#include <EngEphemeris.hpp>
Inheritance diagram for EngEphemeris:


This class encapsulates the ephemeris navigation message (subframes 1-3) and provides functions to decode the as-broadcast ephemerides.
Definition at line 70 of file EngEphemeris.hpp.
Public Member Functions | ||||
| EngEphemeris () throw () | ||||
| Default constructor. | ||||
| virtual | ~EngEphemeris () | |||
| Destructor. | ||||
| bool | addSubframe (const long subframe[10], const int gpsWeek, short PRN, short track) throw (gpstk::InvalidParameter) | |||
| Store a subframe in this object. | ||||
| bool | addSubframeNoParity (const long subframe[10], const long gpsWeek, const short PRN, const short track) throw (gpstk::InvalidParameter) | |||
| Store a subframe in this object. | ||||
| bool | addIncompleteSF1Thru3 (const long sf1[8], const long sf2[8], const long sf3[8], const long sf1TransmitSOW, const int gpsWeek, const short PRN, const short track) | |||
| Store a subframe in this object. | ||||
| bool | isData (short subframe) const throw (gpstk::InvalidRequest) | |||
| Query presence of subframe in this object. | ||||
| void | setAccuracy (const double &acc) throw (gpstk::InvalidParameter) | |||
| Set the value of the SV accuracy (in meters). | ||||
| short | getFitInterval () const throw (gpstk::InvalidRequest) | |||
| This computes and returns the fit interval for the satellite ephemeris from the IODC and the fit interval flag. | ||||
| unsigned char | getTLMPreamble () const throw () | |||
| Return 0x8b, the upper 5 bits of the 22-bit TLM word. | ||||
| unsigned | getTLMMessage (short subframe) const throw (gpstk::InvalidRequest) | |||
| Return the lower 16 bits of the TLM word for the given subframe. | ||||
| DayTime | getEphemerisEpoch () const throw (InvalidRequest) | |||
| Extracts the epoch time from this ephemeris, correcting for half weeks and HOW time. | ||||
| DayTime | getEpochTime () const throw (gpstk::InvalidRequest) | |||
| Extracts the epoch time (time of clock) from this ephemeris, correcting for half weeks and HOW time. | ||||
| DayTime | getTransmitTime () const throw (gpstk::InvalidRequest) | |||
| Extracts the transmit time from the ephemeris using the Tot. | ||||
| DayTime | getTimestamp () const throw (gpstk::InvalidRequest) | |||
| used for template functions | ||||
| short | getPRNID () const throw (gpstk::InvalidRequest) | |||
| This function returns the PRN ID of the SV. | ||||
| short | getTracker () const throw (gpstk::InvalidRequest) | |||
| This function returns the tracker number. | ||||
| double | getHOWTime (short subframe) const throw (gpstk::InvalidRequest) | |||
| This function returns the time of the HOW in subframe 1 or 2 or 3 in seconds of week. | ||||
| short | getASAlert (short subframe) const throw (gpstk::InvalidRequest) | |||
| This function returns the A-S alert flag for either subframe 1 or 2 or 3. | ||||
| short | getFullWeek () const throw (gpstk::InvalidRequest) | |||
| This function return the GPS week number for the ephemeris. | ||||
| short | getCodeFlags () const throw (gpstk::InvalidRequest) | |||
| This function returns the values of the L2 codes. | ||||
| double | getAccuracy () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the SV accuracy (m) computed from the accuracy flag in the nav message, or as set by the setAccuracy() method. | ||||
| short | getAccFlag () const throw (gpstk::InvalidRequest) | |||
| This function returns the flag based on the SV accuracy flag as it appears in the nav message. | ||||
| short | getHealth () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the SV health flag. | ||||
| short | getL2Pdata () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the L2 P-code data flag. | ||||
| short | getIODC () const throw (gpstk::InvalidRequest) | |||
| This function returns the IODC for the given PRN. | ||||
| short | getIODE () const throw (gpstk::InvalidRequest) | |||
| This function return the IODE for the ephemeris. | ||||
| long | getAODO () const throw (gpstk::InvalidRequest) | |||
| This function return the AODO for the ephemeris. | ||||
| double | getToc () const throw (gpstk::InvalidRequest) | |||
| This function returns the clock epoch in GPS seconds of week. | ||||
