本文整理汇总了C++中EngEphemeris::getOrbit方法的典型用法代码示例。如果您正苦于以下问题：C++ EngEphemeris::getOrbit方法的具体用法？C++ EngEphemeris::getOrbit怎么用？C++ EngEphemeris::getOrbit使用的例子？那么恭喜您, 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::getOrbit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: firstTest
//.........这里部分代码省略.........
ofstream outf("Logs/CNAVEphemeris_Output", ios::out);
outf.precision(11);
// First test case. Create an CE object with data available from RINEX file.
outf << endl << "Test Case 1: Creating CE object with data from RINEX file." << endl;
outf << "Time = " << g << endl;
CNAVEphemeris ce1;
ce1.loadData(SysID, obsID, PRNID, AlertMsg10, TOWMsg10_1, AlertMsg11,
TOWMsg11_1, rTOWWeek, Top, URAoe, L1Health, L2Health,
L5Health, rToe, raccuracy, rCuc, rCus, rCrc, rCrs, rCic,
rCis, rM0, rdn, rdnDot, recc, deltaA, rAdot, rOMEGA0,
ri0, rw, deltaOMEGAdot1, ridot );
Xv xv1 = ce1.svXv( dt );
outf << "Position ce1: " << xv1.x << endl;
outf << "Velocity ce1: " << xv1.v << endl;
outf << "RelCorr ce1: " << ce1.svRelativity(dt) << endl;
outf << "Time of Prediction ce1: " << GPSWeekSecond(ce1.getTimeOfPrediction()).printf("%F, %g") << endl;
outf << "CNAV Accuracy Test: " << SV_CNAV_ACCURACY_GPS_MAX_INDEX[URAoe+15] << endl;
outf << "legacy Accuracy Test: " << SV_ACCURACY_GPS_MAX_INDEX[URAoe] << endl;
// Second test case. Create an CE object with data available from navdump.
outf << endl << "Test Case 2: Creating CE object with data from navdump." << endl;
outf << "Time = " << ct2 << endl;
CNAVEphemeris ce2;
ce2.loadData( SysID, obsID2, PRNID2, AlertMsg10, TOWMsg10_2, AlertMsg11,
TOWMsg11_2, TOWWeek2, Top2, URAoe2, L1Health, L2Health,
L5Health, Toe2, accuracy2, Cuc2, Cus2, Crc2, Crs2, Cic2,
Cis2, M02, dn2, dnDot2, ecc2, deltaA2, Adot2, OMEGA02,
i02, w2, deltaOMEGAdot2, idot2 );
Xv xv2 = ce2.svXv( dt2 );
outf << "Position ce2: " << xv2.x << endl;
outf << "Velocity ce2: " << xv2.v << endl;
outf << "RelCorr ce2: " << ce2.svRelativity(dt2) << endl;
outf << "Time of Prediction ce2: " << GPSWeekSecond(ce2.getTimeOfPrediction()).printf("%F, %g") << endl;
// Third test case. Create an CE object with data available from navdump.
outf << endl << "Test Case 3: Creating CE object with data from navdump." << endl;
outf << "Time = " << ct3 << endl;
CNAVEphemeris ce3;
ce3.loadData( SysID, obsID, PRNID3, AlertMsg10, TOWMsg10_3, AlertMsg11,
TOWMsg11_3, TOWWeek3, Top3, URAoe3, L1Health, L2Health,
L5Health, Toe3, accuracy3, Cuc3, Cus3, Crc3, Crs3, Cic3,
Cis3, M03, dn3, dnDot3, ecc3, deltaA3, Adot3, OMEGA03,
i03, w3, deltaOMEGAdot3, idot3 );
Xv xv3 = ce3.svXv( dt3 );
outf << "Position ce3: " << xv3.x << endl;
outf << "Velocity ce3: " << xv3.v << endl;
outf << "RelCorr ce3: " << ce3.svRelativity(dt3) << endl;
outf << "Time of Prediction ce3: " << GPSWeekSecond(ce3.getTimeOfPrediction()).printf("%F, %g") << endl;
// Fourth test case. Compare against "classic" EngEphemeris
outf << endl << "Test Case 4: Calculated position using 'classic' EngEphemeris." << endl;
outf<< "Time= "<< g << endl;
EngEphemeris EE;
EE.addSubframe(subframe1, TOWWeek, 3, 1);
EE.addSubframe(subframe2, TOWWeek, 3, 1);
EE.addSubframe(subframe3, TOWWeek, 3, 1);
Xvt xvt = EE.svXvt(dt);
outf<< "Position EE: " << xvt.x << endl;
outf<< "Velocity EE: " << xvt.v << endl;
outf<< "RelCorr EE: " << EE.svRelativity(dt) << endl;
outf << endl;
outf << "CE Object Dump:" << endl;
outf << ce1 << endl;
if ( ce1.getOrbit().isHealthy()) outf << "CE.orbit is healthy." << endl;
else outf << "CE.orbit is NOT healthy." << endl;
outf << endl;
outf << "CE2 Object Dump:" << endl;
outf << ce2 << endl;
if ( ce2.getOrbit().isHealthy()) outf << "CE2.orbit is healthy." << endl;
else outf << "CE2.orbit is NOT healthy." << endl;
outf << endl;
outf << "CE3 Object Dump:" << endl;
outf << ce3 << endl;
if ( ce3.getOrbit().isHealthy()) outf << "CE3.orbit is healthy." << endl;
else outf << "CE3.orbit is NOT healthy." << endl;
outf << endl;
outf << "Fit Interval Tests" << endl;
outf << "BeginFit ce1: " << GPSWeekSecond(ce1.getOrbit().getBeginningOfFitInterval()).printf("%F, %g") << endl;
outf << "BeginFit EE: " << GPSWeekSecond(EE.getOrbit().getBeginningOfFitInterval()).printf("%F, %g") << endl;
outf << endl;
outf << "EndFit ce1: " << GPSWeekSecond(ce1.getOrbit().getEndOfFitInterval()).printf("%F, %g") << endl;
outf << "EndFit EE : " << GPSWeekSecond(EE.getOrbit().getEndOfFitInterval()).printf("%F, %g") << endl;
outf << endl;
outf << "Within Fit Interval: " << ce1.getOrbit().withinFitInterval(dt) << endl;
outf << "Within Fit Interval: " << EE.getOrbit().withinFitInterval(dt) << endl;
CPPUNIT_ASSERT(fileEqualTest((char*)"Logs/CNAVEphemeris_Truth",(char*)"Logs/CNAVEphemeris_Output"));
}