//=============================================================================
// General test for the SP3EphemerisStore
// Makes sure SP3EphemerisStore can be instantiated and can load
// a file; also ensures that nonexistent files throw an exception
//=============================================================================
int SP3ESTest(void)
{
TUDEF( "SP3EphemerisStore", "Constructor" );
// Verify the consturctor builds the SP3EphemerisStore object
try
{
SP3EphemerisStore store;
TUPASS("SP3EphemerisStore object successfully created");
}
catch (...)
{
TUFAIL("SP3EphemerisStore object could not be created");
}
SP3EphemerisStore store;
// Verify opening an empty file throws an error
try
{
store.loadFile(inputNotaFile);
TUFAIL("Opening an empty file did not throw an exception");
}
catch (Exception& e)
{
TUPASS("Opening an empty file threw the correct exception");
}
catch (...)
{
TUFAIL("Opening an empty file caused an unexpected exception");
}
// Verify opening a file works with no errors
try
{
/*
fstream smoo;
smoo.open(inputSP3Data.c_str(),std::ios::in);
testFramework.assert(smoo, "plain file open fail", __LINE__);
smoo.close();
cerr << "-------------------------" << endl;
*/
store.loadFile(inputSP3Data);
// cerr << "-------------------------" << endl;
TUPASS("Opening a valid file works with no exceptions");
}
catch (...)
{
// cerr << "-------------------------" << endl;
TUFAIL("Exception thrown when opening a valid file");
}
// Write the dump of the loaded file
ofstream DumpData;
DumpData.open (outputDataDump.c_str());
store.dump(DumpData,1);
DumpData.close();
return testFramework.countFails();
}
gpstk::CommonTime compSatVis::setStartTime()
{
CommonTime retDT = GPSWeekSecond( 621, 0.0 ); // 12/1/1991
CommonTime initialTime;
CommonTime finalTime;
switch(navFileType)
{
case FIC_EPH:
case RINEX_NAV:
initialTime = BCEphList.getInitialTime();
finalTime = BCEphList.getFinalTime();
break;
case FIC_ALM:
initialTime = BCAlmList.getInitialTime();
finalTime = BCAlmList.getFinalTime();
break;
case Yuma_ALM:
initialTime = YumaAlmStore.getInitialTime();
finalTime = YumaAlmStore.getFinalTime();
break;
case SEM_ALM:
initialTime = SEMAlmStore.getInitialTime();
finalTime = SEMAlmStore.getFinalTime();
break;
// If loading "day at a time" files, will need
// three days to cover middle day. We need to
// find the middle of whatever period was loaded
// and back up to the beginning of that day.
case SP3:
{
initialTime = SP3EphList.getInitialTime();
finalTime = SP3EphList.getFinalTime();
break;
}
}
double diff = finalTime - initialTime;
retDT = initialTime;
retDT += diff/2.0;
retDT = YDSTime( static_cast<YDSTime>(retDT).year, static_cast<YDSTime>(retDT).doy, 0.0 );
return(retDT);
}
//=============================================================================
// Test for getFinalTime
// Tests getFinalTime method in SP3EphemerisStore by ensuring that
// the method outputs the final time stamp in an SP3 file
//=============================================================================
int getFinalTimeTest (void)
{
TUDEF( "SP3EphemerisStore", "getFinalTime" );
try
{
SP3EphemerisStore store;
store.loadFile(inputSP3Data);
CommonTime computedFinalTime = store.getFinalTime();
CivilTime knownFinalTime_civ(1997,4,6,23,45,0);
CommonTime knownFinalTime = knownFinalTime_civ.convertToCommonTime();
// Check that the function returns the initial time from the file
TUASSERTE(CommonTime, knownFinalTime, computedFinalTime);
}
catch (...)