| double | getAf0 () const throw (gpstk::InvalidRequest) | |||
| This function returns the SV clock error in seconds. | ||||
| double | getAf1 () const throw (gpstk::InvalidRequest) | |||
| This function returns the SV clock drift in seconds/seconds. | ||||
| double | getAf2 () const throw (gpstk::InvalidRequest) | |||
| This function returns the SV clock rate of change of the drift in seconds/(seconds*seconds). | ||||
| double | getTgd () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the group delay differential in seconds. | ||||
| double | getCus () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the sine latitude harmonic perturbation in radians. | ||||
| double | getCrs () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the sine radius harmonic perturbation in meters. | ||||
| double | getCis () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the sine inclination harmonic perturbation in radians. | ||||
| double | getCrc () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the cosine radius harmonic perturbation in meters. | ||||
| double | getCuc () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the cosine latitude harmonic perturbation in radians. | ||||
| double | getCic () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the cosine inclination harmonic perturbation in radians. | ||||
| double | getToe () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the time of ephemeris in GPS seconds of week. | ||||
| double | getM0 () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the mean anomaly in radians. | ||||
| double | getDn () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the correction to the mean motion in radians/second. | ||||
| double | getEcc () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the eccentricity. | ||||
| double | getAhalf () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the square root of the semi-major axis in square root of meters. | ||||
| double | getA () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the semi-major axis in meters. | ||||
| double | getOmega0 () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the right ascension of the ascending node in radians. | ||||
| double | getI0 () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the inclination in radians. | ||||
| double | getW () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the argument of perigee in radians. | ||||
| double | getOmegaDot () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the rate of the right ascension of the ascending node in radians/second. | ||||
| double | getIDot () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the rate of the inclination in radians/second. | ||||
| Xvt | svXvt (const DayTime &t) const throw (gpstk::InvalidRequest) | |||
| Compute satellite velocity/position at the given time using this ephemeris. | ||||
| double | svRelativity (const DayTime &t) const throw (gpstk::InvalidRequest) | |||
Compute satellite relativity correction (sec) at the given time
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| double | svClockBias (const DayTime &t) const throw (gpstk::InvalidRequest) | |||
Compute the satellite clock bias (sec) at the given time
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| double | svClockDrift (const DayTime &t) const throw (gpstk::InvalidRequest) | |||
Compute the satellite clock drift (sec/sec) at the given time
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| short | getFitInt () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the fit interval flag. | ||||
| double | getEphkey () const throw (gpstk::InvalidRequest) | |||
| This function returns the value of the ephemeris key that is used to sort the ephemerides when they are stored in the bcetable. | ||||
| long | getTot () const throw (gpstk::InvalidRequest) | |||
| This function returnst the value of the Time of Transmit. | ||||
| EngEphemeris & | setSF1 (unsigned tlm, double how, short asalert, short fullweek, short cflags, short acc, short svhealth, short iodc, short l2pdata, double tgd, double toc, double Af2, double Af1, double Af0, short Tracker, short prn) throw () | |||
| Set the values contained in SubFrame 1. | ||||
