本文整理汇总了C++中EngEphemeris::getHealth方法的典型用法代码示例。如果您正苦于以下问题：C++ EngEphemeris::getHealth方法的具体用法？C++ EngEphemeris::getHealth怎么用？C++ EngEphemeris::getHealth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EngEphemeris的用法示例。
在下文中一共展示了EngEphemeris::getHealth方法的3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: ConvertEEtoAO
AlmOrbit ConvertEEtoAO(EngEphemeris& ee)
{
AlmOrbit ao(
ee.getPRNID() , ee.getEcc() , ee.getI0()-0.3*PI, ee.getOmegaDot() ,
ee.getAhalf() , ee.getOmega0(), ee.getW() , ee.getM0() ,
ee.getAf0() , ee.getAf1() , long(ee.getToe()), long(ee.getHOWTime(1)),
ee.getFullWeek(), ee.getHealth()
);
return ao;
}示例2: RinexSatID
// Deprecated; used GPSEphemeris.
// This routine uses EngEphemeris, so is for GPS data only.
// The comments about GPS v. Galileo next to each elements are just notes
// from sorting out the ICDs in the RINEX 3 documentation. Please leave
// them there until we add a routine for handling GalRecord or similar.
Rinex3NavData::Rinex3NavData(const EngEphemeris& ee) // GPS only
{
// epoch info
satSys = ee.getSatSys();
PRNID = ee.getPRNID();
sat = RinexSatID(PRNID,SatID::systemGPS);
time = ee.getEpochTime();
Toc = ee.getToc();
HOWtime = long(ee.getHOWTime(1));
weeknum = ee.getFullWeek();
accuracy = ee.getAccuracy();
health = ee.getHealth();
// GPS or Galileo data
af0 = ee.getAf0(); // GPS and Galileo only
af1 = ee.getAf1(); // GPS and Galileo only
af2 = ee.getAf2(); // GPS and Galileo only
Crs = ee.getCrs(); // GPS and Galileo only
dn = ee.getDn(); // GPS and Galileo only
M0 = ee.getM0(); // GPS and Galileo only
Cuc = ee.getCuc(); // GPS and Galileo only
ecc = ee.getEcc(); // GPS and Galileo only
Cus = ee.getCus(); // GPS and Galileo only
Ahalf = ee.getAhalf(); // GPS and Galileo only
Toe = ee.getToe(); // GPS and Galileo only
Cic = ee.getCic(); // GPS and Galileo only
OMEGA0 = ee.getOmega0(); // GPS and Galileo only
Cis = ee.getCis(); // GPS and Galileo only
i0 = ee.getI0(); // GPS and Galileo only
Crc = ee.getCrc(); // GPS and Galileo only
w = ee.getW(); // GPS and Galileo only
OMEGAdot = ee.getOmegaDot(); // GPS and Galileo only
idot = ee.getIDot(); // GPS and Galileo only
// GPS-only data
IODE = ee.getIODE(); // GPS only
codeflgs = ee.getCodeFlags(); // GPS only
L2Pdata = ee.getL2Pdata(); // GPS only
Tgd = ee.getTgd(); // GPS only
IODC = ee.getIODC(); // GPS only
fitint = ee.getFitInterval(); // GPS only
} // End of 'Rinex3NavData::Rinex3NavData(const EngEphemeris& ee)'示例3: process
//.........这里部分代码省略.........
mismatch = true;
fp << "ERROR: IODCs do not match.";
}
if (ee.getIODE()!=eeMin.getIODE())
{
mismatch = true;
fp << "ERROR: IODCs do not match.";
}
if (ee.getFitInterval() != eeMin.getFitInterval() )
{
mismatch = true;
fp << "ERROR: fit intervals do not match.";
}
if (ee.getCodeFlags()!=eeMin.getCodeFlags() )
{
mismatch = true;
fp << "ERROR: code flags do not match.";
}
if (ee.getL2Pdata()!=eeMin.getL2Pdata() )
{
mismatch = true;
fp << "ERROR: L2P data flags do not match.";
}
if (ee.getAccuracy()!=eeMin.getAccuracy() )
{
mismatch = true;
fp << "ERROR: accuracy values do not match.";
}
if (ee.getAccFlag()!=eeMin.getAccFlag() )
{
mismatch = true;
fp << "ERROR: accuracy flags do not match.";
}
if (ee.getHealth()!=eeMin.getHealth() )
{
mismatch = true;
fp << "ERROR: health values do not match.";
}
if (ee.getFitInt()!=eeMin.getFitInt() )
{
mismatch = true;
fp << "ERROR: Fit interval values do not match.";
}
if (mismatch)
{
fp << " PRNID: " << PRNID << ", IODC: 0x " << hex << ee.getIODC() << dec << endl;
numMismatches++;
}
itr++;
count++;
}
cout << "Number of Block 109 records read: " << count << endl;
if (numMismatches!=0)
{
printf("Errors detected. Some ephemerides did not match in both forms.\n");
printf("Number of mismatches: %d\n",numMismatches);
}
fp << "Number of mismatches detected: " << numMismatches << endl;
if (debugLevel) cout << "done." << endl;
// Generate test positions for PRN 1 and PRN 31 at
// earliest epoch, latest epoch, and middle of the time span.
try