{
TUFAIL("Unexpected exception");
}
return testFramework.countFails();
}
//------------------------------------------------------------------------------------
//------------------------------------------------------------------------------------
int FillEphemerisStore(const vector<string>& files, SP3EphemerisStore& PE,
GPSEphemerisStore& BCE)
{
try
{
int nread = 0;
Rinex3NavHeader rnh;
Rinex3NavData rne;
for(size_t nfile = 0; nfile < files.size(); nfile++) {
if(files[nfile].empty()) {
Exception e("File name is empty");
GPSTK_THROW(e);
}
if(isRinex3NavFile(files[nfile]) || isRinexNavFile(files[nfile])) {
Rinex3NavStream instrm(files[nfile].c_str());
instrm.exceptions(fstream::failbit);
try {
instrm >> rnh;
while (instrm >> rne) {
// check health...
if(rne.health == 0)
BCE.addEphemeris(rne);
}
nread++;
}
catch(Exception& e) {
GPSTK_RETHROW(e);
}
}
else if(isSP3File(files[nfile])) {
try {
PE.loadFile(files[nfile]);
nread++;
}
catch(Exception& e) { GPSTK_RETHROW(e); }
}
else {
Exception e("File " + files[nfile]
+ " is neither Rinex Nav nor SP3 file.");
GPSTK_THROW(e);
}
}
void compSatVis::computeVisibility( gpstk::CommonTime currT )
{
gpstk::Position SVpos[gpstk::MAX_PRN+1];
bool SVAvail[gpstk::MAX_PRN+1];
Xvt SVxvt;
// Compute SV positions for this epoch
int PRNID;
for (PRNID=1;PRNID<=gpstk::MAX_PRN;++PRNID)
{
SVAvail[PRNID] = false;
try
{
SatID satid(PRNID,SatID::systemGPS);
switch(navFileType)
{
case FIC_EPH:
case RINEX_NAV:
SVxvt = BCEphList.getXvt( satid, currT );
break;
case FIC_ALM:
SVxvt = BCAlmList.getXvt( satid, currT );
break;
case Yuma_ALM:
SVxvt = YumaAlmStore.getXvt( satid, currT );
break;
case SEM_ALM:
SVxvt = SEMAlmStore.getXvt( satid, currT );
break;
case SP3:
SVxvt = SP3EphList.getXvt( satid, currT );
break;
default:
cerr << "Unknown navigation file type in computeVisibility()." << endl;
cerr << "Fatal error. compSatVis will halt." << endl;
exit(1);
}
SVpos[PRNID] = SVxvt.x;
SVAvail[PRNID] = true;
}
catch(InvalidRequest& e)
{
continue;
}
}
// If first time through, print the detail hearder if required.
if (detailPrint && currT==startT)
{
fprintf(logfp," Number of Stations visible to each SV by epoch\n");
fprintf(logfp," PRN, ");
for (int pi=1;pi<=gpstk::MAX_PRN;++pi)
{
if (SVAvail[pi]) fprintf(logfp," %4d,",pi);
}
fprintf(logfp," Max, Min\n");
}
if (detailPrint) fprintf(logfp,"%s, ",printTime(currT,"%02H:%02M").c_str());
// Now count number of Stations visible to each SV
int maxNum = 0;
int minNum = stationPositions.size() + 1;
StaPosList::const_iterator splCI;
DiscreteVisibleCounts& dvc0 = dvcList.find(0)->second;
for (PRNID=1;PRNID<=gpstk::MAX_PRN;++PRNID)
{
if (!SVAvail[PRNID]) continue;
int numVis = 0;
for (splCI =stationPositions.begin();
splCI!=stationPositions.end();
++splCI)
{
Position staPos = splCI->second;
double elv = staPos.elvAngle( SVpos[PRNID] );
if (elv>=minimumElevationAngle) numVis++;
}
if (detailPrint) fprintf(logfp," %2d,",numVis);
if (numVis>maxNum) maxNum = numVis;
if (numVis<minNum) minNum = numVis;
StaStatsList::iterator sslI = staStatsList.find( PRNID );
if (sslI==staStatsList.end())
{
cerr << "Missing statistics object for satellite " << PRNID << endl;
cerr << "Fatal error. compSatVis will termination." << endl;
}
StaStats& ss = sslI->second;
ss.addEpochInfo( numVis, epochCount );
statsOverAllPRNs.addEpochInfo( numVis, epochCount );
DiscreteVisibleCounts& dvc = dvcList.find(PRNID)->second;
dvc.addCount(numVis);
dvc0.addCount(numVis);
}
if (detailPrint) fprintf(logfp," %2d, %2d\n",maxNum,minNum);
}
void compSatVis::printNavFileReferenceTime(FILE* logfp)
{
string tform2 = "%02m/%02d/%02y DOY %03j, GPS Week %F, DOW %w, %02H:%02M:%02S";
CommonTime t;
// If the user did not specify a start time for the evaulation, find the
// epoch time of the navigation data set and work from that.
