本文整理汇总了C++中ostream::fill方法的典型用法代码示例。如果您正苦于以下问题：C++ ostream::fill方法的具体用法？C++ ostream::fill怎么用？C++ ostream::fill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ostream的用法示例。
在下文中一共展示了ostream::fill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: exc
void OrbSysGpsC_30::dumpBody(ostream& s) const
throw( InvalidRequest )
{
if (!dataLoadedFlag)
{
InvalidRequest exc("Required data not stored.");
GPSTK_THROW(exc);
}
s << endl
<< " GROUP DELAY CORRECTIONS"
<< endl
<< "Parameter Avail? Value" << endl;
s.setf(ios::scientific, ios::floatfield);
s.precision(8);
s.setf(ios::right, ios::adjustfield);
s.fill(' ');
s << "Tgd ";
if (avail_Tgd)
s << "Y " << setw(16) << Tgd << endl;
else
s << "N" << endl;
s << "ISC(L1CA) ";
if (avail_L1CA)
s << "Y " << setw(16) << ISC_L1CA << endl;
else
s << "N" << endl;
s << "ISC(L2C) ";
if (avail_L2C)
s << "Y " << setw(16) << ISC_L2C << endl;
else
s << "N" << endl;
s << "ISC(L5I5) ";
if (avail_L5I5)
s << "Y " << setw(16) << ISC_L5I5 << endl;
else
s << "N" << endl;
s << "ISC(L5Q5) ";
if (avail_L5Q5)
s << "Y " << setw(16) << ISC_L5Q5 << endl;
else
s << "N" << endl;
s << endl
<< " IONOSPHERIC PARAMETERS"
<< endl;
s << " Alpha 0: " << setw(16) << alpha[0] << " sec "
<< " Beta 0: " << setw(16) << beta[0] << " sec " << endl;
s << " Alpha 1: " << setw(16) << alpha[1] << " sec/rad "
<< " Beta 1: " << setw(16) << beta[1] << " sec/rad " << endl;
s << " Alpha 2: " << setw(16) << alpha[2] << " sec/rad**2"
<< " Beta 2: " << setw(16) << beta[2] << " sec/rad**2" << endl;
s << " Alpha 3: " << setw(16) << alpha[3] << " sec/rad**3"
<< " Beta 3: " << setw(16) << beta[3] << " sec/rad**3" << endl;
} // end of dumpBody() 示例2: dump
void CNAVEphemeris :: dump(ostream& s) const
throw()
{
s.setf(ios::fixed, ios::floatfield);
s.setf(ios::right, ios::adjustfield);
s.setf(ios::uppercase);
s.precision(0);
s.fill(' ');
s << "****************************************************************"
<< "************" << endl
<< "CNAV Message Types 10 and 11" << endl
<< endl
<< "PRN : " << setw(2) << PRNID << " "
<< "System : " << satSys << " "
<< "Carrier: " << ObsID::cbDesc[obsID.band] << " "
<< "Code: " << ObsID::tcDesc[obsID.code] << endl << endl;
s << " Week SOW DOW UTD SOD"
<< " MM/DD/YYYY HH:MM:SS\n";
s << "Transmit Time: ";
timeDisplay(s, getTransmitTime());
s << endl;
s << "Time of Predict:";
timeDisplay(s, getTimeOfPrediction());
s << endl;
s << endl
<< " ACCURACY PARAMETERS"
<< endl
<< endl
<< "URAoe index: " << setw(4) << orbit.getURAoe() << endl;
s.setf(ios::scientific, ios::floatfield);
s.precision(11);
s << endl
<< " SIGNAL PARAMETERS"
<< endl
<< endl
<< "L1 Health bit: " << setw(2) << L1Health << endl
<< "L2 Health bit: " << setw(2) << L2Health << endl
<< "L5 Health bit: " << setw(2) << L5Health << endl
<< setfill(' ') << endl;
s << endl
<< " ORBIT PARAMETERS"
<< endl
<< endl
<< "Semi-major axis: " << setw(18) << orbit.getAhalf() << " m**.5" << endl
<< "Motion correction: " << setw(18) << orbit.getDn() << " rad/sec"
<< endl
<< "Eccentricity: " << setw(18) << orbit.getEcc() << endl
