本文整理汇总了C++中SkyPoint::vGeocentric方法的典型用法代码示例。如果您正苦于以下问题：C++ SkyPoint::vGeocentric方法的具体用法？C++ SkyPoint::vGeocentric怎么用？C++ SkyPoint::vGeocentric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SkyPoint的用法示例。
在下文中一共展示了SkyPoint::vGeocentric方法的1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: processLines
//.........这里部分代码省略.........
if ( AllRadioBatch->isChecked() )
ostream << decB.toDMSString() << space;
else
if(DecCheckBatch->isChecked() )
ostream << decB.toDMSString() << space;
// Read Epoch and write in ostream if corresponds
if(EpochCheckBatch->isChecked() ) {
epoch0B = fields[i];
i++;
} else
epoch0B = EpochBoxBatch->text();
if ( AllRadioBatch->isChecked() )
ostream << epoch0B << space;
else
if(EpochCheckBatch->isChecked() )
ostream << epoch0B << space;
// Read vlsr and write in ostream if corresponds
if(InputVelocityCheckBatch->isChecked() ) {
vlsrB = fields[i].toDouble();
i++;
} else
vlsrB = InputVelocityComboBatch->currentText().toDouble();
if ( AllRadioBatch->isChecked() )
ostream << vlsrB << space;
else
if(InputVelocityCheckBatch->isChecked() )
ostream << vlsrB << space;
// Read Longitude and write in ostream if corresponds
if (LongCheckBatch->isChecked() ) {
longB = dms::fromString( fields[i],true);
i++;
} else
longB = LongitudeBoxBatch->createDms(true);
if ( AllRadioBatch->isChecked() )
ostream << longB.toDMSString() << space;
else
if (LongCheckBatch->isChecked() )
ostream << longB.toDMSString() << space;
// Read Latitude
if (LatCheckBatch->isChecked() ) {
latB = dms::fromString( fields[i], true);
i++;
} else
latB = LatitudeBoxBatch->createDms(true);
if ( AllRadioBatch->isChecked() )
ostream << latB.toDMSString() << space;
else
if (LatCheckBatch->isChecked() )
ostream << latB.toDMSString() << space;
// Read height and write in ostream if corresponds
if(ElevationCheckBatch->isChecked() ) {
heightB = fields[i].toDouble();
i++;
} else
heightB = ElevationBoxBatch->text().toDouble();
if ( AllRadioBatch->isChecked() )
ostream << heightB << space;
else
if(ElevationCheckBatch->isChecked() )
ostream << heightB << space;
// We make the first calculations
spB = SkyPoint (raB, decB);
dt0B.setFromEpoch(epoch0B);
vhB = spB.vHeliocentric(vlsrB, dt0B.djd());
jd0 = KStarsDateTime(dtB,utB).djd();
vgB = spB.vGeocentric(vlsrB, jd0);
geoPlace->setLong( longB );
geoPlace->setLat( latB );
geoPlace->setHeight( heightB );
dms gsidt = KStarsDateTime(dtB,utB).gst();
geoPlace->TopocentricVelocity(vtopo, gsidt);
spB.ra().SinCos(sra, cra);
spB.dec().SinCos(sdc, cdc);
vtB = vgB - (vtopo[0]*cdc*cra + vtopo[1]*cdc*sra + vtopo[2]*sdc);
ostream << vhB << space << vgB << space << vtB << endl;
}
fOut.close();
}