// In the case of almanac data, the "initial time" is derived from the
// earliest almanac reference time minus a half week. Therefore, we
// add the halfweek back in.
switch(navFileType)
{
// For ephemeris, initial time is earliest beginning of effectivty.
case FIC_EPH:
case RINEX_NAV:
t = BCEphList.getInitialTime();
t += HALFWEEK;
fprintf(logfp," Ephemeris effectivity\n");
fprintf(logfp," Earliest : %s\n",
printTime(t,tform2).c_str());
t = BCEphList.getFinalTime();
t -= HALFWEEK;
fprintf(logfp," Latest : %s\n",
printTime(t,tform2).c_str());
break;
case FIC_ALM:
t = BCAlmList.getInitialTime();
t += HALFWEEK;
fprintf(logfp," Almanac reference time\n");
fprintf(logfp," Earliest : %s\n",
printTime(t,tform2).c_str());
t = BCAlmList.getFinalTime();
t -= HALFWEEK;
fprintf(logfp," Latest : %s\n",
printTime(t,tform2).c_str());
break;
case Yuma_ALM:
t = YumaAlmStore.getInitialTime();
t += HALFWEEK;
fprintf(logfp," Almanac reference time\n");
fprintf(logfp," Earliest : %s\n",
printTime(t,tform2).c_str());
t = YumaAlmStore.getFinalTime();
t -= HALFWEEK;
fprintf(logfp," Latest : %s\n",
printTime(t,tform2).c_str());
break;
case SEM_ALM:
t = SEMAlmStore.getInitialTime();
t += HALFWEEK;
fprintf(logfp," Almanac reference time\n");
fprintf(logfp," Earliest : %s\n",
printTime(t,tform2).c_str());
t = SEMAlmStore.getFinalTime();
t -= HALFWEEK;
fprintf(logfp," Latest : %s\n",
printTime(t,tform2).c_str());
break;
case SP3:
{
CommonTime begin = SP3EphList.getInitialTime();
CommonTime end = SP3EphList.getFinalTime();
fprintf(logfp," Ephemeris effectivity\n");
fprintf(logfp," Earliest : %s\n",
printTime(begin,tform2).c_str());
fprintf(logfp," Latest : %s\n",
printTime(end,tform2).c_str());
break;
}
}
return;
}
//=============================================================================
// Test for getVelocity
// Tests getPosition method in SP3EphemerisStore by comparing the outputs
// of the method to known values in an SP3 files with position and
// velocity values
//=============================================================================
int getVelocityTest (void)
{
TUDEF( "SP3EphemerisStore", "getVelocity" );
try
{
SP3EphemerisStore Store;
Store.loadFile(inputAPCData);
const short PRN1 = 1;
const short PRN31 = 31;
CivilTime testTime_civ(2001,7,22,2,0,0);
CommonTime testTime = testTime_civ.convertToCommonTime();
SatID sid1(PRN1,SatID::systemGPS);
SatID sid31(PRN31,SatID::systemGPS);
Triple computedVelocity_1 = Store.getVelocity(sid1,testTime);
Triple computedVelocity_31 = Store.getVelocity(sid31,testTime);
Triple knownVelocity_1(1541.6040306,-2000.8516260,-1256.4479944);
Triple knownVelocity_31(1165.3672035,-1344.4254143,2399.1497704);
double relativeError;
std::stringstream testMessageStream;
std::string testMessageP2,
testMessageP1 = "getVelocity obtained the wrong velocity in the ";
//--------------------------------------------------------------------
// Check that the computed position matches the known value for SatID 1
//--------------------------------------------------------------------
testMessageP2 = " direction for SatID 1";
for (int i = 0; i < 3; i++)
{
testMessageStream << testMessageP1 << i << testMessageP2;
relativeError = fabs(knownVelocity_1[i] - computedVelocity_1[i]) /fabs(
computedVelocity_1[i] );
testFramework.assert( relativeError < epsilon , testMessageStream.str() ,
__LINE__);
testMessageStream.str(std::string());
}
//--------------------------------------------------------------------
// Check that the computed position matches the known value for SatID 1
//--------------------------------------------------------------------
testMessageP2 = " direction for SatID 31";
for (int i = 0; i < 3; i++)
{
testMessageStream << testMessageP1 << i << testMessageP2;
relativeError = fabs(knownVelocity_31[i] - computedVelocity_31[i])/fabs(
computedVelocity_31[i]);
testFramework.assert( relativeError < epsilon , testMessageStream.str() ,
__LINE__);
testMessageStream.str(std::string());
}
}
catch (...)
