose (fpLog);
sprintf (command, "ident %s | sort -u >> %s", argv[0], fnameLog);
/* we don't check this. If it fails, we assume that */
/* one of the system-commands was not available, and */
/* therefore the CVS-versions will not be logged */
if ( system(command) ) fprintf (stderr, "\nsystem('%s') returned non-zero status!\n\n", command );
LALFree(fnameLog);
}
/* open output file for writing */
fpOut= fopen(uvar_fnameOut, "w");
/*setlinebuf(fpOut);*/ /* line buffered on */
setvbuf(fpOut, (char *)NULL, _IOLBF, 0);
/*****************************************************************/
/* read template file */
/*****************************************************************/
{
FILE *fpIn = NULL;
INT4 r;
REAL8 temp1, temp2, temp3, temp4, temp5;
UINT8 templateCounter;
fpIn = fopen(uvar_fnameIn, "r");
if ( !fpIn )
{
fprintf(stderr, "Unable to fine file %s\n", uvar_fnameIn);
return DRIVEHOUGHCOLOR_EFILE;
}
nTemplates = 0;
do
{
r=fscanf(fpIn,"%lf%lf%lf%lf%lf\n", &temp1, &temp2, &temp3, &temp4, &temp5);
/* make sure the line has the right number of entries or is EOF */
if (r==5) nTemplates++;
} while ( r != EOF);
rewind(fpIn);
alphaVec = (REAL8 *)LALMalloc(nTemplates*sizeof(REAL8));
deltaVec = (REAL8 *)LALMalloc(nTemplates*sizeof(REAL8));
freqVec = (REAL8 *)LALMalloc(nTemplates*sizeof(REAL8));
spndnVec = (REAL8 *)LALMalloc(nTemplates*sizeof(REAL8));
for (templateCounter = 0; templateCounter < nTemplates; templateCounter++)
{
r=fscanf(fpIn,"%lf%lf%lf%lf%lf\n", &temp1, alphaVec + templateCounter, deltaVec + templateCounter,
freqVec + templateCounter, spndnVec + templateCounter);
}
fclose(fpIn);
}
/**************************************************/
/* read sfts */
/*************************************************/
f_min = freqVec[0]; /* initial frequency to be analyzed */
/* assume that the last frequency in the templates file is also the highest frequency */
f_max = freqVec[nTemplates-1] ;
/* we need to add wings to fmin and fmax to account for
the Doppler shift, the size of the rngmed block size
and also nfsizecylinder. The block size and nfsizecylinder are
specified in terms of frequency bins...this goes as one of the arguments of
LALReadSFTfiles */
/* first correct for Doppler shift */
fWings = f_max * VTOT;
f_min -= fWings;
f_max += fWings;
/* create pattern to look for in SFT directory */
{
CHAR *tempDir = NULL;
SFTCatalog *catalog = NULL;
static SFTConstraints constraints;
/* set detector constraint */
constraints.detector = NULL;
if ( XLALUserVarWasSet( &uvar_ifo ) )
constraints.detector = XLALGetChannelPrefix ( uvar_ifo );
/* get sft catalog */
tempDir = (CHAR *)LALCalloc(512, sizeof(CHAR));
strcpy(tempDir, uvar_sftDir);
strcat(tempDir, "/*SFT*.*");
XLAL_CHECK_MAIN( ( catalog = XLALSFTdataFind( tempDir, &constraints) ) != NULL, XLAL_EFUNC);
detector = XLALGetSiteInfo( catalog->data[0].header.name);
mObsCoh = catalog->length;
timeBase = 1.0 / catalog->data->header.deltaF;
XLAL_CHECK_MAIN( ( inputSFTs = XLALLoadSFTs ( catalog, f_min, f_max) ) != NULL, XLAL_EFUNC);
XLAL_CHECK_MAIN( XLALNormalizeSFTVect( inputSFTs, uvar_blocksRngMed, 0.0 ) == XLAL_SUCCESS, XLAL_EFUNC);
if ( XLALUserVarWasSet( &uvar_ifo ) )
LALFree( constraints.detector );
LALFree( tempDir);
XLALDestroySFTCatalog(catalog );
}
sftlength = inputSFTs->data->data->length;
{
INT4 tempFbin;
sftFminBin = floor( (REAL4)(timeBase * inputSFTs->data->f0) + (REAL4)(0.5));
tempFbin = floor( timeBase * inputSFTs->data->f0 + 0.5);
if (tempFbin - sftFminBin)
{
fprintf(stderr, "Rounding error in calculating fminbin....be careful! \n");
}
}
/* loop over sfts and select peaks */
/* first the memory allocation for the peakgramvector */
pgV = NULL;
pgV = (UCHARPeakGram **)LALMalloc(mObsCoh*sizeof(UCHARPeakGram *));
/* memory for peakgrams */
for (tempLoopId=0; tempLoopId < mObsCoh; tempLoopId++)
{
pgV[tempLoopId] = (UCHARPeakGram *)LALMalloc(sizeof(UCHARPeakGram));
pgV[tempLoopId]->length = sftlength;
pgV[tempLoopId]->data = NULL;
pgV[tempLoopId]->data = (UCHAR *)LALMalloc(sftlength* sizeof(UCHAR));
LAL_CALL (SFTtoUCHARPeakGram( &status, pgV[tempLoopId], inputSFTs->data + tempLoopId, uvar_peakThreshold), &status);
}
/* having calculated the peakgrams we don't need the sfts anymore */
XLALDestroySFTVector( inputSFTs);
/* ****************************************************************/
/* setting timestamps vector */
/* ****************************************************************/
timeV.length = mObsCoh;
timeV.data = NULL;
timeV.data = (LIGOTimeGPS *)LALMalloc(mObsCoh*sizeof(LIGOTimeGPS));
{
UINT4 j;
for (j=0; j < mObsCoh; j++){
timeV.data[j].gpsSeconds = pgV[j]->epoch.gpsSeconds;
timeV.data[j].gpsNanoSeconds = pgV[j]->epoch.gpsNanoSeconds;
}
}
/******************************************************************/
/* compute the time difference relative to startTime for all SFTs */
/******************************************************************/
timeDiffV.length = mObsCoh;
timeDiffV.data = NULL;
timeDiffV.data = (REAL8 *)LALMalloc(mObsCoh*sizeof(REAL8));
{
REAL8 t0, ts, tn, midTimeBase;
UINT4 j;
midTimeBase=0.5*timeBase;
ts = timeV.data[0].gpsSeconds;
tn = timeV.data[0].gpsNanoSeconds * 1.00E-9;
t0=ts+tn;
timeDiffV.data[0] = midTimeBase;
for (j=1; j< mObsCoh; ++j){
ts = timeV.data[j].gpsSeconds;
tn = timeV.data[j].gpsNanoSeconds * 1.00E-9;
timeDiffV.data[j] = ts + tn -t0 + midTimeBase;
}
}
/******************************************************************/
/* compute detector velocity for those time stamps */
/******************************************************************/
velV.length = mObsCoh;
velV.data = NULL;
velV.data = (REAL8Cart3Coor *)LALMalloc(mObsCoh*sizeof(REAL8Cart3Coor));
{
VelocityPar velPar;
REAL8 vel[3];
UINT4 j;
velPar.detector = *detector;
velPar.tBase = timeBase;
velPar.vTol = ACCURACY;
velPar.edat = NULL;
/* read in ephemeris data */
XLAL_CHECK_MAIN( ( edat = XLALInitBarycenter( uvar_earthEphemeris, uvar_sunEphemeris ) ) != NULL, XLAL_EFUNC);
velPar.edat = edat;
/* now calculate average velocity */
for(j=0; j< velV.length; ++j){
velPar.startTime.gpsSeconds = timeV.data[j].gpsSeconds;
velPar.startTime.gpsNanoSeconds = timeV.data[j].gpsNanoSeconds;
LAL_CALL( LALAvgDetectorVel ( &status, vel, &velPar), &status );
velV.data[j].x= vel[0];
velV.data[j].y= vel[1];
velV.data[j].z= vel[2];
}
}
/* amplitude modulation stuff */
{
AMCoeffs XLAL_INIT_DECL(amc);
AMCoeffsParams *amParams;
EarthState earth;
BarycenterInput baryinput; /* Stores detector location and other barycentering data */
/* detector location */
baryinput.site.location[0] = detector->location[0]/LAL_C_SI;
baryinput.site.location[1] = detector->location[1]/LAL_C_SI;
baryinput.site.location[2] = detector->location[2]/LAL_C_SI;
baryinput.dInv = 0.e0;
/* alpha and delta must come from the skypatch */
/* for now set it to something arbitrary */
baryinput.alpha = 0.0;
baryinput.delta = 0.0;
/* Allocate space for amParams stucture */
/* Here, amParams->das is the Detector and Source info */
amParams = (AMCoeffsParams *)LALMalloc(sizeof(AMCoeffsParams));
amParams->das = (LALDetAndSource *)LALMalloc(sizeof(LALDetAndSource));
amParams->das->pSource = (LALSource *)LALMalloc(sizeof(LALSource));
/* Fill up AMCoeffsParams structure */
amParams->baryinput = &baryinput;
amParams->earth = &earth;
amParams->edat = edat;
amParams->das->pDetector = detector;
/* make sure alpha and delta are correct */
amParams->das->pSource->equatorialCoords.latitude = baryinput.delta;
amParams->das->pSource->equatorialCoords.longitude = baryinput.alpha;
amParams->das->pSource->orientation = 0.0;
amParams->das->pSource->equatorialCoords.system = COORDINATESYSTEM_EQUATORIAL;
amParams->polAngle = amParams->das->pSource->orientation ; /* These two have to be the same!!*/
/* timeV is start time ---> change to mid time */
LAL_CALL (LALComputeAM(&status, &amc, timeV.data, amParams), &status);
/* calculate a^2 and b^2 */
/* for (ii=0, asq=0.0, bsq=0.0; ii<mObsCoh; ii++) */
/* { */
/* REAL8 *a, *b; */
/* a = amc.a + ii; */
/* b = amc.b + ii; */
/* asq += (*a) * (*a); */
/* bsq += (*b) * (*b); */
/* } */
/* free amParams */
LALFree(amParams->das->pSource);
LALFree(amParams->das);
LALFree(amParams);
}
/* loop over templates */
for(loopId=0; loopId < nTemplates; ++loopId){
/* set template parameters */
pulsarTemplate.f0 = freqVec[loopId];
pulsarTemplate.longitude = alphaVec[loopId];
pulsarTemplate.latitude = deltaVec[loopId];
pulsarTemplate.spindown.data[0] = spndnVec[loopId];
{
REAL8 f0new, vcProdn, timeDiffN;
REAL8 sourceDelta, sourceAlpha, cosDelta, factorialN;
UINT4 j, i, f0newBin;
REAL8Cart3Coor sourceLocation;
sourceDelta = pulsarTemplate.latitude;
sourceAlpha = pulsarTemplate.longitude;
cosDelta = cos(sourceDelta);
sourceLocation.x = cosDelta* cos(sourceAlpha);
sourceLocation.y = cosDelta* sin(sourceAlpha);
sourceLocation.z = sin(sourceDelta);
/* loop for all different time stamps,calculate frequency and produce number count*/
/* first initialize number count */
numberCount=0;
for (j=0; j<mObsCoh; ++j)
{
/* calculate v/c.n */
vcProdn = velV.data[j].x * sourceLocation.x
+ velV.data[j].y * sourceLocation.y
+ velV.data[j].z * sourceLocation.z;
/* loop over spindown values to find f_0 */
f0new = pulsarTemplate.f0;
factorialN = 1.0;
timeDiffN = timeDiffV.data[j];
for (i=0; i<msp;++i)
{
factorialN *=(i+1.0);
f0new += pulsarTemplate.spindown.data[i]*timeDiffN / factorialN;
timeDiffN *= timeDiffN;
}
f0newBin = floor(f0new*timeBase + 0.5);
foft = f0newBin * (1.0 +vcProdn) / timeBase;
/* get the right peakgram */
pg1 = pgV[j];
/* calculate frequency bin for template */
ind = floor( foft * timeBase + 0.5 ) - sftFminBin;
/* update the number count */
numberCount+=pg1->data[ind];
}
} /* end of block calculating frequency path and number count */
/******************************************************************/
