本文整理汇总了C++中DayTime::DOYsecond方法的典型用法代码示例。如果您正苦于以下问题：C++ DayTime::DOYsecond方法的具体用法？C++ DayTime::DOYsecond怎么用？C++ DayTime::DOYsecond使用的例子？那么, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类DayTime的用法示例。
在下文中一共展示了DayTime::DOYsecond方法的2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: setprecision
// Method to print solution values
void example9::printSolution( ofstream& outfile,
const SolverLMS& solver,
const DayTime& time,
const ComputeDOP& cDOP,
bool useNEU,
int numSats,
double dryTropo,
int precision )
{
// Prepare for printing
outfile << fixed << setprecision( precision );
// Print results
outfile << time.year() << " "; // Year - #1
outfile << time.DOY() << " "; // DayOfYear - #2
outfile << time.DOYsecond() << " "; // SecondsOfDay - #3
if( useNEU )
{
outfile << solver.getSolution(TypeID::dLat) << " "; // dLat - #4
outfile << solver.getSolution(TypeID::dLon) << " "; // dLon - #5
outfile << solver.getSolution(TypeID::dH) << " "; // dH - #6
// We add 0.1 meters to 'wetMap' because 'NeillTropModel' sets a
// nominal value of 0.1 m. Also to get the total we have to add the
// dry tropospheric delay value
// ztd - #7
outfile << solver.getSolution(TypeID::wetMap) + 0.1 + dryTropo << " ";
outfile << solver.getVariance(TypeID::dLat) << " "; // Cov dLat - #8
outfile << solver.getVariance(TypeID::dLon) << " "; // Cov dLon - #9
outfile << solver.getVariance(TypeID::dH) << " "; // Cov dH - #10
outfile << solver.getVariance(TypeID::wetMap) << " "; // Cov ztd - #11
}
else
{
outfile << solver.getSolution(TypeID::dx) << " "; // dx - #4
outfile << solver.getSolution(TypeID::dy) << " "; // dy - #5
outfile << solver.getSolution(TypeID::dz) << " "; // dz - #6
// We add 0.1 meters to 'wetMap' because 'NeillTropModel' sets a
// nominal value of 0.1 m. Also to get the total we have to add the
// dry tropospheric delay value
// ztd - #7
outfile << solver.getSolution(TypeID::wetMap) + 0.1 + dryTropo << " ";
outfile << solver.getVariance(TypeID::dx) << " "; // Cov dx - #8
outfile << solver.getVariance(TypeID::dy) << " "; // Cov dy - #9
outfile << solver.getVariance(TypeID::dz) << " "; // Cov dz - #10
outfile << solver.getVariance(TypeID::wetMap) << " "; // Cov ztd - #11
}
outfile << numSats << " "; // Number of satellites - #12
outfile << cDOP.getGDOP() << " "; // GDOP - #13
outfile << cDOP.getPDOP() << " "; // PDOP - #14
outfile << cDOP.getTDOP() << " "; // TDOP - #15
outfile << cDOP.getHDOP() << " "; // HDOP - #16
outfile << cDOP.getVDOP() << " "; // VDOP - #17
// Add end-of-line
outfile << endl;
return;
} // End of method 'example9::printSolution()'示例2: getCorrection
double IonoModel::getCorrection(const DayTime& time,
const Geodetic& rxgeo,
double svel,
double svaz,
Frequency freq) const
throw(IonoModel::InvalidIonoModel)
{
if (!valid)
{
InvalidIonoModel e("Alpha and beta parameters invalid.");
GPSTK_THROW(e);
}
// all angle units are in semi-circles (radians / TWO_PI)
// Note: math functions (cos, sin, etc.) require arguments in
// radians so all semi-circles must be multiplied by TWO_PI
double azRad = svaz * DEG_TO_RAD;
double svE = svel / 180.0;
double phi_u = rxgeo.getLatitude() / 180.0;
double lambda_u = rxgeo.getLongitude() / 180.0;
double psi = (0.0137 / (svE + 0.11)) - 0.022;
double phi_i = phi_u + psi * cos(azRad);
if (phi_i > 0.416)
phi_i = 0.416;
if (phi_i < -0.416)
phi_i = -0.416;
double lambda_i = lambda_u + psi * sin(azRad) / cos(phi_i*PI);
double phi_m = phi_i + 0.064 * cos((lambda_i - 1.617)*PI);
double iAMP = 0.0;
double iPER = 0.0;
iAMP = alpha[0]+phi_m*(alpha[1]+phi_m*(alpha[2]+phi_m*alpha[3]));
iPER = beta[0]+phi_m*( beta[1]+phi_m*( beta[2]+phi_m* beta[3]));
if (iAMP < 0.0)
iAMP = 0.0;
if (iPER < 72000.0)
iPER = 72000.0;
double t = 43200.0 * lambda_i + time.DOYsecond();
if (t >= 86400.0)
t -= 86400.0;
if (t < 0)
t += 86400.0;
double x = TWO_PI * (t - 50400.0) / iPER; // x is in radians
double iF = 1.0 + 16.0 * (0.53 - svE)*(0.53 - svE)*(0.53 - svE);
double t_iono = 0.0;
if (fabs(x) < 1.57)
t_iono = iF * (5.0e-9 + iAMP * (1 + x*x * (-0.5 + x*x/24.0)));
else
t_iono = iF * 5.0e-9;
if (freq == L2)
{
// see ICD-GPS-200 20.3.3.3.3.2
t_iono *= GAMMA_GPS; // GAMMA_GPS = (fL1 / fL2)^2
}
double correction = t_iono * C_GPS_M;
return correction;
}