{
TUFAIL("Unexpected exception");
}
return testFramework.countFails();
}
//=============================================================================
// Test for getPosition
// Tests getPosition method in SP3EphemerisStore by comparing the outputs
// of the method to known values in two SP3 files--one with position and
// velocity values and one with only position values
//=============================================================================
int getPositionTest (void)
{
TUDEF( "SP3EphemerisStore", "getPosition" );
try
{
SP3EphemerisStore igsStore;
igsStore.loadFile(inputSP3Data);
const short PRN1 = 1;
const short PRN31 = 31;
CivilTime igsTime_civ(1997,4,6,2,0,0);
CommonTime igsTime = igsTime_civ.convertToCommonTime();
SatID sid1(PRN1,SatID::systemGPS);
SatID sid31(PRN31,SatID::systemGPS);
Triple computedPosition_igs1 = igsStore.getPosition(sid1,igsTime);
Triple computedPosition_igs31 = igsStore.getPosition(sid31,igsTime);
Triple knownPosition_igs1(-17432922.132,6688018.407,-18768291.053);
Triple knownPosition_igs31(-5075919.490,25101160.691,-6633797.696);
double relativeError;
std::stringstream testMessageStream;
std::string testMessageP1 = "getPosition obtained the wrong position in the ";
std::string testMessageP2 = " direction for SatID 1";
//--------------------------------------------------------------------
// Check that the computed position matches the known value for SatID 1
//--------------------------------------------------------------------
for (int i = 0; i < 3; i++)
{
testMessageStream << testMessageP1 << i << testMessageP2;
relativeError = fabs(knownPosition_igs1[i] - computedPosition_igs1[i]) /fabs(
knownPosition_igs1[i] );
testFramework.assert( relativeError < epsilon , testMessageStream.str() ,
__LINE__);
testMessageStream.str(std::string());
}
//--------------------------------------------------------------------
// Check that the computed position matches the known value for SatID 31
//--------------------------------------------------------------------
testMessageP2 = " direction for SatID 31";
for (int i = 0; i < 3; i++)
{
testMessageStream << testMessageP1 << i << testMessageP2;
relativeError = fabs(knownPosition_igs31[i] -
computedPosition_igs31[i]) /fabs(knownPosition_igs31[i] );
testFramework.assert( relativeError < epsilon , testMessageStream.str() ,
__LINE__);
testMessageStream.str(std::string());
}
SP3EphemerisStore apcStore;
apcStore.loadFile(inputAPCData);
CivilTime apcTime_civ(2001,7,22,2,0,0);
CommonTime apcTime = apcTime_civ.convertToCommonTime();
Triple computedPosition_apc1 = apcStore.getPosition(sid1,apcTime);
Triple computedPosition_apc31 = apcStore.getPosition(sid31,apcTime);
Triple knownPosition_apc1(-5327654.053,-16633919.811,20164748.602);
Triple knownPosition_apc31(2170451.938,-22428932.839,-14059088.503);
//--------------------------------------------------------------------
// Check that the computed position matches the known value for SatID 1
//--------------------------------------------------------------------
testMessageP2 = " direction for SatID 1";
for (int i = 0; i < 3; i++)
{
testMessageStream << testMessageP1 << i << testMessageP2;
relativeError = fabs(knownPosition_apc1[i] - computedPosition_apc1[i]) /fabs(
knownPosition_apc1[i] );
testFramework.assert( relativeError < epsilon , testMessageStream.str() ,
__LINE__);
testMessageStream.str(std::string());
}
//--------------------------------------------------------------------
// Check that the computed position matches the known value for SatID 31
//--------------------------------------------------------------------
testMessageP2 = " direction for SatID 31";
for (int i = 0; i < 3; i++)
{
testMessageStream << testMessageP1 << i << testMessageP2;
relativeError = fabs(knownPosition_apc31[i] -
computedPosition_apc31[i]) /fabs(knownPosition_apc31[i] );
testFramework.assert( relativeError < epsilon , testMessageStream.str() ,
__LINE__);
testMessageStream.str(std::string());
}
}
catch (...)