/* printing result in the output file */
/******************************************************************/
fprintf(fpOut,"%d %f %f %f %g \n",
numberCount, pulsarTemplate.longitude, pulsarTemplate.latitude, pulsarTemplate.f0,
pulsarTemplate.spindown.data[0] );
} /* end of loop over templates */
/******************************************************************/
/* Closing files */
/******************************************************************/
fclose(fpOut);
/******************************************************************/
/* Free memory and exit */
/******************************************************************/
LALFree(alphaVec);
LALFree(deltaVec);
LALFree(freqVec);
LALFree(spndnVec);
for (tempLoopId = 0; tempLoopId < mObsCoh; tempLoopId++){
pg1 = pgV[tempLoopId];
LALFree(pg1->data);
LALFree(pg1);
}
LALFree(pgV);
LALFree(timeV.data);
LALFree(timeDiffV.data);
LALFree(velV.data);
LALFree(pulsarTemplate.spindown.data);
XLALDestroyEphemerisData(edat);
XLALDestroyUserVars();
LALCheckMemoryLeaks();
return DRIVEHOUGHCOLOR_ENORM;
}
/** Initialize Fstat-code: handle user-input and set everything up. */
int
XLALInitCode ( ConfigVariables *cfg, const UserInput_t *uvar )
{
/* generate log-string for file-output, containing cmdline-options + code VCS version info */
char *vcs;
if ( (vcs = XLALGetVersionString(0)) == NULL ) { /* short VCS version string */
XLALPrintError ( "%s: XLALGetVersionString(0) failed with errno=%d.\n", __func__, xlalErrno );
XLAL_ERROR ( XLAL_EFUNC );
}
char *cmdline;
if ( (cmdline = XLALUserVarGetLog ( UVAR_LOGFMT_CMDLINE )) == NULL ) {
XLALPrintError ( "%s: XLALUserVarGetLog ( UVAR_LOGFMT_CMDLINE ) failed with errno=%d.\n", __func__, xlalErrno );
XLAL_ERROR ( XLAL_EFUNC );
}
const char fmt[] = "%%%% cmdline: %s\n%%%%\n%s%%%%\n";
UINT4 len = strlen(vcs) + strlen(cmdline) + strlen(fmt) + 1;
if ( ( cfg->logString = XLALMalloc ( len )) == NULL ) {
XLALPrintError ("%s: XLALMalloc ( %d ) failed.\n", __func__, len );
XLAL_ERROR ( XLAL_ENOMEM );
}
sprintf ( cfg->logString, fmt, cmdline, vcs );
XLALFree ( cmdline );
XLALFree ( vcs );
/* trivial settings from user-input */
cfg->SignalOnly = uvar->SignalOnly;
/* ----- parse user-input on signal amplitude-paramters + ranges ----- */
/* skypos */
cfg->skypos.longitude = uvar->Alpha; /* Alpha < 0 indicates 'allsky' */
cfg->skypos.latitude = uvar->Delta;
cfg->skypos.system = COORDINATESYSTEM_EQUATORIAL;
/* ----- amplitude-params: create prior pdfs reflecting the user-input */
if ( XLALInitAmplitudePrior ( &cfg->AmpPrior, uvar ) != XLAL_SUCCESS )
XLAL_ERROR ( XLAL_EFUNC );
/* ----- initialize random-number generator ----- */
/* read out environment variables GSL_RNG_xxx
* GSL_RNG_SEED: use to set random seed: default = 0, override by using --randSeed on cmdline
* GSL_RNG_TYPE: type of random-number generator to use: default = 'mt19937'
*/
gsl_rng_env_setup ();
/* allow overriding the random-seed per command-line */
if ( XLALUserVarWasSet ( &uvar->randSeed ) )
gsl_rng_default_seed = uvar->randSeed;
cfg->rng = gsl_rng_alloc (gsl_rng_default);
LogPrintf ( LOG_DEBUG, "random-number generator type: %s\n", gsl_rng_name (cfg->rng));
LogPrintf ( LOG_DEBUG, "seed = %lu\n", gsl_rng_default_seed );
/* init ephemeris-data */
EphemerisData *edat = XLALInitBarycenter( uvar->ephemEarth, uvar->ephemSun );
if ( !edat ) {
LogPrintf ( LOG_CRITICAL, "%s: XLALInitBarycenter failed: could not load Earth ephemeris '%s' and Sun ephemeris '%s'\n", __func__, uvar->ephemEarth, uvar->ephemSun);
XLAL_ERROR ( XLAL_EFUNC );
}
/* init detector info */
LALDetector *site;
if ( (site = XLALGetSiteInfo ( uvar->IFO )) == NULL ) {
XLALPrintError ("%s: Failed to get site-info for detector '%s'\n", __func__, uvar->IFO );
XLAL_ERROR ( XLAL_EFUNC );
}
MultiLALDetector multiDet;
multiDet.length = 1;
multiDet.sites[0] = (*site); /* copy! */
XLALFree ( site );
/* init timestamps vector covering observation time */
UINT4 numSteps = (UINT4) ceil ( uvar->dataDuration / uvar->TAtom );
MultiLIGOTimeGPSVector * multiTS;
if ( (multiTS = XLALCalloc ( 1, sizeof(*multiTS))) == NULL ) {
XLAL_ERROR ( XLAL_ENOMEM );
}
multiTS->length = 1;
if ( (multiTS->data = XLALCalloc (1, sizeof(*multiTS->data))) == NULL ) {
XLAL_ERROR ( XLAL_ENOMEM );
}
if ( (multiTS->data[0] = XLALCreateTimestampVector (numSteps)) == NULL ) {
XLALPrintError ("%s: XLALCreateTimestampVector(%d) failed.\n", __func__, numSteps );
}
multiTS->data[0]->deltaT = uvar->TAtom;
UINT4 i;
for ( i=0; i < numSteps; i ++ )
{
UINT4 ti = uvar->dataStartGPS + i * uvar->TAtom;
multiTS->data[0]->data[i].gpsSeconds = ti;
multiTS->data[0]->data[i].gpsNanoSeconds = 0;
}
/* get detector states */
if ( (cfg->multiDetStates = XLALGetMultiDetectorStates ( multiTS, &multiDet, edat, 0.5 * uvar->TAtom )) == NULL ) {
XLALPrintError ( "%s: XLALGetMultiDetectorStates() failed.\n", __func__ );
XLAL_ERROR ( XLAL_EFUNC );
}
/* get rid of all temporary memory allocated for this step */
XLALDestroyEphemerisData ( edat );
XLALDestroyMultiTimestamps ( multiTS );
multiTS = NULL;
/* ---------- initialize transient window ranges, for injection ... ---------- */
transientWindowRange_t XLAL_INIT_DECL(InjectRange);
int twtype;
XLAL_CHECK ( (twtype = XLALParseTransientWindowName ( uvar->injectWindow_type )) >= 0, XLAL_EFUNC );
InjectRange.type = twtype;
/* make sure user doesn't set window=none but sets window-parameters => indicates she didn't mean 'none' */
if ( InjectRange.type == TRANSIENT_NONE ) {
if ( XLALUserVarWasSet ( &uvar->injectWindow_t0Days ) || XLALUserVarWasSet ( &uvar->injectWindow_t0DaysBand ) ||
XLALUserVarWasSet ( &uvar->injectWindow_tauDays ) || XLALUserVarWasSet ( &uvar->injectWindow_tauDaysBand ) ) {
XLALPrintError ("%s: ERROR: injectWindow_type == NONE, but window-parameters were set! Use a different window-type!\n", __func__ );
XLAL_ERROR ( XLAL_EINVAL );
}
}
if ( uvar->injectWindow_t0DaysBand < 0 || uvar->injectWindow_tauDaysBand < 0 ) {
XLALPrintError ("%s: only positive t0/tau window injection bands allowed (%f, %f)\n", __func__, uvar->injectWindow_t0DaysBand, uvar->injectWindow_tauDaysBand );
XLAL_ERROR ( XLAL_EINVAL );
}
/* apply correct defaults if unset: t0=dataStart, t0Band=dataDuration-3*tauMax */
InjectRange.t0 = uvar->dataStartGPS + uvar->injectWindow_t0Days * DAY24;
REAL8 tauMax = ( uvar->injectWindow_tauDays + uvar->injectWindow_tauDaysBand ) * DAY24;
if ( XLALUserVarWasSet (&uvar->injectWindow_t0DaysBand ) )
InjectRange.t0Band = uvar->injectWindow_t0DaysBand * DAY24;
else
InjectRange.t0Band = fmax ( 0.0, uvar->dataDuration - TRANSIENT_EXP_EFOLDING * tauMax - InjectRange.t0 ); /* make sure it's >= 0 */
InjectRange.tau = (UINT4) ( uvar->injectWindow_tauDays * DAY24 );
InjectRange.tauBand = (UINT4) ( uvar->injectWindow_tauDaysBand * DAY24 );
cfg->transientInjectRange = InjectRange;
/* ---------- ... and for search -------------------- */
transientWindowRange_t XLAL_INIT_DECL(SearchRange);
XLAL_CHECK ( (twtype = XLALParseTransientWindowName ( uvar->searchWindow_type )) >= 0, XLAL_EFUNC );
SearchRange.type = twtype;
/* apply correct defaults if unset: use inect window */
if ( !XLALUserVarWasSet ( &uvar->searchWindow_type ) )
SearchRange.type = InjectRange.type;
if ( !XLALUserVarWasSet ( &uvar->searchWindow_t0Days ) )
SearchRange.t0 = InjectRange.t0;
else
SearchRange.t0 = uvar->dataStartGPS + uvar->searchWindow_t0Days * DAY24;
if ( !XLALUserVarWasSet ( &uvar->searchWindow_t0DaysBand ) )
SearchRange.t0Band = InjectRange.t0Band;
else
SearchRange.t0Band = (UINT4) (uvar->searchWindow_t0DaysBand * DAY24);
if ( !XLALUserVarWasSet ( &uvar->searchWindow_tauDays ) )
SearchRange.tau = InjectRange.tau;
else
SearchRange.tau = (UINT4) ( uvar->searchWindow_tauDays * DAY24 );
if ( !XLALUserVarWasSet ( &uvar->searchWindow_tauDaysBand ) )
SearchRange.tauBand = InjectRange.tauBand;
else
SearchRange.tauBand = (UINT4) ( uvar->searchWindow_tauDaysBand * DAY24 );
if ( XLALUserVarWasSet ( &uvar->searchWindow_dt0 ) )
SearchRange.dt0 = uvar->searchWindow_dt0;
else
SearchRange.dt0 = uvar->TAtom;
if ( XLALUserVarWasSet ( &uvar->searchWindow_dtau ) )
SearchRange.dtau = uvar->searchWindow_dtau;
else
SearchRange.dtau = uvar->TAtom;
/* make sure user doesn't set window=none but sets window-parameters => indicates she didn't mean 'none' */
if ( SearchRange.type == TRANSIENT_NONE )
if ( XLALUserVarWasSet ( &uvar->searchWindow_t0Days ) || XLALUserVarWasSet ( &uvar->searchWindow_t0DaysBand ) ||
XLALUserVarWasSet ( &uvar->searchWindow_tauDays ) || XLALUserVarWasSet ( &uvar->searchWindow_tauDaysBand ) ) {
XLALPrintError ("%s: ERROR: searchWindow_type == NONE, but window-parameters were set! Use a different window-type!\n", __func__ );
XLAL_ERROR ( XLAL_EINVAL );
}
if ( uvar->searchWindow_t0DaysBand < 0 || uvar->searchWindow_tauDaysBand < 0 ) {
XLALPrintError ("%s: only positive t0/tau window injection bands allowed (%f, %f)\n", __func__, uvar->searchWindow_t0DaysBand, uvar->searchWindow_tauDaysBand );
XLAL_ERROR ( XLAL_EINVAL );
}
cfg->transientSearchRange = SearchRange;
return XLAL_SUCCESS;
} /* XLALInitCode() */
/*--------------main function---------------*/
int main(int argc, char **argv){
const CHAR *fn = __func__;
InputParams XLAL_INIT_DECL(inputs);
REAL8 srate = 16384.0; /*sample rate defaulted to 16384 */
/* read in command line input args */
ReadInput( &inputs, argc, argv );
LALStatus XLAL_INIT_DECL(status);
EphemerisData *edat;
if ( (edat = InitEphemeris ( inputs.ephemType, inputs.ephemDir)) == NULL ){
XLALPrintError ( "%s: Failed to init ephemeris data\n", fn );
XLAL_ERROR ( XLAL_EFUNC );
}
/*init detector info */
LALDetector *site;
if ( ( site = XLALGetSiteInfo ( inputs.det )) == NULL ){
XLALPrintError("%s: Failed to get site-info for detector '%s'\n", fn,
inputs.det );
XLAL_ERROR ( XLAL_EFUNC );
}
