本文整理汇总了C++中GPSTK_THROW函数的典型用法代码示例。如果您正苦于以下问题：C++ GPSTK_THROW函数的具体用法？C++ GPSTK_THROW怎么用？C++ GPSTK_THROW使用的例子？那么恭喜您, 这里精选的函数代码示例或许可以为您提供帮助。
在下文中一共展示了GPSTK_THROW函数的15个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C++代码示例。
示例1: throw
/* Computes the quantile function ( cdf^-1() )
*
* @param p Probability value
*
* \ warning Value "p" must be in the range (0, 1)
*/
double GaussianDistribution::invcdf(double p)
throw(InvalidParameter)
{
double inf( 9.0e+99 );
// Check limits
if( ( p < 0.0 ) ||
( p > 1.0 ) )
{
InvalidParameter e( "Invalid input value for 'p'." );
GPSTK_THROW(e);
}
if( p == 0.0 ) return -inf;
if( p == 1.0 ) return inf;
// Compute invcdf
return ( mean
+ 1.4142135623730951 * sigma * gpstk::inverf( 2.0 * p - 1.0 ) );
} // End of method 'GaussianDistribution::invcdf()'示例2: throw
/* Returns a reference to a gnnsRinex object after solving
* the previously defined equation system.
*
* @param gData Data object holding the data.
*/
gnssRinex& SolverPPPFB::Process(gnssRinex& gData)
throw(ProcessingException)
{
try
{
SolverPPP::Process(gData);
// Before returning, store the results for a future iteration
if(firstIteration)
{
// Create a new gnssRinex structure with just the data we need
gnssRinex gBak(gData.extractTypeID(keepTypeSet));
// Store observation data
ObsData.push_back(gBak);
// Update the number of processed measurements
processedMeasurements += gData.numSats();
}
return gData;
}
catch(Exception& u)
{
// Throw an exception if something unexpected happens
ProcessingException e( getClassName() + ":"
+ u.what() );
GPSTK_THROW(e);
}
} // End of method 'SolverPPPFB::Process()'示例3: throw
FileSpec::FileSpecType FileSpec::convertFileSpecType(const string& fst)
throw(FileSpecException)
{
if (fst == string("n")) return station;
else if (fst == string("r")) return receiver;
else if (fst == string("p")) return prn;
else if (fst == string("t")) return selected;
else if (fst == string("I")) return sequence;
else if (fst == string("v")) return version;
else if (fst == string("k")) return clock;
else if (fst == string("x")) return text;
else if (fst == string("Y") ||
fst == string("y")) return year;
else if (fst == string("m")) return month;
else if (fst == string("d")) return dayofmonth;
else if (fst == string("H")) return hour;
else if (fst == string("M")) return minute;
else if (fst == string("S")) return second;
else if (fst == string("f")) return fsecond;
else if (fst == string("G")) return gpsweek;
else if (fst == string("F")) return fullgpsweek;
else if (fst == string("g")) return gpssecond;
else if (fst == string("Q")) return mjd;
else if (fst == string("w")) return dayofweek;
else if (fst == string("j")) return day;
else if (fst == string("s")) return doysecond;
else if (fst == string("Z")) return zcount;
else if (fst == string("z")) return zcountfloor;
else if (fst == string("U")) return unixsec;
else if (fst == string("u")) return unixusec;
else if (fst == string("C") ||
fst == string("c")) return fullzcount;
else
{
FileSpecException fse("Unknown FileSpecType: " + fst);
GPSTK_THROW(fse);
}
}示例4: throw
/* Set the number of degrees of freedom.
*
* @param n Degrees of freedom
*
* \warning "n" must be > 0.0, otherwise n = |n|.
*/
StudentDistribution& StudentDistribution::setNDF(int n)
throw(InvalidParameter)
{
if( n == 0 )
{
InvalidParameter e( "Invalid value for NDF." );
GPSTK_THROW(e);
}
if( n < 0 )
{
ndf = -n;
}
else
{
ndf = n;
}
return (*this);
} // End of method 'StudentDistribution::setNDF()'示例5: throw
void RinexNavData::getBroadcastOrbit6(const string& currentLine)
throw(StringException, FFStreamError)
{
try
{
double SV_health;
accuracy = gpstk::StringUtils::for2doub(currentLine.substr(3,19));
SV_health = gpstk::StringUtils::for2doub(currentLine.substr(22,19));
Tgd = gpstk::StringUtils::for2doub(currentLine.substr(41,19));
IODC = gpstk::StringUtils::for2doub(currentLine.substr(60,19));
health = (short) SV_health;
}
catch (std::exception &e)
{
FFStreamError err("std::exception: " +
string(e.what()));
GPSTK_THROW(err);
}
}示例6: fromString
void fromString(const std::string str)
{
std::string STR(gpstk::StringUtils::upperCase(str));
if(STR == std::string("GPUT"))
{ type = GPUT; frTS = TimeSystem::GPS; toTS = TimeSystem::UTC; }
else if(STR == std::string("GAUT"))
{ type = GAUT; frTS = TimeSystem::GAL; toTS = TimeSystem::UTC; }
else if(STR == std::string("SBUT"))
// TD ??