{
TUFAIL("Unexpected exception");
}
return testFramework.countFails();
}
//=============================================================================
// Test for getXvt.
// Tests the getXvt method in SP3EphemerisStore by comparing known
// results with the method's output for various time stamps in an
// SP3 file; also ensures nonexistent SatIDs throw an exception
//=============================================================================
int getXvtTest (void)
{
TUDEF( "SP3EphemerisStore", "getXvt" );
try
{
SP3EphemerisStore store;
store.loadFile(inputSP3Data);
stringstream outputStream1;
stringstream outputStream15;
stringstream outputStream31;
const short PRN0 = 0; // Nonexistent in SP3 file
const short PRN1 = 1;
const short PRN15 = 15;
const short PRN31 = 31;
const short PRN32 = 32; // Nonexistent in SP3 file
SatID sid0(PRN0,SatID::systemGPS);
SatID sid1(PRN1,SatID::systemGPS);
SatID sid15(PRN15,SatID::systemGPS);
SatID sid31(PRN31,SatID::systemGPS);
SatID sid32(PRN32,SatID::systemGPS);
CivilTime eTime_civ(1997,4,6,6,15,0); // Time stamp of one epoch
CommonTime eTime = eTime_civ.convertToCommonTime();
CivilTime bTime_civ(1997,4,6,0,0,0); // Time stamp of first epoch
CommonTime bTime = bTime_civ.convertToCommonTime();
try
{
// Verify that an InvalidRequest exception is thrown when SatID is not in the data
try
{
store.getXvt(sid0,bTime);
TUFAIL("No exception thrown when getXvt looks for an invalid"
" SatID");
}
catch (InvalidRequest& e)
{
TUPASS("Expected exception thrown when getXvt looks for an invalid"
" SatID");
}
catch (...)
{
TUFAIL("Unexpected exception thrown when getXvt looks for an"
" invalid SatID");
}
// Verify that an InvalidRequest exception is thrown when SatID is not in the data
try
{
store.getXvt(sid32,bTime);
TUFAIL("No exception thrown when getXvt looks for an invalid"
" SatID");
}
catch (InvalidRequest& e)
{
TUPASS("Expected exception thrown when getXvt looks for an invalid"
" SatID");
}
catch (...)
{
TUFAIL("Unexpected exception thrown when getXvt looks for an"
" invalid SatID");
}
// Verify that no exception is thrown for SatID in the data set
try
{
store.getXvt(sid1,eTime);
TUPASS("No exception thrown when getXvt looks for a valid SatID");
}
catch (...)
{
TUFAIL("Exception thrown when getXvt looks for a valid SatID");
}
outputStream1 << store.getXvt(sid1,eTime);
outputStream15 << store.getXvt(sid15,eTime);
outputStream31 << store.getXvt(sid31,eTime);
}
catch (Exception& e)
{
cout << e;
}
//--------------------------------------------------------------------
// Were the values set to expectation using the explicit constructor?
//--------------------------------------------------------------------
TUASSERTE(std::string, inputComparisonOutput1, outputStream1.str());
TUASSERTE(std::string, inputComparisonOutput15, outputStream15.str());
TUASSERTE(std::string, inputComparisonOutput31, outputStream31.str());
}
catch (...)
{
TUFAIL("Unexpected exception");
}
return testFramework.countFails();
}
int main(int argc, char *argv[])
{
if (argc<2) {
cout << "Usage: petest <SP3-format files ...>\n";
return -1;
}
try
{
bool firstEpochFound=true;
DayTime firstTime;
DayTime lastTime;
SatID firstSat;
int i,ip,it,nf=0,np=0,nt=0;
SP3EphemerisStore EphList;
for(i=1; i<argc; i++) {
SP3Header header;
SP3Data data;
// you can't open, close, and reopen a file w/o abort on second open...