if( inputs.geocentre ){ /* set site to the geocentre */
site->location[0] = 0.0;
site->location[1] = 0.0;
site->location[2] = 0.0;
}
struct dirent **pulsars;
INT4 n=scandir(inputs.pulsarDir, &pulsars, 0, alphasort);
if ( n < 0){
XLALPrintError("scandir failed\n");
XLAL_ERROR(XLAL_EIO);
}
UINT4 numpulsars = (UINT4)n;
UINT4 h=0;
CHAR parname[256];
PulsarParameters *pulparams[numpulsars];
for(h=2; h<numpulsars; h++){
if(strstr(pulsars[h]->d_name,".par") == NULL){
free(pulsars[h]);
continue;
}
else{
sprintf(parname,"%s/%s", inputs.pulsarDir, pulsars[h]->d_name);
fprintf(stderr, "%s\n", parname);
FILE *inject;
if (( inject = fopen ( parname, "r" )) == NULL ){
fprintf(stderr,"Error opening file: %s\n", parname);
XLAL_ERROR ( XLAL_EIO );
}
pulparams[h] = XLALReadTEMPOParFile( parname );
fclose( inject );
}
}
LIGOTimeGPS epoch;
UINT4 ndata;
epoch.gpsSeconds = inputs.epoch;
epoch.gpsNanoSeconds = 0;
ndata = inputs.frDur;
REAL8TimeSeries *series=NULL;
CHAR out_file[256];
sprintf(out_file, "%s-%s-%d-%d.gwf", inputs.det, inputs.outStr,
epoch.gpsSeconds, ndata );
LALFrameH *outFrame = NULL;
if ((outFrame = XLALFrameNew( &epoch, (REAL8)ndata, inputs.channel, 1, 0,
0 )) == NULL) {
LogPrintf(LOG_CRITICAL, "%s : XLALFrameNew() filed with error = %d.\n", fn, xlalErrno);
XLAL_ERROR( XLAL_EFAILED);
}
if ((series = XLALCreateREAL8TimeSeries( inputs.channel, &epoch, 0.,
1./srate,&lalSecondUnit, (int)(ndata*srate) )) == NULL) {
XLAL_ERROR( XLAL_EFUNC );
}
UINT4 counter=0;
for (counter = 0; counter < series->data->length; counter++)
series->data->data[counter] = 0;
/*** Read Pulsar Data ***/
for (h=0; h < numpulsars; h++){
if(strstr(pulsars[h]->d_name,".par")==NULL){
free(pulsars[h]);
continue;
}
else{
PulsarSignalParams XLAL_INIT_DECL(params);
/* set signal generation barycenter delay look-up table step size */
params.dtDelayBy2 = 10.; /* generate table every 10 seconds */
if (( params.pulsar.spindown = XLALCreateREAL8Vector(1)) == NULL ){
XLALPrintError("Out of memory");
XLAL_ERROR ( XLAL_EFUNC );
}
INT4 dtpos = 0;
if ( PulsarCheckParam(pulparams[h], "POSEPOCH") )
dtpos = epoch.gpsSeconds - (INT4)PulsarGetREAL8Param(pulparams[h], "POSEPOCH");
else
dtpos = epoch.gpsSeconds - (INT4)PulsarGetREAL8Param(pulparams[h], "PEPOCH");
REAL8 ra = 0., dec = 0.;
if ( PulsarCheckParam( pulparams[h], "RAJ" ) ) {
ra = PulsarGetREAL8Param( pulparams[h], "RAJ" );
}
else if ( PulsarCheckParam( pulparams[h], "RA" ) ){
ra = PulsarGetREAL8Param( pulparams[h], "RA" );
}
else{
XLALPrintError("No right ascension found");
XLAL_ERROR ( XLAL_EFUNC );
}
if ( PulsarCheckParam( pulparams[h], "DECJ" ) ) {
dec = PulsarGetREAL8Param( pulparams[h], "DECJ" );
}
else if ( PulsarCheckParam( pulparams[h], "DEC" ) ){
dec = PulsarGetREAL8Param( pulparams[h], "DEC" );
}
else{
XLALPrintError("No declination found");
XLAL_ERROR ( XLAL_EFUNC );
}
params.pulsar.position.latitude = dec + (REAL8)dtpos * PulsarGetREAL8ParamOrZero(pulparams[h], "PMDEC");
params.pulsar.position.longitude = ra + (REAL8)dtpos * PulsarGetREAL8ParamOrZero(pulparams[h], "PMRA") / cos(params.pulsar.position.latitude);
params.pulsar.position.system = COORDINATESYSTEM_EQUATORIAL;
REAL8Vector *fs = PulsarGetREAL8VectorParam(pulparams[h], "F");
if ( fs->length == 0 ){
XLALPrintError("No frequencies found");
XLAL_ERROR ( XLAL_EFUNC );
}
params.pulsar.f0 = 2.*fs->data[0];
if ( fs->length > 1 ){
params.pulsar.spindown->data[0] = 2.*fs->data[1];
}
if (( XLALGPSSetREAL8(&(params.pulsar.refTime), PulsarGetREAL8Param(pulparams[h], "PEPOCH")) ) == NULL )
XLAL_ERROR ( XLAL_EFUNC );
params.pulsar.psi = PulsarGetREAL8ParamOrZero(pulparams[h], "PSI");
params.pulsar.phi0 = PulsarGetREAL8ParamOrZero(pulparams[h], "PHI0");
REAL8 cosiota = PulsarGetREAL8ParamOrZero(pulparams[h], "COSIOTA");
REAL8 h0 = PulsarGetREAL8ParamOrZero(pulparams[h], "H0");
params.pulsar.aPlus = 0.5 * h0 * (1. + cosiota * cosiota );
params.pulsar.aCross = h0 * cosiota;
/*Add binary later if needed!*/
params.site = site;
params.ephemerides = edat;
params.startTimeGPS = epoch;
params.duration = ndata;
params.samplingRate = srate;
params.fHeterodyne = 0.;
REAL4TimeSeries *TSeries = NULL;
LALGeneratePulsarSignal( &status, &TSeries, ¶ms );
if (status.statusCode){
fprintf(stderr, "LAL Routine failed!\n");
XLAL_ERROR (XLAL_EFAILED);
}
UINT4 i;
for (i=0; i < TSeries->data->length; i++)
series->data->data[i] += TSeries->data->data[i];
XLALDestroyREAL4TimeSeries(TSeries);
XLALDestroyREAL8Vector(params.pulsar.spindown);
}
}
if (XLALFrameAddREAL8TimeSeriesProcData(outFrame,series)){
LogPrintf(LOG_CRITICAL, "%s : XLALFrameAddREAL8TimeSeries() failed with error = %d.\n",fn,xlalErrno);
XLAL_ERROR(XLAL_EFAILED);
}
CHAR OUTFILE[256];
sprintf(OUTFILE, "%s/%s", inputs.outDir, out_file);
if ( XLALFrameWrite(outFrame, OUTFILE)){
LogPrintf(LOG_CRITICAL, "%s : XLALFrameWrite() failed with error = %d.\n", fn, xlalErrno);
XLAL_ERROR( XLAL_EFAILED );
}
XLALFrameFree(outFrame);
XLALDestroyREAL8TimeSeries( series );
return 0;
}
int main(int argc, char **argv)
{
FILE *fp = NULL;
FILE *fp2 = NULL;
FILE *fp3 = NULL;
FILE *fp4 = NULL;
LALStatus status = blank_status;
SFTCatalog *catalog = NULL;
SFTVector *sft_vect = NULL;
INT4 i,j,k,l;
INT4 numBins, nSFT;
SFTConstraints constraints=empty_SFTConstraints;
LIGOTimeGPS startTime, endTime;
REAL8 avg =0;
REAL4 *timeavg =NULL;
REAL4 PWR,SNR;
REAL8 f =0;
CHAR outbase[256],outfile[256],outfile2[256],outfile3[256], outfile4[256]; /*, outfile6[256]; */
REAL8 NumBinsAvg =0;
REAL8 timebaseline =0;
BOOLEAN help = 0;
CHAR *SFTpatt = NULL;
CHAR *IFO = NULL;
INT4 startGPS = 0;
INT4 endGPS = 0;
REAL8 f_min = 0.0;
REAL8 f_max = 0.0;
REAL8 freqres =0.0;
INT4 blocksRngMed = 101;
CHAR *outputBname = NULL;
INT4 cur_epoch = 0, next_epoch = 0;
/* these varibales are for converting GPS seconds into UTC time and date*/
struct tm date;
CHARVector *timestamp = NULL;
CHARVector *year_date = NULL;
REAL8Vector *timestamps=NULL;
CHAR *psrInput = NULL;
CHAR *psrEphemeris = NULL;
CHAR *earthFile = NULL;
CHAR *sunFile = NULL;
/*========================================================================================================================*/
LAL_CALL(LALRegisterBOOLUserVar (&status, "help", 'h', UVAR_HELP, "Print this help message", &help ), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "SFTs", 'p', UVAR_REQUIRED, "SFT location/pattern", &SFTpatt ), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "IFO", 'I', UVAR_REQUIRED, "Detector", &IFO ), &status);
LAL_CALL(LALRegisterINTUserVar (&status, "startGPS", 's', UVAR_REQUIRED, "Starting GPS time", &startGPS ), &status);
LAL_CALL(LALRegisterINTUserVar (&status, "endGPS", 'e', UVAR_REQUIRED, "Ending GPS time", &endGPS ), &status);
LAL_CALL(LALRegisterREALUserVar (&status, "fMin", 'f', UVAR_REQUIRED, "Minimum frequency", &f_min ), &status);
LAL_CALL(LALRegisterREALUserVar (&status, "fMax", 'F', UVAR_REQUIRED, "Maximum frequency", &f_max ), &status);
LAL_CALL(LALRegisterINTUserVar (&status, "blocksRngMed", 'w', UVAR_OPTIONAL, "Running Median window size", &blocksRngMed), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "outputBname", 'o', UVAR_OPTIONAL, "Base name of output files", &outputBname ), &status);
LAL_CALL(LALRegisterREALUserVar (&status, "freqRes", 'r', UVAR_REQUIRED, "Spectrogram freq resolution", &freqres ), &status);
LAL_CALL(LALRegisterREALUserVar (&status, "timeBaseline", 't', UVAR_REQUIRED, "The time baseline of sfts", &timebaseline), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "psrInput", 'P', UVAR_OPTIONAL, "name of tempo pulsar file", &psrInput ), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "psrEphemeris", 'S', UVAR_OPTIONAL, "pulsar ephemeris file", &psrEphemeris ), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "earthFile", 'y', UVAR_OPTIONAL, "earth .dat file", &earthFile ), &status);
LAL_CALL(LALRegisterSTRINGUserVar(&status, "sunFile", 'z', UVAR_OPTIONAL, "sun .dat file", &sunFile ), &status);
LAL_CALL(LALUserVarReadAllInput(&status, argc, argv), &status);
if (help)
return(0);
startTime.gpsSeconds = startGPS;/*cg; startTime is a structure, and gpsSeconds is a member of that structure*/
startTime.gpsNanoSeconds = 0;/*cg; gps NanoSeconds is also a member of the startTime structure */
constraints.minStartTime = &startTime; /*cg; & operator gets the address of variable, &a is a pointer to a. This line puts the startTime structure into the structure constraints*/
endTime.gpsSeconds = endGPS;
endTime.gpsNanoSeconds = 0;
constraints.maxEndTime = &endTime;/*cg; This line puts the end time into the structure constraints*/
constraints.detector = IFO;/*cg; this adds the interferometer into the contraints structure*/
LALSFTdataFind ( &status, &catalog, SFTpatt, &constraints );/*cg; creates SFT catalog, uses the constraints structure*/
if (catalog == NULL)/*need to check for a NULL pointer, and print info about circumstances if it is null*/
{
fprintf(stderr, "SFT catalog pointer is NULL! There has been an error with LALSFTdataFind\n");
fprintf(stderr, "LALStatus info.... status code: %d, message: %s, offending function: %s\n", status.statusCode, status.statusDescription, status.function);
exit(0);
}
if (catalog->length == 0)
{
fprintf(stderr, "No SFTs found, please exmanine start time, end time, frequency range etc\n");
exit(0);
}
LALLoadSFTs ( &status, &sft_vect, catalog, f_min,f_max);/*cg;reads the SFT data into the structure sft_vect*/
if (sft_vect == NULL)
{
fprintf(stderr, "SFT vector pointer is NULL! There has been an error with LALLoadSFTs\n");
fprintf(stderr, "LALStatus info.... status code: %d, message: %s, offending function: %s\n", status.statusCode, status.statusDescription, status.function);
exit(0);
}
LALDestroySFTCatalog( &status, &catalog);/*cg; desctroys the SFT catalogue*/
numBins = sft_vect->data->data->length;/*the number of bins in the freq_range*/