| EngEphemeris & | setSF2 (unsigned tlm, double how, short asalert, short iode, double crs, double Dn, double m0, double cuc, double Ecc, double cus, double ahalf, double toe, short fitInt) throw () | |||
| Set the values contained in SubFrame 2. | ||||
| EngEphemeris & | setSF3 (unsigned tlm, double how, short asalert, double cic, double Omega0, double cis, double I0, double crc, double W, double OmegaDot, double IDot) throw () | |||
| Set the values contained in SubFrame 2. | ||||
| void | dump (std::ostream &s=std::cout) const | |||
| Output the contents of this ephemeris to the given stream. | ||||
Protected Attributes | ||||
| bool | haveSubframe [3] | |||
| flags indicating presence of a subframe | ||||
| unsigned short | tlm_message [3] | |||
| short | PRNID | |||
| SV PRN ID. | ||||
| short | tracker | |||
| Tracker number. | ||||
| long | HOWtime [3] | |||
| Time of subframe 1-3 (sec of week). | ||||
| short | ASalert [3] | |||
| A-S and "alert" flags for each subframe. | ||||
| short | weeknum | |||
| GPS full week number that corresponds to the HOWtime of SF1. | ||||
| short | codeflags | |||
| L2 codes. | ||||
| double | accuracy | |||
| SV accuracy (m). | ||||
| short | accFlag | |||
| User Range Accuracy (URA) the accuracy flag. | ||||
| short | health | |||
| SV health. | ||||
| short | L2Pdata | |||
| L2 P data flag. | ||||
| short | IODC | |||
| Index of data-clock. | ||||
| short | IODE | |||
| Index of data-eph. | ||||
| long | AODO | |||
| Age of Data Offset for NMCT. | ||||
| double | Toc | |||
| Clock epoch (sec of week). | ||||
| double | af0 | |||
| SV clock error (sec). | ||||
| double | af1 | |||
| SV clock drift (sec/sec). | ||||
| double | af2 | |||
| SV clock drift rate (sec/sec**2). | ||||
| double | Tgd | |||
| Group delay differential (sec). | ||||
| double | Cuc | |||
| Cosine latitude (rad). | ||||
| double | Cus | |||
| Sine latitude (rad). | ||||
| double | Crc | |||
| Cosine radius (m). | ||||
| double | Crs | |||
| Sine radius (m). | ||||
| double | Cic | |||
| Cosine inclination (rad). | ||||
| double | Cis | |||
| Sine inclination (rad). | ||||
| double | Toe | |||
| Ephemeris epoch (sec of week). | ||||
| double | M0 | |||
| Mean anomaly (rad). | ||||
| double | dn | |||
| Correction to mean motion (rad/sec). | ||||
| double | ecc | |||
| Eccentricity. | ||||
| double | Ahalf | |||
| SQRT of semi-major axis (m**1/2). | ||||
| double | OMEGA0 | |||
| Rt ascension of ascending node (rad). | ||||
| double | i0 | |||
| Inclination (rad). | ||||
| double | w | |||
| Argument of perigee (rad). | ||||
| double | OMEGAdot | |||
| Rate of Rt ascension (rad/sec). | ||||
| double | idot | |||
| Rate of inclination angle (rad/sec). | ||||
| short | fitint | |||
| Fit interval flag. | ||||
Friends | ||||
| std::ostream & | operator<< (std::ostream &s, const EngEphemeris &eph) | |||
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Destructor.
Definition at line 77 of file EngEphemeris.hpp. |
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Store a subframe in this object. This method is provided in order to provide a path to a EngEphemeris object for cases where a receiver only provides words 3-10 of subframes 1-3.
Definition at line 182 of file EngEphemeris.cpp. References EngEphemeris::accFlag, EngEphemeris::accuracy, EngEphemeris::af0, EngEphemeris::af1, EngEphemeris::af2, EngEphemeris::Ahalf, EngEphemeris::ASalert, EngEphemeris::Cic, EngEphemeris::Cis, EngEphemeris::codeflags, EngEphemeris::Crc, EngEphemeris::Crs, EngEphemeris::Cuc, EngEphemeris::Cus, EngEphemeris::dn, EngEphemeris::ecc, EngEphemeris::fitint, EngEphemeris::haveSubframe, EngEphemeris::health, EngEphemeris::HOWtime, EngEphemeris::i0, EngEphemeris::idot, EngEphemeris::IODC, EngEphemeris::IODE, EngEphemeris::L2Pdata, EngEphemeris::M0, EngEphemeris::OMEGA0, EngEphemeris::OMEGAdot, EngEphemeris::PRNID, EngNav::subframeConvert(), EngEphemeris::Tgd, EngEphemeris::tlm_message, EngEphemeris::Toc, EngEphemeris::Toe, EngEphemeris::tracker, gpstk::ura2accuracy(), EngEphemeris::w, and EngEphemeris::weeknum. Referenced by MinSfTest::process(). |
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Store a subframe in this object.