SP3Stream pefile;
pefile.exceptions(ifstream::failbit);
cout << "Reading SP3 file " << argv[i] << "." << endl;
pefile.open(argv[i],ios::in);
pefile >> header;
data.version = header.version;
//cout << "Dump header:\n";
//header.dump(cout);
//cout << endl;
ip = it = 0;
DayTime t(DayTime::BEGINNING_OF_TIME);
while(pefile >> data) {
if (firstEpochFound)
{
firstSat = data.sat;
firstTime = data.time;
lastTime = firstTime;
firstEpochFound=false;
}
if (data.time > lastTime) lastTime = data.time;
if(data.time > t) {
//cout << "Epoch " << data.time << endl;
t = data.time;
it++; nt++;
}
//data.dump(cout);
ip++; np++;
}
cout << "\nDone with file " << argv[i] << ": read "
<< ip << " P/V records and " << it << " epochs." << endl;
pefile.close();
nf++;
// add to store
EphList.loadFile(string(argv[i]));
}
cout << "\nDone with " << nf << " files: read "
<< np << " P/V records and " << nt << " epochs." << endl;
//EphList.dump(2);
unsigned long ref;
// choose a time tag within the data....
DayTime tt = firstTime + (lastTime-firstTime)/2.;
SatID tsat = firstSat;
Xvt PVT;
for(i=0; i<300; i++) {
tt += 30.0;
PVT = EphList.getXvt(tsat,tt);
if (true)
cout << "LI " << tt << " P " << fixed
<< setw(13) << setprecision(6) << PVT.x[0] << " "
<< setw(13) << setprecision(6) << PVT.x[1] << " "
<< setw(13) << setprecision(6) << PVT.x[2] << " "
<< setw(13) << setprecision(6) << PVT.dtime
<< " V "
<< setw(13) << setprecision(6) << PVT.v[0] << " "
<< setw(13) << setprecision(6) << PVT.v[1] << " "
<< setw(13) << setprecision(6) << PVT.v[2] << " "
<< setw(13) << setprecision(6) << PVT.ddtime
<< endl;
}
}
catch (Exception& e)
{
cout << e;
exit(-1);
}
catch (...)
{
cout << "Caught an unknown exception" << endl;
exit(-1);
}
return 0;
}
//------------------------------------------------------------------------------------
// Configure(1)
// open and read navigation files
// open and read headers of all observation files
int Initialize(void) throw(Exception)
{
try {
size_t i;
// global pEph will point to one of these
static GPSEphemerisStore BCEphList;
static SP3EphemerisStore SP3EphList;
if(CI.Verbose) oflog << "BEGIN Configure(1)"
<< " at total time " << fixed << setprecision(3)
<< double(clock()-totaltime)/double(CLOCKS_PER_SEC) << " seconds."
<< endl;
if(CI.Frequency == 1) wave = wl1;
if(CI.Frequency == 2) wave = wl2;
// NB wave should never be used for L3 -- see warning in CommandInput.cpp
else if(CI.Frequency == 3) wave = wl1;
// open nav files, if any, and read EphemerisStore into EphLists
if(CI.NavFileNames.size() > 0) {
if(!CI.NavPath.empty())
for(i=0; i<CI.NavFileNames.size(); i++)
CI.NavFileNames[i] = CI.NavPath + "/" + CI.NavFileNames[i];
// fill ephemeris store -- this routine in RinexUtilities.cpp
FillEphemerisStore(CI.NavFileNames, SP3EphList, BCEphList);
}
// read all headers and store information in Station object
ReadAllObsHeaders();
// use the information gathered in ReadAllObsHeaders to determine DT
// if the user did not specify --DT, set it
// else if the --DT the user chose is too small, reset it
// else leave --DT alone
double DT=-1.0;
for(i=0; i<ObsFileList.size(); i++) {
if(ObsFileList[i].dt > DT)
DT = ObsFileList[i].dt;
if(ObsFileList[i].firstTime > CI.BegTime)
CI.BegTime = ObsFileList[i].firstTime;
}
if(CI.DataInterval == -1) {
CI.DataInterval = DT;
if(CI.Verbose) oflog << "DDBase has determined the data interval (--DT) to be "