{ type = SBUT; frTS = TimeSystem::GPS; toTS = TimeSystem::UTC; }
else if(STR == std::string("GLUT"))
{ type = GLUT; frTS = TimeSystem::GLO; toTS = TimeSystem::UTC; }
else if(STR == std::string("GPGA"))
{ type = GPGA; frTS = TimeSystem::GPS; toTS = TimeSystem::GAL; }
else if(STR == std::string("GLGP"))
{ type = GLGP; frTS = TimeSystem::GLO; toTS = TimeSystem::GPS; }
else if(STR == std::string("QZGP"))
{ type = QZGP; frTS = TimeSystem::QZS; toTS = TimeSystem::GPS; }
else if(STR == std::string("QZUT"))
{ type = QZUT; frTS = TimeSystem::QZS; toTS = TimeSystem::UTC; }
else if(STR == std::string("BDUT"))
{ type = BDUT; frTS = TimeSystem::BDT; toTS = TimeSystem::UTC; }
else if(STR == std::string("BDGP"))
{ type = BDGP; frTS = TimeSystem::BDT; toTS = TimeSystem::GPS; }
else {
Exception e("Unknown TimeSystemCorrection type: " + str);
GPSTK_THROW(e);
}
}示例7: MEstimate
T MEstimate(const T *xd, int nd, const T& M, const T& MAD, T *w=NULL)
throw(Exception)
{
try {
T tv, m, mold, sum, sumw, *wt, weight, *t;
T tol=0.000001;
int i, n, N=10; // N is the max number of iterations
if(!xd || nd < 2) {
Exception e("Invalid input");
GPSTK_THROW(e);
}
tv = T(RobustTuningT)*MAD;
n = 0;
m = M;
do {
mold = m;
n++;
sum = sumw = T();
for(i=0; i<nd; i++) {
if(w) wt=&w[i];
else wt=&weight;
*wt = T(1);
if(xd[i]<m-tv) *wt = -tv/(xd[i]-m);
else if(xd[i]>m+tv) *wt = tv/(xd[i]-m);
sumw += (*wt);
sum += (*wt)*xd[i];
}
m = sum / sumw;
} while(T(ABSOLUTE((m-mold)/m)) > tol && n < N);
return m;
}
catch(Exception& e) { GPSTK_RETHROW(e); }
} // end MEstimate示例8: throw
// Compute the pressure and temperature at height, and the undulation,
// for the given position and time.
void GlobalTropModel::getGPT(double& P, double& T, double& U)
throw(InvalidTropModel)
{
try { testValidity(); }
catch(InvalidTropModel& e) { GPSTK_RETHROW(e); }
int i;
// undulation and orthometric height
U = 0.0;
for(i=0; i<55; i++) U += (Ageoid[i]*aP[i] + Bgeoid[i]*bP[i]);
double orthoht(height - U);
if(orthoht > 44247.) GPSTK_THROW(InvalidTropModel(
"Invalid Global trop model: Rx Height is too large"));
// press at geoid
double am(0.0),aa(0.0),v0;
for(i=0; i<55; i++) {
am += (APressMean[i]*aP[i] + BPressMean[i]*bP[i]);
aa += (APressAmp[i]*aP[i] + BPressAmp[i]*bP[i]);
}
v0 = am + aa * ::cos(dayfactor);
// pressure at height
// NB this implies any orthoht > 1/2.26e-5 == 44247.78m is invalid!
P = v0 * ::pow(1.0-2.26e-5*orthoht,5.225);
// temper on geoid
am = aa = 0.0;
for(i=0; i<55; i++) {
am += (ATempMean[i]*aP[i] + BTempMean[i]*bP[i]);
aa += (ATempAmp[i]*aP[i] + BTempAmp[i]*bP[i]);
}
v0 = am + aa * ::cos(dayfactor);
// temp at height
T = v0 - 6.5e-3 * orthoht;
}示例9: cfIBeta
// Compute continued fractions portion of incomplete beta function I_x(a,b)
/// Routine used internally for Incomplete beta function I_x(a,b)
double cfIBeta(const double& x, const double& a, const double& b) throw(Exception)
{
static const int imax(100);
static const double eps(10*std::numeric_limits<double>().epsilon());
static const double fpmin(10*std::numeric_limits<double>().min());
const double qab(a+b);
const double qap(a+1.0);
const double qam(a-1.0);
double c(1),d(1-qab*x/qap),aa,del;
if(::fabs(d) < fpmin) d=fpmin;
d = 1.0/d;
double h(d);
int i,i2;
for(i=1; i<=imax; i++) {
i2 = 2*i;
aa = i*(b-i)*x/((qam+i2)*(a+i2));
d = 1.0 + aa*d;
if(::fabs(d) < fpmin) d=fpmin;
c = 1.0 + aa/c;
if(::fabs(c) < fpmin) c=fpmin;
d = 1.0/d;
h *= d*c;
aa = -(a+i)*(qab+i)*x/((a+i2)*(qap+i2));
d = 1.0 + aa*d;
if(::fabs(d) < fpmin) d=fpmin;
c = 1.0 + aa/c;
if(::fabs(c) < fpmin) c=fpmin;
d = 1.0/d;
del = d*c;
h *= del;
if(::fabs(del-1.0) < eps) break;
}
if(i > imax) {
Exception e("Overflow in cfIBeta(); a or b too big");
GPSTK_THROW(e);
}
return h;
}示例10: throw
/* Dumps data from a satTypeValueMap object.