Definition at line 83 of file EngEphemeris.cpp. References GPSTK_THROW, and gpstk::ura2accuracy(). Referenced by gpstk::makeEngEphemeris(), FICData::operator EngEphemeris(), and NovatelData::operator RinexNavData(). |
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Store a subframe in this object. This method is provided in order to allow construction of an EngEphemeris object for cases where a receiver only provides the 24 msb of each word and strips the parity.l
Definition at line 161 of file EngEphemeris.cpp. |
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Output the contents of this ephemeris to the given stream.
Definition at line 1217 of file EngEphemeris.cpp. References EngEphemeris::accFlag, EngEphemeris::af0, EngEphemeris::af1, EngEphemeris::af2, EngEphemeris::Ahalf, EngEphemeris::ASalert, EngEphemeris::Cic, EngEphemeris::Cis, EngEphemeris::Crc, EngEphemeris::Crs, EngEphemeris::Cuc, EngEphemeris::Cus, EngEphemeris::dn, EngEphemeris::ecc, EngEphemeris::fitint, EngEphemeris::getEphemerisEpoch(), EngEphemeris::getEpochTime(), EngEphemeris::getFitInt(), DayTime::GPSsecond(), EngEphemeris::health, EngEphemeris::HOWtime, EngEphemeris::i0, EngEphemeris::idot, EngEphemeris::L2Pdata, EngEphemeris::M0, EngEphemeris::OMEGA0, EngEphemeris::OMEGAdot, EngEphemeris::PRNID, EngEphemeris::Tgd, EngEphemeris::w, and EngEphemeris::weeknum. Referenced by gpstk::operator<<(). |
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This function returns the value of the semi-major axis in meters.
Definition at line 973 of file EngEphemeris.cpp. References EngEphemeris::Ahalf, GPSTK_THROW, and EngEphemeris::haveSubframe. |
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This function returns the flag based on the SV accuracy flag as it appears in the nav message.
Definition at line 731 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), ComputeIURAWeights::getWeight(), SimpleIURAWeight::getWeights(), and MinSfTest::process(). |
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This function returns the value of the SV accuracy (m) computed from the accuracy flag in the nav message, or as set by the setAccuracy() method.
Definition at line 720 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the SV clock error in seconds.
Definition at line 808 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the SV clock drift in seconds/seconds.
Definition at line 819 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the SV clock rate of change of the drift in seconds/(seconds*seconds).
Definition at line 830 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the square root of the semi-major axis in square root of meters.
Definition at line 962 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function return the AODO for the ephemeris.
Definition at line 786 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. |
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This function returns the A-S alert flag for either subframe 1 or 2 or 3.
Definition at line 686 of file EngEphemeris.cpp. References GPSTK_THROW. Referenced by FICData9::firstFiveItems(). |
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This function returns the value of the cosine inclination harmonic perturbation in radians.
Definition at line 907 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the sine inclination harmonic perturbation in radians.
Definition at line 874 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the values of the L2 codes.
Definition at line 709 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the cosine radius harmonic perturbation in meters.
Definition at line 885 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the sine radius harmonic perturbation in meters.
Definition at line 863 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the cosine latitude harmonic perturbation in radians.
Definition at line 896 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the sine latitude harmonic perturbation in radians.
Definition at line 852 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the correction to the mean motion in radians/second.
Definition at line 940 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the eccentricity.
Definition at line 951 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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Extracts the epoch time from this ephemeris, correcting for half weeks and HOW time.
Definition at line 637 of file EngEphemeris.cpp. References EngEphemeris::getFullWeek(), EngEphemeris::getHOWTime(), EngEphemeris::getToe(), and DayTime::setGPSfullweek(). Referenced by EngEphemeris::dump(). |
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This function returns the value of the ephemeris key that is used to sort the ephemerides when they are stored in the bcetable.