<< "Arg of perigee: " << setw(18) << orbit.getW() << " rad" << endl
<< "Mean anomaly at epoch: " << setw(18) << orbit.getM0() << " rad" << endl
<< "Right ascension: " << setw(18) << orbit.getOmega0() << " rad "
<< setw(18) << orbit.getOmegaDot() << " rad/sec" << endl
<< "Inclination: " << setw(18) << orbit.getI0() << " rad "
<< setw(18) << orbit.getIDot() << " rad/sec" << endl;
s << endl
<< " HARMONIC CORRECTIONS"
<< endl
<< endl
<< "Radial Sine: " << setw(18) << orbit.getCrs() << " m Cosine: "
<< setw(18) << orbit.getCrc() << " m" << endl
<< "Inclination Sine: " << setw(18) << orbit.getCis() << " rad Cosine: "
<< setw(18) << orbit.getCic() << " rad" << endl
<< "In-track Sine: " << setw(18) << orbit.getCus() << " rad Cosine: "
<< setw(18) << orbit.getCuc() << " rad" << endl;
s << "****************************************************************"
<< "************" << endl;
} // end of CNAVEphemeris::dump()示例3: dump
void EngAlmanac::dump(ostream& s, bool checkFlag) const
{
ios::fmtflags oldFlags = s.flags();
s.fill(' ');
s << "****************************************************************"
<< "***************" << endl
<< "Broadcast Almanac (Engineering Units)" << endl
<< endl;
s << endl << " Iono Parameters" << endl << endl;
s << "Alpha: " << scientific << setprecision(6);
for (int i=0; i<4; i++)
s << setw(13) << alpha[i] << " ";
s << " various" << endl;
s << " Beta: " << fixed << setprecision(1);
for (int i=0; i<4; i++)
s << setw(13) << beta[i] << " ";
s << " various" << endl;
s << endl << " UTC Paramters" << endl << endl;
s << scientific << setprecision(8)
<< "A0: " << setw(15) << A0 << " sec" << endl
<< "A1: " << setw(15) << A1 << " sec/sec" << endl
<< fixed << setprecision(1)
<< "dt_ls: " << setw(15) << dt_ls << " sec" << endl
<< "t_ot: " << setw(15) << t_ot << " sec" << endl
<< "wn_t: " << setw(15) << wn_t << " week" << endl
<< "wn_lsf " << setw(15) << wn_lsf << " week" << endl
<< "dn: " << setw(15) << (int)dn << " days" << endl
<< "dt_lsf: " << setw(15) << dt_lsf << " sec" << endl;
s << endl << " Orbit Parameters" << endl << endl;
for (AlmOrbits::const_iterator i = almPRN.begin(); i != almPRN.end(); i++)
s<< scientific << (*i).second;
s << endl << " Special Message" << endl << endl;
StringUtils::hexDumpData(s, special_msg);
s << endl << " Page 25 Health, AS, & SV config" << endl << endl;
s << "Toa: " << setfill(' ') << setw(8) << t_oa
<< ", week: " << setw(5) << wn_a << " (" << alm_wk << ")" << endl << endl
<< "PRN health AS cfg PRN health AS cfg" << endl;
string bits[33];
for (SVBitsMap::const_iterator i = health.begin(); i != health.end(); i++)
{
int prn = i->first;
if (prn >= 1 && prn <= 32)
bits[prn] = int2bin(i->second, 6);
}
for (SVBitsMap::const_iterator i = SV_config.begin(); i != SV_config.end(); i++)
{
int prn = i->first;
if (prn >= 1 && prn <= 32)
{
bits[prn] += " " + int2bin(i->second, 4);
bits[prn].insert(9, " ");
}
}
for (int i=1; i<=16; i++)
s << setw(2) << i << " " << bits[i] << " "
<< setw(2) << i+16 << " " << bits[i+16] << endl;
s << endl;
if (checkFlag)
check(s);
s << endl;
s.flags(oldFlags);
} // end of dump()