nSFT = sft_vect->length;/* the number of sfts.*/
fprintf(stderr, "nSFT = %d\tnumBins = %d\tf0 = %f\n", nSFT, numBins,sft_vect->data->f0);/*print->logs/spectrumAverage_testcg_0.err */
if (LALUserVarWasSet(&outputBname))
strcpy(outbase, outputBname);
else
sprintf(outbase, "spec_%.2f_%.2f_%s_%d_%d", f_min,f_max,constraints.detector,startTime.gpsSeconds,endTime.gpsSeconds);/*cg; this is the default name for producing the output files, the different suffixes are just added to this*/
sprintf(outfile, "%s", outbase);/*cg; name of first file to be output*/
sprintf(outfile2, "%s_timestamps", outbase);/*cg: name of second file to be output*/
sprintf(outfile3, "%s.txt", outbase);/*cg; name of third file to be output*/
sprintf(outfile4, "%s_date", outbase);/*cg;file for outputting the date, which is used in matlab plotting.*/
fp = fopen(outfile, "w");/*cg; open all three files for writing, if they don't exist create them, if they do exist overwrite them*/
fp2 = fopen(outfile2, "w");
fp3 = fopen(outfile3, "w");
fp4 = fopen(outfile4, "w");
/*----------------------------------------------------------------------------------------------------------------*/
/*cg; Create the first file called spec_blah_blah. This file outputs the power in each spectrogram bin. The number of bins depends on the frequency range, freq resolution, and number of SFTs.*/
/*cg; Create the second file, called blah_b;ah_blah_timestamps. This will simply contain the time in GPS seconds of each SFT.*/
NumBinsAvg = freqres*numBins/(f_max-f_min);/*this calcs the number of bins over which to average the sft data, this is worked out so it produces the same freq resolution as specified in the arguments passed to fscanDriver.py. numBins is the total number of bins in the raw sft data*/
l=0;/*l is used as a counter to count how many SFTs and fake zero SFTs (used for gaps) are output for specgram.*/
timestamps = XLALCreateREAL8Vector(l);/*test for getting rid of second loop*/
LALCHARCreateVector(&status, &year_date, (UINT4)128);
/*create output files and check for missing sfts*/
for (j=0;j<nSFT;j++)/*cg;nSFT is the numnber of SFT files used for the time specified. So process is repeated for each SFT*/
{
cur_epoch = sft_vect->data[j].epoch.gpsSeconds;/*finds the gps time of the current sft in the sequence with index j*/
fprintf(fp2, "%d.\t%d\n", l, cur_epoch);/*cg; this bit writes the second file, i.e. the timestamps*/
XLALResizeREAL8Vector(timestamps, l+1);/*resizes the vector timestamps, so cur_epoch can be added*/
timestamps->data[l]= cur_epoch;/*number of gaps is not know in advance, hence need for te resizing*/
XLALGPSToUTC(&date, cur_epoch);/*cg; gets the UTC date in struct tm format from the GPS seconds.*/
fprintf(fp4, "%d\t %i\t %i\t %i\t %i\t %i\t %i\n", l, (date.tm_year+1900), date.tm_mon+1, date.tm_mday, date.tm_hour, date.tm_min, date.tm_sec);
for ( i=0; i < (numBins-2); i+=NumBinsAvg)/*cg; this loop works out the powers and writes the first file.*/
{/*cg; each SFT is split up into a number of bins, the number of bins is read in from the SFT file*/
avg = 0.0;/*cg; the vairable avg is reset each time.*/
if (i+NumBinsAvg>numBins) {printf("Error\n");return(2);}/*cg; error is detected, to prevent referencing data past the end of sft_vect.*/
for (k=0;k<NumBinsAvg;k++)/*cg; for each bin, k goes trhough each entry from 0 to 180.*/
avg += sqrt(2*(crealf(sft_vect->data[j].data->data[i+k])*crealf(sft_vect->data[j].data->data[i+k]) +
cimagf(sft_vect->data[j].data->data[i+k])*cimagf(sft_vect->data[j].data->data[i+k]))/timebaseline);/*cg; re amd im are real and imaginary parts of SFT, duh!*/
fprintf(fp,"%e\t",avg/NumBinsAvg);
}
fprintf(fp,"\n");
/*------------------------------*/
/*Bit to check if there is a gap in the sfts*/
if ( j < (nSFT-1) )/*in all cases except when we are examining the last sft, check that there is no gap to the next sft*/
{
next_epoch = sft_vect->data[j+1].epoch.gpsSeconds;
/*test to see if SFT gap is longer than 3/2*timebaseline, if so create another entry in the matrix*/
while ((cur_epoch+((3/2)*timebaseline)) < next_epoch)
{
for ( i=0; i < (numBins-2); i+=NumBinsAvg)
{
avg = 0.0;
if (i+NumBinsAvg>numBins) {printf("Error\n");return(2);}
fprintf(fp,"%e\t",avg);
}
fprintf(fp,"\n");
l=l+1;
cur_epoch=cur_epoch+timebaseline;
fprintf(fp2, "%d.\t%d\n", l, cur_epoch );
XLALResizeREAL8Vector(timestamps, l+1);
timestamps->data[l]= cur_epoch;
XLALGPSToUTC(&date, cur_epoch);/*cg; gets the UTC date in struct tm format from the GPS seconds.*/
fprintf(fp4, "%d\t %i\t %i\t %i\t %i\t %i\t %i\n", l, (date.tm_year+1900), date.tm_mon+1, date.tm_mday, date.tm_hour, date.tm_min, date.tm_sec);
}
}
l=l+1;
}
fprintf(stderr,"finished checking for missing sfts, l=%d\n", l);
/*----------------------------------------------------------------------------------------------------------------*/
/*cg; Create the third and final file, called blah_blah_blah.txt. This file will contain the data used in the matlab plot script to plot the normalised average power vs the frequency.*/
/* Find time average of normalized SFTs */
LALNormalizeSFTVect(&status, sft_vect, blocksRngMed);
LALNormalizeSFTVect(&status, sft_vect, blocksRngMed);
timeavg = XLALMalloc(numBins*sizeof(REAL4));
if (timeavg == NULL) fprintf(stderr,"Timeavg memory not allocated\n");
for (j=0;j<nSFT;j++)
{
for ( i=0; i < numBins; i++)
{
if (j == 0)
{
timeavg[i] = crealf(sft_vect->data[j].data->data[i])*crealf(sft_vect->data[j].data->data[i]) +
cimagf(sft_vect->data[j].data->data[i])*cimagf(sft_vect->data[j].data->data[i]);
}
else
{
timeavg[i] += crealf(sft_vect->data[j].data->data[i])*crealf(sft_vect->data[j].data->data[i]) +
cimagf(sft_vect->data[j].data->data[i])*cimagf(sft_vect->data[j].data->data[i]);
}
}
}
/*timeavg records the power of each bin*/
for ( i=0; i < numBins; i++)
{
f = sft_vect->data->f0 + ((REAL4)i)*sft_vect->data->deltaF;
PWR=timeavg[i]/((REAL4)nSFT);
SNR=(PWR-1)*(sqrt(((REAL4)nSFT)));
fprintf(fp3,"%16.8f %g %g\n",f, PWR, SNR);
}
/*------------------------------------------------------------------------------------------------------------------------*/
/*End of normal spec_avg code, the remaining code is for crab freq calc.*/
/*================================================================================================================*/
/*================================================================================================================*/
/*This next block of code is for the crab specific changes to fscan*/
#define CRAB 0
/*change this to CRAB 0 to prevent this section of code from compiling, change to 1 to compile it.*/
#if CRAB
/*--------------------------------------------------------------------------------------------------------------*/
/*some header files for the crab*/
/*#include "../TDS_isolated/HeterodyneCrabPulsar.h"*/
/*#include "../TDS_isolated/heterodyne_pulsar.h"*/
#include<../TDS_isolated/HeterodyneCrabPulsar.h>
if (psrInput != NULL){
fprintf(stderr,"--------------------\n\n");
fprintf(stderr,"start of crab stuff\n");
LIGOTimeGPS dataEpoch;
/*below 4 structures are from HeterodyneCrabPulsar.h*/
GetCrabEphemerisInput input; /*this is needed to get the crab ephemeris*/
CrabSpindownParamsInput crabEphemerisData;
CrabSpindownParamsOutput crabOutput;
ParamsForHeterodyne hetParams;
/*CG; these lines allocate memory for the crab ephemeris and crab output variables...*/
crabEphemerisData.f1 = NULL;
LALDCreateVector( &status, &crabEphemerisData.f1, NUM);
crabEphemerisData.f0 = NULL;
LALDCreateVector( &status, &crabEphemerisData.f0, NUM);
crabEphemerisData.tArr = NULL;
LALDCreateVector( &status, &crabEphemerisData.tArr, NUM);
crabOutput.tArr = NULL;
LALDCreateVector( &status, &crabOutput.tArr, NUM);
crabOutput.f0 = NULL;
LALDCreateVector( &status, &crabOutput.f0, NUM);
crabOutput.f1 = NULL;
LALDCreateVector( &status, &crabOutput.f1, NUM);
crabOutput.f2 = NULL;
LALDCreateVector( &status, &crabOutput.f2, NUM);
crabOutput.f3 = NULL;
LALDCreateVector( &status, &crabOutput.f3, NUM);
crabOutput.f4 = NULL;
LALDCreateVector( &status, &crabOutput.f4, NUM);
/*This next set of variables are to do with the doppler shifts that are then applied to to the crab feq.*/
REAL8 t2=0., tdt=0.;
EphemerisData *edat=NULL;
BarycenterInput baryinput, baryinput2;
EarthState earth, earth2;
EmissionTime emit, emit2;
REAL8 df=0., freq, finalFreq, max_df, minf, maxf;
REAL8 dtpos=0.; /* time between position epoch and data timestamp */
BinaryPulsarParams pulsarParams; /*general pulsar params strcut, despite binary name*/
/*CHAR *psrInput = NULL;*/ /* pulsar input file containing params f0, f1 etc. */
LALDetector det;
CHAR detName[256];
REAL8 ecliptic_lat, e_tilt=0.409092627;/*the ecliptic latitude of the source, and hte earth's tilt in radians (23.439281 degrees)*/
char outfile5[256];
FILE *fp5 = NULL;
sprintf(outfile5, "%s_crab", outbase);
fp5 = fopen(outfile5, "w");
/*----------------------------------------------------------------------------------------------------------------*/
/*cg; calculating the crab freq, done in three steps. This is done for each sft*/
/*----------------------------------------------------------------------------------------------------------------*/
/* ---1--- */
/*Find rough guess of crabs freq from ephemeris*/
/*----------------------------------------------------------------------------------------------------------------*/
/*Get detector position, this is needed for barycentre calcs*/
det = *XLALGetSiteInfo( IFO );
/* read in tempo par file for pulsar, This is one of the optional command line arguments*/
/*fprintf(stderr,"%s\n",psrInput);*/
fprintf(stderr,"%s\n",psrInput);
XLALReadTEMPOParFile(&pulsarParams, psrInput);
/*Make sure that posepoch and pepoch are set*/
if(pulsarParams.pepoch == 0. && pulsarParams.posepoch != 0.)