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Extracts the epoch time (time of clock) from this ephemeris, correcting for half weeks and HOW time.
Definition at line 624 of file EngEphemeris.cpp. References EngEphemeris::getFullWeek(), EngEphemeris::getHOWTime(), EngEphemeris::getToc(), and DayTime::setGPSfullweek(). Referenced by GPSEphemerisStore::dump(), GalEphemerisStore::dump(), EngEphemeris::dump(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the fit interval flag.
Definition at line 1039 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by EngEphemeris::dump(), FICData9::FICData9(), EngEphemeris::getFitInterval(), and MinSfTest::process(). |
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This computes and returns the fit interval for the satellite ephemeris from the IODC and the fit interval flag. This fit interval is centered around the Toe (time of ephemeris) for the ephemeris. See Table 20-XIA in the ICD-GPS-200 and section 20.3.3.4.3.1 for more information.
Definition at line 522 of file EngEphemeris.cpp. References EngEphemeris::getFitInt(), and EngEphemeris::getIODC(). Referenced by GPSEphemerisStore::findNearEphemeris(), GalEphemerisStore::findNearEphemeris(), GPSEphemerisStore::findUserEphemeris(), GalEphemerisStore::findUserEphemeris(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function return the GPS week number for the ephemeris. this is the full GPS week (ie > 10 bits). Definition at line 698 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by EngEphemeris::getEphemerisEpoch(), EngEphemeris::getEpochTime(), EngEphemeris::getTransmitTime(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the SV health flag.
Definition at line 742 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), GPSEphemerisStore::getSatHealth(), GalEphemerisStore::getSatHealth(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the time of the HOW in subframe 1 or 2 or 3 in seconds of week.
Definition at line 672 of file EngEphemeris.cpp. References GPSTK_THROW. Referenced by FICData9::firstFiveItems(), EngEphemeris::getEphemerisEpoch(), EngEphemeris::getEpochTime(), EngEphemeris::getTot(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the inclination in radians.
Definition at line 995 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the rate of the inclination in radians/second.
Definition at line 1028 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the IODC for the given PRN.
Definition at line 764 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), EngEphemeris::getFitInterval(), GPSEphemerisStore::getXvt(), GalEphemerisStore::getXvt(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function return the IODE for the ephemeris.
Definition at line 775 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the L2 P-code data flag.
Definition at line 753 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), MinSfTest::process(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the mean anomaly in radians.
Definition at line 929 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the right ascension of the ascending node in radians.
Definition at line 984 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the rate of the right ascension of the ascending node in radians/second.
Definition at line 1017 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the PRN ID of the SV.
Definition at line 650 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the group delay differential in seconds.
Definition at line 841 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), ModelObsFixedStation::getTGDCorrections(), ModeledReferencePR::getTGDCorrections(), BasicModel::getTGDCorrections(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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used for template functions
Definition at line 198 of file EngEphemeris.hpp. |
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Return the lower 16 bits of the TLM word for the given subframe.
Definition at line 604 of file EngEphemeris.cpp. References GPSTK_THROW. Referenced by FICData9::firstFiveItems(). |
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Return 0x8b, the upper 5 bits of the 22-bit TLM word.
Definition at line 180 of file EngEphemeris.hpp. |
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This function returns the clock epoch in GPS seconds of week.
Definition at line 797 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), EngEphemeris::getEpochTime(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returns the value of the time of ephemeris in GPS seconds of week.
Definition at line 918 of file EngEphemeris.cpp. References GPSTK_THROW, and EngEphemeris::haveSubframe. Referenced by FICData9::FICData9(), EngEphemeris::getEphemerisEpoch(), Rinex3NavData::Rinex3NavData(), and RinexNavData::RinexNavData(). |
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This function returnst the value of the Time of Transmit. Basically just the earliest of the HOWs. Definition at line 1050 of file EngEphemeris.cpp. References EngEphemeris::getHOWTime(), GPSTK_THROW, EngEphemeris::haveSubframe, and gpstk::min(). Referenced by EngEphemeris::getTransmitTime(). |