*
* @param gData Data object holding the data.
*/
satTypeValueMap& Dumper::Process( satTypeValueMap& gData )
throw(ProcessingException)
{
try
{
// Iterate through all items in the GNSS Data Structure
for( satTypeValueMap::const_iterator it = gData.begin();
it!= gData.end();
it++ )
{
// First, print satellite (system and PRN)
*outStr << (*it).first << " ";
// Now, print TypeIDs
printTypeID( (*it).second );
// Print end of line
*outStr << std::endl;
} // End of 'for( satTypeValueMap::const_iterator it = ...'
return gData;
}
catch(Exception& u)
{
// Throw an exception if something unexpected happens
ProcessingException e( getClassName() + ":"
+ u.what() );
GPSTK_THROW(e);
}
} // End of method 'Dumper::Process()'示例11: throw
/* Returns a gnnsSatTypeValue object, adding the new data generated
* when calling this object.
*
* @param gData Data object holding the data.
*/
gnssSatTypeValue& PhaseCodeAlignment::Process(gnssSatTypeValue& gData)
throw(ProcessingException)
{
try
{
Process(gData.header.epoch, gData.body);
return gData;
}
catch(Exception& u)
{
// Throw an exception if something unexpected happens
ProcessingException e( getClassName() + ":"
+ u.what() );
GPSTK_THROW(e);
}
} // End of 'PhaseCodeAlignment::Process()'示例12: throw
/* Returns a gnnsRinex object, adding the new data generated when
* calling this object.
*
* @param gData Data object holding the data.
*/
gnssRinex& LICSDetector::Process(gnssRinex& gData)
throw(ProcessingException)
{
try
{
Process(gData.header.epoch, gData.body, gData.header.epochFlag);
return gData;
}
catch(Exception& u)
{
// Throw an exception if something unexpected happens
ProcessingException e( getClassName() + ":"
+ u.what() );
GPSTK_THROW(e);
}
} // End of method 'LICSDetector::Process()'示例13: throw
/* Returns a gnnsRinex object, adding the new data generated
* when calling this object.
*
* @param gData Data object holding the data.
*/
gnssRinex& ComputeSimpleWeights::Process(gnssRinex& gData)
throw(ProcessingException)
{
try
{
Process(gData.header.epoch, gData.body);
return gData;
}
catch(Exception& u)
{
// Throw an exception if something unexpected happens
ProcessingException e( getClassName() + ":"
+ u.what() );
GPSTK_THROW(e);
}
} // End of method 'ComputeSimpleWeightsWeights::Process()'示例14: throw
/* Returns a gnnsRinex object, adding the new data generated when
* calling this object.
*
* @param gData Data object holding the data.
*/
gnssRinex& EclipsedSatFilter::Process(gnssRinex& gData)
throw(ProcessingException)
{
try
{
Process(gData.header.epoch, gData.body);
return gData;
}
catch(Exception& u)
{
// Throw an exception if something unexpected happens
ProcessingException e( getClassName() + ":"
+ u.what() );
GPSTK_THROW(e);
}
} // End of 'EclipsedSatFilter::Process()'示例15: GPSTK_THROW
// Dump the overhead information as a string containing a single line.
// @throw Invalid Request if the required data has not been stored.
string GPSEphemeris::asString(void) const
{
if(!dataLoadedFlag)
GPSTK_THROW(InvalidRequest("Data not loaded"));
try {
ostringstream os;
CivilTime ct;
os << "EPH G" << setfill('0') << setw(2) << satID.id << setfill(' ');
ct = CivilTime(beginValid);
os << printTime(ct," | %4Y %3j %02H:%02M:%02S |");
ct = CivilTime(ctToe);
os << printTime(ct," %3j %02H:%02M:%02S |");
ct = CivilTime(ctToc);
os << printTime(ct," %3j %02H:%02M:%02S |");
ct = CivilTime(endValid);
os << printTime(ct," %3j %02H:%02M:%02S |");
ct = CivilTime(transmitTime);
os << printTime(ct," %3j %02H:%02M:%02S | ");
os << setw(3) << IODE << " | " << setw(3) << IODC << " | " << health;
return os.str();
}
catch(Exception& e) { GPSTK_RETHROW(e);
}
}