pulsarParams.pepoch = pulsarParams.posepoch;
else if(pulsarParams.posepoch == 0. && pulsarParams.pepoch != 0.)
pulsarParams.posepoch = pulsarParams.pepoch;
fprintf(stderr,"Check on read tempo file, pepoch: %f\n", pulsarParams.pepoch);
/*input.filename=psrEphemeris;*/ /*/archive/home/colingill/lalsuite/lalapps/src/pulsar/fscan/ /archive/home/colingill/public_html/crab_ephemeris.txt*/
input.filename = XLALMalloc(sizeof(CHAR)*256);
if(input.filename == NULL) fprintf(stderr,"input.filename pointer memory not allocated\t");
strcpy(input.filename,psrEphemeris);
/*fprintf(stderr,"psrEphemeris:%s\n", input.filename);*/
/*The first stage is to read in f and fdot from the ephemeris, the crab_ephemeris.txt file is part of lalapps and is maintained by matt*/
LALGetCrabEphemeris( &status, &crabEphemerisData, &input );
/*check on the outputs, crabEphemerisData is a struct of type CrabSpindownParamsInput, and has members tArr, f0, f1*/
fprintf(stderr,"input crab ephemeris present, number of entries: %i\n", crabEphemerisData.numOfData);
fprintf(stderr,"crabEphemerisData: \ttarr= %f\tf0= %f\tf_dot= %e\n", crabEphemerisData.tArr->data[0], crabEphemerisData.f0->data[0], crabEphemerisData.f1->data[0]);
/*Now I have f and fdot, use function below to compute the higher order derrivatives of the crabs frequency*/
LALComputeFreqDerivatives( &status, &crabOutput, &crabEphemerisData );
/*check on this function, crabOutput is datatype CrabSpindownParamsOutput*/
fprintf(stderr,"crabOutput:\tf0= %f\tf1= %e\tf2= %e\n", crabOutput.f0->data[0], crabOutput.f1->data[0], crabOutput.f2->data[0]);/*need to change the type of printf for F1 and f2 to exponentials.*/
fprintf(stderr,"--------------------\n");
/*Allocate memory for edat, no need to do in the loop*/
edat = XLALMalloc(sizeof(*edat));
(*edat).ephiles.earthEphemeris = earthFile; /*"/archive/home/colingill/lalsuite/lal/packages/pulsar/test/earth05-09.dat";*/
(*edat).ephiles.sunEphemeris = sunFile;/*"/archive/home/colingill/lalsuite/lal/packages/pulsar/test/sun05-09.dat";*/
/*work out the eclitptic lattitude of the source, used in max freq calc.*/
ecliptic_lat=asin(cos(e_tilt)*sin(pulsarParams.dec)-sin(pulsarParams.ra)*cos(pulsarParams.dec)*sin(e_tilt));
fprintf(stderr,"eqcliptic_lat: %e\t", ecliptic_lat);
for (i=0;i<l;i++)
{
if (i == (l-1))/*catches the last iteration where there is no i+1 entry in timestamps*/
{
cur_epoch = timestamps->data[i]+(timebaseline/2);
}
else
{
cur_epoch = timestamps->data[i]+((timestamps->data[i+1] - timestamps->data[i])/2);
}
fprintf(stderr,"cur_epoch: %d\t", cur_epoch);
/*The time has to be set so that the nearest entry to that time in the ephemeris can be used*/
dataEpoch.gpsSeconds = cur_epoch; /*INT8)floor(time->data[j]);*/
dataEpoch.gpsNanoSeconds = 0;
/*prepare hetParams, which is then used to get the freq derrivatives out and also in the next sub-section for Bary functions*/
LALSetSpindownParams( &status, &hetParams, &crabOutput, dataEpoch );
fprintf(stderr,"hetparams epoch: %f\t f0= %f\tf1= %e\n", hetParams.epoch, hetParams.f0, hetParams.f1);
/*----------------------------------------------------------------------------------------------------------------*/
/* ---2--- */
/*Add corrections for timing noise to get a better guess at the freq*/
/*----------------------------------------------------------------------------------------------------------------*/
/*now I want to use these params to calc the freq at any point in time. Using the higher order derrivatives is how we adjust for timing noise.*/
/*Get the time difference between the current epoch and the epoch of the ephemeris entry*/
tdt= cur_epoch - hetParams.epoch;
fprintf(stderr,"dt: %f,\tf1= %e,\tf2= %e,\tf3= %e,\tf4=%e\n", tdt, hetParams.f1, hetParams.f2, hetParams.f3, hetParams.f4);
freq = 2.0*( hetParams.f0 + ((hetParams.f1)*tdt) + (((hetParams.f2)*tdt*tdt)/2) + (((hetParams.f3)*tdt*tdt*tdt)/6) + (((hetParams.f4)*tdt*tdt*tdt*tdt)/24) );
fprintf(stderr,"crab fcoarse: %f\t", freq);
/*freq = 2.0*(params->f0 + params->f1*t1 + (params->f2)*t1*t1+ (params->f3)*t1*t1*t1 + (params->f4)*t1*t1*t1*t1);*/ /*cg;line 486 from hetcrabpulsar, works out freq, this is with one order of t removed for each of the derrivatives of f, and also each term is divided by a factorial, 1!, 2!, 3!, but this starts one term along from the oroginal code as we have integrated the orginal code to get freq not phase*/
/*----------------------------------------------------------------------------------------------------------------*/
/* ---3--- */
/*Add doppler shifts for earth's motion back onto the freq to get actual observed freq at detectors.*/
/*----------------------------------------------------------------------------------------------------------------*/
/*now I have the freq, I need to add the doppler shift for the earths motion around the sun */
baryinput.dInv = 0.;/*I can always set this to zero, as Matt said so, I must ask him why*/
LAL_CALL( LALInitBarycenter(&status, edat), &status );/* */
/*this lines take position of detector which are in xyz coords in meters from earths centre and converts them into seconds (time)*/
baryinput.site.location[0] = det.location[0]/LAL_C_SI;
baryinput.site.location[1] = det.location[1]/LAL_C_SI;
baryinput.site.location[2] = det.location[2]/LAL_C_SI;
/*dtpos should be the time between the entry in the ephemeris and the point in time for which doppler shifts are being calc.ed*/
dtpos = cur_epoch - pulsarParams.posepoch;
/* set up RA, DEC, and distance variables for LALBarycenter*/
baryinput.delta = pulsarParams.dec + dtpos*pulsarParams.pmdec;
baryinput.alpha = pulsarParams.ra + dtpos*pulsarParams.pmra/cos(baryinput.delta);
t2=cur_epoch+1;
baryinput2 = baryinput;
baryinput.tgps.gpsSeconds = (INT4)floor(cur_epoch);
baryinput.tgps.gpsNanoSeconds = (INT4)floor((fmod(cur_epoch,1.0)*1.e9));
baryinput2.tgps.gpsSeconds = (INT4)floor(t2);
baryinput2.tgps.gpsNanoSeconds = (INT4)floor((fmod(t2,1.0)*1.e9));
/*the barycentre functions are needed to calc the inputs for the correction to fcoarse, namely emit, earth and baryinput*/
LAL_CALL( LALBarycenterEarth(&status, &earth, &baryinput.tgps, edat), &status );
LAL_CALL( LALBarycenter(&status, &emit, &baryinput, &earth), &status );
LAL_CALL( LALBarycenterEarth(&status, &earth2, &baryinput2.tgps, edat), &status );
LAL_CALL( LALBarycenter(&status, &emit2, &baryinput2, &earth2), &status );
/* I need to calc the correction to the freq for the doppler shifts, the correction is df, from line 1074 heterdyne_pulsar. deltaT is T_emission in TDB - T_arrrival in GPS + light travel time to SSB. we are working out delta(delatT) over 1 second, so do not bother with the divide by one bit.*/
df = freq*(emit2.deltaT - emit.deltaT);
fprintf(stderr,"df: %f,\t", df);
/*Calc maximum possible df and then subtract applied df from it, use the remaining df to plot range over which f will wander.*/
max_df=freq*(( (29.783e3*cos(ecliptic_lat))+(465*cos(pulsarParams.dec)) )/3.0e8);/*max doppler shift, from speed of earth in plane of direction to source over c.*/
fprintf(stderr,"max df: %f\tbeta: %e\n", max_df, ecliptic_lat);
maxf=freq+max_df;
minf=freq-max_df;
finalFreq=freq+df;
/*df = fcoarse*(emit2.deltaT - emit.deltaT + binOutput2.deltaT - binOutput.deltaT);*//*use when have binary calcs in here also.*/
fprintf(fp5,"%f\t%f\t%f\t%f\t%f\n", freq, df, minf, finalFreq, maxf);
fprintf(stderr,"crab freq calc, i:%d, minf:%f, f:%f, maxf:%f\n", i, minf, finalFreq, maxf);
/*----------------------------------------------------------------------------------------------------------------*/
}
fclose(fp5);
fprintf(stderr,"end of crab stuff\n");
/*Free up any memory allocated in crab section*/
XLALFree(edat);
}
#endif
/*fprintf(stderr,"end of spec_avg 1\n");*/
/*=======================================================================================================================*/
/*=======================================================================================================================*/
/*release a;; the allocaeted memory*/
LALCHARDestroyVector(&status, ×tamp);
LALCHARDestroyVector(&status, &year_date);
LALDestroySFTVector (&status, &sft_vect );
/*fprintf(stderr,"end of spec_avg 2\n");*/
if (timeavg != NULL) XLALFree(timeavg);
/*fprintf(stderr,"end of spec_avg 3\n");*/
LAL_CALL(LALDestroyUserVars(&status), &status);
/*fprintf(stderr,"end of spec_avg 4\n");*/
/*close all the files, spec_avg.c is done, all info written to the files.*/