<< CI.DataInterval << " seconds." << endl;
}
else if(CI.DataInterval < DT) {
CI.DataInterval = DT;
oflog << "Warning - DDBase has changed the data interval (--DT) to "
<< CI.DataInterval << " seconds." << endl;
}
// dump SP3 store to log
if(SP3EphList.size()) {
if(CI.Verbose) SP3EphList.dump(oflog,0);
}
else if(CI.Verbose) oflog << "SP3 Ephemeris store is empty" << endl;
// dump BCE store to log
if(BCEphList.size()) {
// this causes the CorrectedEphemerisRange routines to pick the
// closest TOE in either future or past of the epoch, rather
// than the closest in the past -- see GPSEphemerisStore.hpp
BCEphList.SearchNear();
if(CI.Debug) BCEphList.dump(oflog,1);
else if(CI.Verbose) BCEphList.dump(oflog,0);
}
else if(CI.Verbose) oflog << "BC Ephemeris store is empty" << endl;
// assign pointer
// NB SP3 takes precedence
if(SP3EphList.size()) pEph = &SP3EphList;
else if(BCEphList.size()) pEph = &BCEphList;
else {
cerr << "Initialize ERROR: no ephemeris. Abort." << endl;
oflog << "Initialize ERROR: no ephemeris. Abort." << endl;
return 1;
}
// open all EOP files and fill the EOPstore
if(!CI.EOPPath.empty())
for(i=0; i<CI.EOPFileNames.size(); i++)
CI.EOPFileNames[i] = CI.EOPPath + "/" + CI.EOPFileNames[i];
if(CI.EOPFileNames.size() > 0) {
for(i=0; i<CI.EOPFileNames.size(); i++)
EOPList.addFile(CI.EOPFileNames[i]);
}
else {
try {
EOPList.addIERSFile("finals.daily");
}
catch(FileMissingException& fme) {
string msg("DDBase was unable to find any Earth Orientation parameters:\n"
" either add option --EOPFile <file> or put file 'finals.daily' in the"
" current directory.\n (http://maia.usno.navy.mil/ser7/finals.daily)\n");
cerr << msg;
oflog << msg;
GPSTK_RETHROW(fme);
}
}
if(EOPList.size()) {
if(CI.Debug) EOPList.dump(1,oflog);
else if(CI.Verbose) EOPList.dump(0,oflog);
}
else oflog << "Warning - no Earth Orientation Parameters were input\n";
// add path to output files
if(!CI.OutPath.empty()) {
if(!CI.OutputClkFile.empty())
CI.OutputClkFile = CI.OutPath + "/" + CI.OutputClkFile;
if(!CI.OutputDDDFile.empty())
CI.OutputDDDFile = CI.OutPath + "/" + CI.OutputDDDFile;
if(!CI.OutputTDDFile.empty())
CI.OutputTDDFile = CI.OutPath + "/" + CI.OutputTDDFile;
if(!CI.OutputRawFile.empty())
CI.OutputRawFile = CI.OutPath + "/" + CI.OutputRawFile;
if(!CI.OutputRawDDFile.empty())
CI.OutputRawDDFile = CI.OutPath + "/" + CI.OutputRawDDFile;
if(!CI.OutputPRSFile.empty())
CI.OutputPRSFile = CI.OutPath + "/" + CI.OutputPRSFile;
if(!CI.OutputDDRFile.empty())
CI.OutputDDRFile = CI.OutPath + "/" + CI.OutputDDRFile;
}
// assign trop model for RAIM (model for DD est assigned in Configure(2))
// NB using another, like Saastamoinen, here, is problematic because it
// requires height, latitude and DOY input, [ this because RAIM calls
// CI.pTropModel->correction(elevation) ], and that info is different for
// different sites and not all available.
CI.pTropModel = &TropModelSimple;
// TD per site
CI.pTropModel->setWeather(CI.DefaultTemp,CI.DefaultPress,CI.DefaultRHumid);
// Define first and last epochs
FirstEpoch = CommonTime::BEGINNING_OF_TIME;
LastEpoch = CommonTime::END_OF_TIME;
return 0;
}
catch(Exception& e) { GPSTK_RETHROW(e); }
catch(std::exception& e) { Exception E("std except: "+string(e.what())); GPSTK_THROW(E); }
catch(...) { Exception e("Unknown exception"); GPSTK_THROW(e); }
}