fclose(fp);
fclose(fp2);
fclose(fp3);
fclose(fp4);
fprintf(stderr,"end of spec_avg\n");
return(0);
}
/**
* Very simple test: pick random skyposition, compute a_i, b_i using
* once LALComputeAM() and once LALNewGetAMCoeffs(), and look at the errors
* sum_i (a_i - a_i')^2
*/
int main(int argc, char *argv[])
{
LALStatus XLAL_INIT_DECL(status);
int opt; /* Command-line option. */
LIGOTimeGPS startTime = {714180733, 0};
REAL8 duration = 180000; /* 50 hours */
REAL8 Tsft = 1800; /* assume 30min SFTs */
LIGOTimeGPSVector *timestamps = NULL;
DetectorStateSeries *detStates = NULL;
SkyPosition XLAL_INIT_DECL(skypos);
EphemerisData XLAL_INIT_DECL(edat);
BarycenterInput XLAL_INIT_DECL(baryinput);
LALDetector *det = NULL;
AMCoeffs XLAL_INIT_DECL(AMold);
AMCoeffs XLAL_INIT_DECL(AMnew1);
AMCoeffs XLAL_INIT_DECL(AMnew2);
REAL8 alpha, delta;
AMCoeffsParams XLAL_INIT_DECL(amParams);
EarthState earth;
UINT4 i;
REAL8 maxerr01, maxerr02, maxerr12, averr01, averr02, averr12;
REAL8 tolerance = 1e-2; /* be generous: allow 1% error */
struct tms buf;
const CHAR *sites[] = {"H1", "L1", "V2", "G1", "T1" };
REAL8 sinzeta; /* zeta = IFO opening angle */
UINT4 pickedSite;
BOOLEAN ignoreErrors = 0; /* Don't fail if tolerance exceeded */
UINT4 numChecks = 1; /* Number of times to check */
char earthEphem[] = TEST_DATA_DIR "earth00-19-DE405.dat.gz";
char sunEphem[] = TEST_DATA_DIR "sun00-19-DE405.dat.gz";
/* ----- old testing code to use 9 degree earth rotations ----- */
/* startTime.gpsSeconds = 714275242;
duration = 86164;
Tsft = 2154.1; */
while ((opt = LALgetopt( argc, argv, "n:qv:" )) != -1) {
switch (opt) {
case 'v': /* set lalDebugLevel */
break;
case 'q': /* don't fail if tolerance exceeded */
ignoreErrors = 1;
break;
case 'n': /* number of times to check */
numChecks = atoi( LALoptarg );
break;
}
}
/* init random-generator */
srand ( times(&buf) );
/* ----- init ephemeris ----- */
edat.ephiles.earthEphemeris = earthEphem;
edat.ephiles.sunEphemeris = sunEphem;
SUB ( LALInitBarycenter(&status, &edat), &status);
/* ----- get timestamps ----- */
SUB ( LALMakeTimestamps ( &status, ×tamps, startTime, duration, Tsft ), &status );
/* ----- allocate memory for AM-coeffs ----- */
AMold.a = XLALCreateREAL4Vector ( timestamps->length );
AMold.b = XLALCreateREAL4Vector ( timestamps->length );
AMnew1.a = XLALCreateREAL4Vector ( timestamps->length );
AMnew1.b = XLALCreateREAL4Vector ( timestamps->length );
AMnew2.a = XLALCreateREAL4Vector ( timestamps->length );
AMnew2.b = XLALCreateREAL4Vector ( timestamps->length );
while ( numChecks-- )
{
/* ----- pick detector-site at random ----- */
pickedSite = floor( 5 * (1.0 * rand() / (RAND_MAX + 1.0) ) ); /* int in [0,5) */
/* NOTE: contrary to ComputeAM() and LALGetAMCoffs(), the new function LALNewGetAMCoeffs()
* computes 'a * sinzeta' and 'b * sinzeta': for the comparison we therefore need to correct
* for GEO's opening-angle of 94.33degrees [JKS98]: */
if ( ! strcmp ( sites[pickedSite], "G1" ) )
sinzeta = 0.997146;
else
sinzeta = 1;
if ( ( det = XLALGetSiteInfo ( sites[pickedSite] )) == NULL )
{
XLALPrintError ("\nCall to XLALGetSiteInfo() has failed for site = '%s'... \n\n",
sites[pickedSite]);
return NEWGETAMCOEFFSTEST_ESUB;
}
/* ----- pick skyposition at random ----- */
alpha = LAL_TWOPI * (1.0 * rand() / ( RAND_MAX + 1.0 ) ); /* uniform in [0, 2pi) */
delta = LAL_PI_2 - acos ( 1 - 2.0 * rand()/RAND_MAX ); /* sin(delta) uniform in [-1,1] */
/* ----- old testing code to put source overhead ----- */
/* alpha = det->frDetector.vertexLongitudeRadians;
delta = det->frDetector.vertexLatitudeRadians; */
/* ===== compute AM-coeffs the 'old way': ===== */
baryinput.site.location[0] = det->location[0]/LAL_C_SI;
baryinput.site.location[1] = det->location[1]/LAL_C_SI;
baryinput.site.location[2] = det->location[2]/LAL_C_SI;
baryinput.alpha = alpha;
baryinput.delta = delta;
baryinput.dInv = 0.e0;
/* amParams structure to compute a(t) and b(t) */
amParams.das = (LALDetAndSource *)LALMalloc(sizeof(LALDetAndSource));
amParams.das->pSource = (LALSource *)LALMalloc(sizeof(LALSource));
amParams.baryinput = &baryinput;
amParams.earth = &earth;
amParams.edat = &edat;
amParams.das->pDetector = det;
amParams.das->pSource->equatorialCoords.longitude = alpha;
amParams.das->pSource->equatorialCoords.latitude = delta;
amParams.das->pSource->orientation = 0.0;
amParams.das->pSource->equatorialCoords.system = COORDINATESYSTEM_EQUATORIAL;
amParams.polAngle = 0;
SUB (LALComputeAM ( &status, &AMold, timestamps->data, &amParams), &status);
/* ===== compute AM-coeffs the 'new way' using LALNewGetAMCoeffs() */
/* ----- get detector-state series ----- */
SUB ( LALGetDetectorStates (&status, &detStates, timestamps, det, &edat, 0 ), &status );
skypos.system = COORDINATESYSTEM_EQUATORIAL;
skypos.longitude = alpha;
skypos.latitude = delta;
/* the 'new' and the 'newer' way ... */
SUB ( LALGetAMCoeffs ( &status, &AMnew1, detStates, skypos ), &status ); /* 'new1' */
SUB ( LALNewGetAMCoeffs ( &status, &AMnew2, detStates, skypos ), &status ); /* 'new2' */
/* ===== analyse relative errors ===== */
maxerr01 = maxerr02 = maxerr12 = 0; /* errors between 0='old', 1='new1', 2='new2' */
averr01 = averr02 = averr12 = 0;
for ( i=0; i < timestamps->length; i ++ )
{
/* printf("GPS time: %d s %d ns; GMST in radians: %f\n",
detStates->data[i].tGPS.gpsSeconds,
detStates->data[i].tGPS.gpsNanoSeconds,
fmod(detStates->data[i].earthState.gmstRad,LAL_TWOPI));
printf("Old AM coeffs: a=%f, b=%f\nNew AM coeffs: a=%f, b=%f\nNEWER AM coeffs: a=%f b=%f",
AMold.a->data[i], AMold.b->data[i],
AMnew.a->data[i], AMnew.b->data[i],
AMnewer.a->data[i], AMnewer.b->data[i]); */
REAL8 thisErr;
/* compare 0-1 */
thisErr = sqrt( SQ ( AMold.a->data[i] - AMnew1.a->data[i] ) / AMold.A );
averr01 += thisErr;
maxerr01 = MYMAX( thisErr, maxerr01 );
thisErr = sqrt( SQ ( AMold.b->data[i] - AMnew1.b->data[i] ) / AMold.B );
averr01 += thisErr;
maxerr01 = MYMAX( thisErr, maxerr01 );
/* compare 0-2 */
thisErr = sqrt( SQ ( AMold.a->data[i] - AMnew2.a->data[i]/sinzeta ) / AMold.A );
averr02 += thisErr;
maxerr02 = MYMAX( thisErr, maxerr02 );
thisErr = sqrt( SQ ( AMold.b->data[i] - AMnew2.b->data[i]/sinzeta ) / AMold.B );
averr02 += thisErr;
maxerr02 = MYMAX( thisErr, maxerr02 );
/* compare 1-2 */
thisErr = sqrt( SQ ( AMnew1.a->data[i] - AMnew2.a->data[i]/sinzeta ) / AMold.A );
averr12 += thisErr;
maxerr12 = MYMAX( thisErr, maxerr12 );
thisErr = sqrt( SQ ( AMnew1.b->data[i] - AMnew2.b->data[i]/sinzeta ) / AMold.B );
averr12 += thisErr;
maxerr12 = MYMAX( thisErr, maxerr12 );
}
averr01 /= 2.0 * timestamps->length;
averr02 /= 2.0 * timestamps->length;
averr12 /= 2.0 * timestamps->length;
if ( lalDebugLevel )
{
printf ("Parameters: IFO = %s, skypos = [%g, %g]\n", sites[pickedSite], alpha, delta );
printf ("Maximal relative errors: maxerr(0-1) = %g %%, maxerr(0-2) = %g %% maxerr(1-2) = %g %%\n",
100.0 * maxerr01, 100.0 * maxerr02, 100.0 * maxerr12 );
printf ("Average relative errors: averr(0-1) = %g %%, averr(0-2) = %g %% averr(1-2) = %g %%\n",
100.0 * averr01, 100.0 * averr02, 100.0 * averr12 );
}
else
printf ("%d %g %g \t %g %g %g \t %g %g %g\n", pickedSite, alpha, delta, averr01, averr02, averr12, maxerr01, maxerr02, maxerr12);
if ( (averr01 > tolerance) || (averr02 > tolerance) || (averr12 > tolerance)
|| (maxerr01 > tolerance) ||(maxerr02 > tolerance) || (maxerr12 > tolerance) )
{
XLALPrintError ("Maximal error-tolerance of %g %% was exceeded!\n", 100.0 * tolerance );
if (!ignoreErrors)
return 1;
}
if ( lalDebugLevel )
printf("%d checks left\n", numChecks);
/* ---- Clean up things that were created in this loop ---- */
XLALDestroyDetectorStateSeries ( detStates );
detStates = NULL;
LALFree ( det );
LALFree ( amParams.das->pSource );
LALFree ( amParams.das );
}
/* ----- free memory ----- */
XLALDestroyTimestampVector ( timestamps );
XLALDestroyREAL4Vector ( AMold.a );
XLALDestroyREAL4Vector ( AMold.b );
XLALDestroyREAL4Vector ( AMnew1.a );
XLALDestroyREAL4Vector ( AMnew1.b );
XLALDestroyREAL4Vector ( AMnew2.a );
XLALDestroyREAL4Vector ( AMnew2.b );
LALFree(edat.ephemE);
LALFree(edat.ephemS);
LALCheckMemoryLeaks();
return 0; /* OK */
} /* main() */
/**
* Very simple test: pick random skyposition, compute a_i, b_i using
* once LALComputeAM() and once LALGetAMCoeffs(), and look at the errors
* sum_i (a_i - a_i')^2
*/
int main(int argc, char *argv[])
{
LALStatus XLAL_INIT_DECL(status);
LIGOTimeGPS startTime = {714180733, 0};
REAL8 duration = 180000; /* 50 hours */
REAL8 Tsft = 1800; /* assume 30min SFTs */
LIGOTimeGPSVector *timestamps = NULL;
DetectorStateSeries *detStates = NULL;
SkyPosition XLAL_INIT_DECL(skypos);
EphemerisData XLAL_INIT_DECL(edat);
BarycenterInput XLAL_INIT_DECL(baryinput);
LALDetector *det = NULL;
AMCoeffs XLAL_INIT_DECL(AMold);
AMCoeffs XLAL_INIT_DECL(AMnew);
REAL8 alpha, delta;
AMCoeffsParams XLAL_INIT_DECL(amParams);
EarthState earth;
UINT4 i;
REAL8 maxerr_a, maxerr_b, averr_a, averr_b;
REAL8 tolerance = 1e-2; /* be generous: allow 1% error */
struct tms buf;
const CHAR *sites[] = {"H1", "L1", "V2", "G1", "T1" };
UINT4 pickedSite;
char earthEphem[] = TEST_DATA_DIR "earth00-19-DE405.dat.gz";
char sunEphem[] = TEST_DATA_DIR "sun00-19-DE405.dat.gz";
if ( argc == 2 && !strcmp(argv[1], "-v1") )
/* init random-generator */
srand ( times(&buf) );
/* ----- init ephemeris ----- */
edat.ephiles.earthEphemeris = earthEphem;
edat.ephiles.sunEphemeris = sunEphem;
SUB ( LALInitBarycenter(&status, &edat), &status);
/* ----- get timestamps ----- */
SUB ( LALMakeTimestamps ( &status, ×tamps, startTime, duration, Tsft ), &status );
/* ----- allocate memory for AM-coeffs ----- */
AMold.a = XLALCreateREAL4Vector ( timestamps->length );
AMold.b = XLALCreateREAL4Vector ( timestamps->length );
AMnew.a = XLALCreateREAL4Vector ( timestamps->length );
AMnew.b = XLALCreateREAL4Vector ( timestamps->length );
/* ----- pick detector-site at random ----- */
pickedSite = floor( 5 * (1.0 * rand() / (RAND_MAX + 1.0) ) ); /* int in [0,5) */
if ( ( det = XLALGetSiteInfo ( sites[pickedSite] )) == NULL )
{
XLALPrintError ("\nCall to XLALGetSiteInfo() has failed for site = '%s'... \n\n",
sites[pickedSite]);
return GETAMCOEFFSTEST_ESUB;
}
/* ----- pick skyposition at random ----- */
alpha = LAL_TWOPI * (1.0 * rand() / ( RAND_MAX + 1.0 ) ); /* uniform in [0, 2pi) */
delta = LAL_PI_2 - acos ( 1 - 2.0 * rand()/RAND_MAX ); /* sin(delta) uniform in [-1,1] */
/* ===== compute AM-coeffs the 'old way': ===== */
baryinput.site.location[0] = det->location[0]/LAL_C_SI;
baryinput.site.location[1] = det->location[1]/LAL_C_SI;
baryinput.site.location[2] = det->location[2]/LAL_C_SI;
baryinput.alpha = alpha;
baryinput.delta = delta;
baryinput.dInv = 0.e0;
/* amParams structure to compute a(t) and b(t) */
amParams.das = (LALDetAndSource *)LALMalloc(sizeof(LALDetAndSource));
amParams.das->pSource = (LALSource *)LALMalloc(sizeof(LALSource));
amParams.baryinput = &baryinput;
amParams.earth = &earth;
amParams.edat = &edat;
amParams.das->pDetector = det;
amParams.das->pSource->equatorialCoords.longitude = alpha;
amParams.das->pSource->equatorialCoords.latitude = delta;
amParams.das->pSource->orientation = 0.0;
amParams.das->pSource->equatorialCoords.system = COORDINATESYSTEM_EQUATORIAL;
amParams.polAngle = 0;
SUB (LALComputeAM ( &status, &AMold, timestamps->data, &amParams), &status);
/* ===== compute AM-coeffs the 'new way' using LALGetAMCoeffs() */
/* ----- get detector-state series ----- */
SUB ( LALGetDetectorStates (&status, &detStates, timestamps, det, &edat, 0 ), &status );
skypos.system = COORDINATESYSTEM_EQUATORIAL;
skypos.longitude = alpha;
skypos.latitude = delta;
SUB ( LALGetAMCoeffs ( &status, &AMnew, detStates, skypos ), &status );
/* ===== analyse relative error ===== */
maxerr_a = maxerr_b = averr_a = averr_b = 0;
for ( i=0; i < timestamps->length; i ++ )
{
REAL8 thisErr;
thisErr = sqrt( SQ ( AMold.a->data[i] - AMnew.a->data[i] ) / AMold.A );
averr_a += thisErr;
maxerr_a = MYMAX( thisErr, maxerr_a );
thisErr = sqrt( SQ ( AMold.b->data[i] - AMnew.b->data[i] ) / AMold.B );
averr_b += thisErr;
maxerr_b = MYMAX( thisErr, maxerr_b );
}
averr_a /= timestamps->length;
averr_b /= timestamps->length;
if ( lalDebugLevel )
{
printf ("Parameters: IFO = %s, skypos = [%g, %g]\n", sites[pickedSite], alpha, delta );
printf ("Maximal relative errors: maxerr(a) = %g %%, maxerr(b) = %g %% \n",
100.0 * maxerr_a, 100.0 * maxerr_b);
printf ("Average relative errors: averr(a) = %g %%, averr(b) = %g %% \n",
100.0 * averr_a, 100.0 * averr_b );
}
else
printf ("%d %g %g %g %g %g %g \n", pickedSite, alpha, delta, averr_a, averr_b, maxerr_a, maxerr_b);
if ( (averr_a > tolerance) || (averr_b > tolerance) || (maxerr_a > tolerance) ||(maxerr_b > tolerance))
{
XLALPrintError ("Maximal error-tolerance of %g %% was exceeded!\n", 100.0 * tolerance );
return 1;
}
/* ----- free memory ----- */
XLALDestroyTimestampVector ( timestamps );
XLALDestroyREAL4Vector ( AMold.a );
XLALDestroyREAL4Vector ( AMold.b );
XLALDestroyREAL4Vector ( AMnew.a );
XLALDestroyREAL4Vector ( AMnew.b );
LALFree ( det );
XLALDestroyDetectorStateSeries ( detStates );
LALFree ( amParams.das->pSource );
LALFree ( amParams.das );
LALFree(edat.ephemE);
LALFree(edat.ephemS);
LALCheckMemoryLeaks();
return 0; /* OK */
} /* main() */
/**
* Handle user-input and check its validity.
* Load ephemeris and calculate AM-coefficients (stored globally)
*/
void
Initialize (LALStatus *status, struct CommandLineArgsTag *CLA)
{
EphemerisData *edat=NULL; /* Stores earth/sun ephemeris data for barycentering */
BarycenterInput baryinput; /* Stores detector location and other barycentering data */
EarthState earth;
AMCoeffsParams *amParams;
LIGOTimeGPS *midTS=NULL; /* Time stamps for amplitude modulation coefficients */
LALDetector *Detector; /* Our detector*/
INT4 k;
INITSTATUS(status);
ATTATCHSTATUSPTR (status);
if ( XLALUserVarWasSet ( &(CLA->nTsft) ) )
CLA->duration = 1.0 * CLA->nTsft * CLA->Tsft;
/* read or generate SFT timestamps */
if ( XLALUserVarWasSet(&(CLA->timestamps)) )
{
XLAL_CHECK_LAL ( status, ( timestamps = XLALReadTimestampsFile ( CLA->timestamps ) ) != NULL, XLAL_EFUNC );
if ( (CLA->nTsft > 0) && ( (UINT4)CLA->nTsft < timestamps->length ) ) /* truncate if required */
timestamps->length = CLA->nTsft;
CLA->nTsft = timestamps->length;
} /* if have_timestamps */
else
{
LIGOTimeGPS tStart;
tStart.gpsSeconds = CLA->gpsStart;
tStart.gpsNanoSeconds = 0;
XLAL_CHECK_LAL ( status, ( timestamps = XLALMakeTimestamps( tStart, CLA->duration, CLA->Tsft, 0 ) ) != NULL, XLAL_EFUNC );
CLA->nTsft = timestamps->length;
} /* no timestamps */
/*---------- initialize detector ---------- */
{
BOOLEAN have_IFO = XLALUserVarWasSet ( &CLA->IFO );
BOOLEAN have_detector = XLALUserVarWasSet ( &CLA->detector );
CHAR *IFO;
if ( !have_IFO && !have_detector ) {
fprintf (stderr, "\nNeed to specify the detector (--IFO) !\n\n");
ABORT (status, SEMIANALYTIC_EINPUT, SEMIANALYTIC_MSGEINPUT);
}
if ( have_IFO )
IFO = CLA->IFO;
else
IFO = CLA->detector;
if ( ( Detector = XLALGetSiteInfo ( IFO ) ) == NULL ) {
ABORT (status, SEMIANALYTIC_EINPUT, SEMIANALYTIC_MSGEINPUT);
}
}
/* ---------- load ephemeris-files ---------- */
{
edat = XLALInitBarycenter( CLA->ephemEarth, CLA->ephemSun );
if ( !edat ) {
XLALPrintError("XLALInitBarycenter failed: could not load Earth ephemeris '%s' and Sun ephemeris '%s'\n", CLA->ephemEarth, CLA->ephemSun);
ABORT (status, SEMIANALYTIC_EINPUT, SEMIANALYTIC_MSGEINPUT);
}
} /* ephemeris-reading */
/* ---------- calculate AM-coefficients ---------- */
/* prepare call to barycentering routing */
baryinput.site.location[0] = Detector->location[0]/LAL_C_SI;
baryinput.site.location[1] = Detector->location[1]/LAL_C_SI;
baryinput.site.location[2] = Detector->location[2]/LAL_C_SI;
baryinput.alpha = CLA->Alpha;
baryinput.delta = CLA->Delta;
baryinput.dInv = 0.e0;
/* amParams structure to compute a(t) and b(t) */
/* Allocate space for amParams stucture */
/* Here, amParams->das is the Detector and Source info */
amParams = (AMCoeffsParams *)LALMalloc(sizeof(AMCoeffsParams));
amParams->das = (LALDetAndSource *)LALMalloc(sizeof(LALDetAndSource));
amParams->das->pSource = (LALSource *)LALMalloc(sizeof(LALSource));
/* Fill up AMCoeffsParams structure */
amParams->baryinput = &baryinput;
amParams->earth = &earth;
amParams->edat = edat;
amParams->das->pDetector = Detector;
amParams->das->pSource->equatorialCoords.system = COORDINATESYSTEM_EQUATORIAL;
amParams->das->pSource->equatorialCoords.longitude = CLA->Alpha;
amParams->das->pSource->equatorialCoords.latitude = CLA->Delta;
amParams->das->pSource->orientation = 0.0;
amParams->polAngle = amParams->das->pSource->orientation ; /* These two have to be the same!!!!!!!!!*/
/* Allocate space for AMCoeffs */
XLAL_INIT_MEM(amc);
TRY ( LALSCreateVector(status->statusPtr, &(amc.a), (UINT4) CLA->nTsft), status);
TRY ( LALSCreateVector(status->statusPtr, &(amc.b), (UINT4) CLA->nTsft), status);
/* Mid point of each SFT */
midTS = (LIGOTimeGPS *)LALCalloc(CLA->nTsft,sizeof(LIGOTimeGPS));
for(k=0; k < CLA->nTsft; k++)
{
/* FIXME: loss of precision; consider
midTS[k] = timestamps->data[k];
XLALGPSAdd(&midTS[k], 0.5*CLA->Tsft);
*/
REAL8 teemp=0.0;
teemp = XLALGPSGetREAL8(&(timestamps->data[k]));
teemp += 0.5*CLA->Tsft;
XLALGPSSetREAL8(&(midTS[k]), teemp);
}
TRY ( LALComputeAM(status->statusPtr, &amc, midTS, amParams), status);
/* Free memory */
XLALDestroyTimestampVector ( timestamps);
LALFree(midTS);
LALFree(Detector);
XLALDestroyEphemerisData(edat);
LALFree(amParams->das->pSource);
LALFree(amParams->das);
LALFree(amParams);
DETATCHSTATUSPTR (status);
RETURN(status);
} /* ParseUserInput() */
int main(int argc, char *argv[]){
/* LALStatus pointer */
static LALStatus status;
/* time and velocity */
static LIGOTimeGPSVector timeV;
REAL8 timeBase;
LALDetector *det;
DetectorStateSeries *detStates=NULL;
/* ephemeris */
EphemerisData *edat=NULL;
/* user input variables */
BOOLEAN uvar_help;
CHAR *uvar_earthEphemeris=NULL;
CHAR *uvar_sunEphemeris=NULL;
CHAR *uvar_sftDir=NULL;
/* Set up the default parameters */
/* LAL error-handler */
lal_errhandler = LAL_ERR_EXIT;
uvar_help = FALSE;
uvar_earthEphemeris = (CHAR *)LALCalloc( 512 , sizeof(CHAR));
strcpy(uvar_earthEphemeris,EARTHEPHEMERIS);
uvar_sunEphemeris = (CHAR *)LALCalloc( 512 , sizeof(CHAR));
strcpy(uvar_sunEphemeris,SUNEPHEMERIS);
/* register user input variables */
LAL_CALL( LALRegisterBOOLUserVar( &status, "help", 'h', UVAR_HELP, "Print this message", &uvar_help), &status);
LAL_CALL( LALRegisterSTRINGUserVar( &status, "earthEphemeris", 'E', UVAR_REQUIRED, "Earth Ephemeris file", &uvar_earthEphemeris), &status);
LAL_CALL( LALRegisterSTRINGUserVar( &status, "sunEphemeris", 'S', UVAR_REQUIRED, "Sun Ephemeris file", &uvar_sunEphemeris), &status);
LAL_CALL( LALRegisterSTRINGUserVar( &status, "sftDir", 'D', UVAR_REQUIRED, "SFT filename pattern", &uvar_sftDir), &status);
/* read all command line variables */
LAL_CALL( LALUserVarReadAllInput(&status, argc, argv), &status);
/* exit if help was required */
if (uvar_help)
exit(0);
/* get ephemeris */
edat = (EphemerisData *)LALCalloc(1, sizeof(EphemerisData));
(*edat).ephiles.earthEphemeris = uvar_earthEphemeris;
(*edat).ephiles.sunEphemeris = uvar_sunEphemeris;
LAL_CALL( LALInitBarycenter( &status, edat), &status);
/* read sft Files and set up weights and nstar vector */
{
/* new SFT I/O data types */
SFTCatalog *catalog = NULL;
static SFTConstraints constraints;
UINT4 k;
/* set detector constraint */
constraints.detector = NULL;
/* get sft catalog */
LAL_CALL( LALSFTdataFind( &status, &catalog, uvar_sftDir, &constraints), &status);
if ( (catalog == NULL) || (catalog->length == 0) ) {
fprintf (stderr,"Unable to match any SFTs with pattern '%s'\n", uvar_sftDir );
exit(1);
}
for (k = 0; k < catalog->length; k++) {
det = XLALGetSiteInfo ( catalog->data[k].header.name);
timeBase = 1./catalog->data[k].header.deltaF;
timeV.length = 1;
timeV.deltaT = timeBase;
timeV.data = &(catalog->data[k].header.epoch);
LAL_CALL( LALGetDetectorStates ( &status, &detStates, &timeV, det, edat, 0.5*timeBase), &status);
fprintf(stdout, "%g %g %g\n", detStates->data[0].vDetector[0], detStates->data[0].vDetector[1],
detStates->data[0].vDetector[2]);
LALDestroyDetectorStateSeries (&status, &detStates );
LALFree (det);
} /* end loop over sfts */
LAL_CALL( LALDestroySFTCatalog( &status, &catalog ), &status);
} /* end of sft reading block */
LALFree(edat->ephemE);
LALFree(edat->ephemS);
LALFree(edat);
LAL_CALL (LALDestroyUserVars(&status), &status);
LALCheckMemoryLeaks();
if ( lalDebugLevel )
REPORTSTATUS ( &status);
return status.statusCode;
}
/* ----- function definitions ---------- */
int main(int argc, char *argv[])
{
int opt; /* Command-line option. */
UINT4 numIFOs = 2;
const CHAR *sites[2] = {"H1", "V1"};
UINT4 startTime = 714180733;
UINT4 duration = 180000; /* 50 hours */
UINT4 Tsft = 1800; /* assume 30min SFTs */
REAL8 tolerance = 2e-6; /* same algorithm, should be basically identical results */
char earthEphem[] = TEST_DATA_DIR "earth00-19-DE405.dat.gz";
char sunEphem[] = TEST_DATA_DIR "sun00-19-DE405.dat.gz";
UINT4 numChecks = 1; /* Number of times to check */
/* read user input */
while ((opt = LALgetopt( argc, argv, "n:qv:" )) != -1) {
switch (opt) {
case 'v': /* set lalDebugLevel */
break;
case 'n': /* number of times to check */
numChecks = atoi( LALoptarg );
break;
}
}
/* init random-generator */
struct tms buf;
UINT4 seed = times(&buf);
srand ( seed );
XLALPrintInfo ("%s: seed used = %d\n", __func__, seed );
/* ----- init ephemeris ----- */
EphemerisData *edat;
if ( (edat = XLALInitBarycenter ( earthEphem, sunEphem )) == NULL ) {
XLALPrintError ("%s: XLALInitBarycenter() failed with xlalErrno = %d\n", __func__, xlalErrno );
return XLAL_EFAILED;
}
/* ----- init detector info ---------- */
UINT4 X;
MultiLALDetector multiDet;
multiDet.length = numIFOs;
for (X=0; X < numIFOs; X ++ )
{
LALDetector *site;
if ( (site = XLALGetSiteInfo ( sites[X] )) == NULL ) {
XLALPrintError ("%s: Failed to get site-info for detector '%s'\n", __func__, sites[X] );
return XLAL_EFAILED;
}
multiDet.sites[X] = (*site); /* copy! */
XLALFree ( site );
}
/* ----- init multi-IFO timestamps vector ---------- */
UINT4 numSteps = (UINT4) ceil ( duration / Tsft );
MultiLIGOTimeGPSVector * multiTS;
if ( (multiTS = XLALCalloc ( 1, sizeof(*multiTS))) == NULL ) {
XLAL_ERROR ( XLAL_ENOMEM );
}
multiTS->length = numIFOs;
if ( (multiTS->data = XLALCalloc (numIFOs, sizeof(*multiTS->data))) == NULL ) {
XLAL_ERROR ( XLAL_ENOMEM );
}
for ( X=0; X < numIFOs; X ++ )
{
if ( (multiTS->data[X] = XLALCreateTimestampVector (numSteps)) == NULL ) {
XLALPrintError ("%s: XLALCreateTimestampVector(%d) failed.\n", __func__, numSteps );
return XLAL_EFAILED;
}
multiTS->data[X]->deltaT = Tsft;
UINT4 i;
for ( i=0; i < numSteps; i ++ )
{
UINT4 ti = startTime + i * Tsft;
multiTS->data[X]->data[i].gpsSeconds = ti;
multiTS->data[X]->data[i].gpsNanoSeconds = 0;
} /* for i < numSteps */
} /* for X < numIFOs */
/* ---------- compute multi-detector states -------------------- */
MultiDetectorStateSeries *multiDetStates;
if ( (multiDetStates = XLALGetMultiDetectorStates ( multiTS, &multiDet, edat, 0.5 * Tsft )) == NULL ) {
XLALPrintError ( "%s: XLALGetMultiDetectorStates() failed.\n", __func__ );
return XLAL_EFAILED;
}
XLALDestroyMultiTimestamps ( multiTS );
XLALDestroyEphemerisData ( edat );
/* ========== MAIN LOOP: N-trials of comparisons XLAL <--> LAL multiAM functions ========== */
while ( numChecks-- )
{
LALStatus XLAL_INIT_DECL(status);
/* ----- pick skyposition at random ----- */
SkyPosition skypos;
skypos.longitude = LAL_TWOPI * (1.0 * rand() / ( RAND_MAX + 1.0 ) ); /* uniform in [0, 2pi) */
skypos.latitude = LAL_PI_2 - acos ( 1 - 2.0 * rand()/RAND_MAX ); /* sin(delta) uniform in [-1,1] */
skypos.system = COORDINATESYSTEM_EQUATORIAL;
MultiNoiseWeights *weights = NULL; /* for now we only deal with unit-weights case */
/* ----- compute multiAM using LAL function ----- */
MultiAMCoeffs *multiAM_LAL = NULL;
LALGetMultiAMCoeffs ( &status, &multiAM_LAL, multiDetStates, skypos );
if ( status.statusCode ) {
XLALPrintError ("%s: LALGetMultiAMCoeffs() failed with statusCode = %d : %s\n", __func__, status.statusCode, status.statusDescription );
return XLAL_EFAILED;
}
if ( XLALWeightMultiAMCoeffs ( multiAM_LAL, weights ) != XLAL_SUCCESS ) {
XLALPrintError ("%s: XLALWeightMultiAMCoeffs() failed with xlalErrno = %d\n", __func__, xlalErrno );
return XLAL_EFAILED;
}
/* ----- compute multiAM using XLAL function ----- */
MultiAMCoeffs *multiAM_XLAL;
if ( ( multiAM_XLAL = XLALComputeMultiAMCoeffs ( multiDetStates, weights, skypos )) == NULL ) {
XLALPrintError ("%s: XLALComputeMultiAMCoeffs() failed with xlalErrno = %d\n", __func__, xlalErrno );
return XLAL_EFAILED;
}
/* now run comparison */
if ( XLALCompareMultiAMCoeffs ( multiAM_XLAL, multiAM_LAL, tolerance ) != XLAL_SUCCESS ) {
XLALPrintError ("%s: comparison between multiAM_XLAL and multiAM_LAL failed.\n", __func__ );
return XLAL_EFAILED;
}
/* free memory created inside this loop */
XLALDestroyMultiAMCoeffs ( multiAM_LAL );
XLALDestroyMultiAMCoeffs ( multiAM_XLAL );
} /* for numChecks */
/* we're done: free memory */
XLALDestroyMultiDetectorStateSeries ( multiDetStates );
LALCheckMemoryLeaks();
printf ("OK. All tests passed successfully\n\n");
return 0; /* OK */
} /* main() */
