Class containing data elements unique to GPS CNav ephemerides.
Definition at line 52 of file GPSCNavEph.hpp.
#include <GPSCNavEph.hpp>
Public Member Functions | |
NavDataPtr | clone () const override |
Create a deep copy of this object. More... | |
void | dumpSVStatus (std::ostream &s) const override |
void | fixFit () |
CommonTime | getUserTime () const override |
GPSCNavEph () | |
Sets the nav message type and all other data members to 0. More... | |
bool | validate () const override |
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GPSCNavData () | |
Initialize data members. More... | |
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bool | getXvt (const CommonTime &when, Xvt &xvt, const ObsID &oid=ObsID()) override |
OrbitDataGPS () | |
double | svRelativity (const CommonTime &when) const override |
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std::list< std::string > | compare (const NavDataPtr &right) const override |
void | dump (std::ostream &s, DumpDetail dl) const override |
virtual void | dumpClock (std::ostream &s) const |
virtual void | dumpHarmonics (std::ostream &s) const |
virtual void | dumpOrbit (std::ostream &s) const |
virtual std::string | getDataType () const |
CommonTime | getNearTime () const override |
bool | getXvt (const CommonTime &when, const EllipsoidModel &ell, Xvt &xvt, const ObsID &oid=ObsID()) |
bool | isSameData (const NavDataPtr &right) const override |
OrbitDataKepler () | |
Initialize all data members to 0. More... | |
double | svClockBias (const CommonTime &when) const |
double | svClockDrift (const CommonTime &when) const |
virtual double | svRelativity (const CommonTime &when, const EllipsoidModel &ell) const |
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virtual std::string | getClassName () const |
std::string | getDumpTime (DumpDetail dl, const CommonTime &t) const |
std::string | getDumpTimeHdr (DumpDetail dl) const |
std::string | getSignalString () const |
bool | getSVN (const SatID &sat, const gnsstk::CommonTime &when, std::string &svn) const |
NavData () | |
Initialize internal data fields. More... | |
Public Attributes | |
bool | alert11 |
Alert flag from message type 11. More... | |
bool | alertClk |
Alert flag from the clock message. More... | |
double | deltaA |
Semi-major axis relative to reference (Aref). More... | |
double | dOMEGAdot |
Rate of right ascension relative to -2.6e-9*pi. More... | |
bool | healthL1 |
L1 signal health from message type 10. More... | |
bool | healthL2 |
L2 signal health from message type 10. More... | |
bool | healthL5 |
L5 signal health from message type 10. More... | |
bool | integStat |
Integrity status flag. More... | |
bool | phasingL2C |
L2C phasing. More... | |
uint32_t | pre11 |
The preamble from the start of message type 11. More... | |
uint32_t | preClk |
CommonTime | top |
Time of prediction. More... | |
int8_t | uraED |
5-bit URA index from message type 10. More... | |
int8_t | uraNED0 |
non-elevation dependent URA from clock message. More... | |
uint8_t | uraNED1 |
non-elevation dependent URA from clock message. More... | |
uint8_t | uraNED2 |
non-elevation dependent URA from clock message. More... | |
CommonTime | xmit11 |
Transmit time for message 11. More... | |
CommonTime | xmitClk |
Transmit time for the clock message. More... | |
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bool | alert |
Alert flag. More... | |
uint32_t | pre |
The preamble from the start of the subframe. More... | |
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double | A |
Semi-major axis (m) More... | |
double | Adot |
Rate of semi-major axis (m/sec) More... | |
double | af0 |
SV clock error (sec) More... | |
double | af1 |
SV clock drift (sec/sec) More... | |
double | af2 |
SV clock drift rate (sec/sec**2) More... | |
double | Ahalf |
Square Root of semi-major axis (m**.5) More... | |
double | Cic |
Cosine inclination (rad) More... | |
double | Cis |
Sine inclination (rad) More... | |
double | Crc |
Cosine radius (m) More... | |
double | Crs |
Sine radius (m) More... | |
double | Cuc |
Cosine latitude (rad) More... | |
double | Cus |
Sine latitude (rad) More... | |
double | dn |
Correction to mean motion (rad/sec) More... | |
double | dndot |
Rate of correction to mean motion (rad/sec/sec) More... | |
double | ecc |
Eccentricity. More... | |
RefFrameSys | frame |
SVHealth | health |
SV health status. More... | |
double | i0 |
Inclination (rad) More... | |
double | idot |
Rate of inclination angle (rad/sec) More... | |
double | M0 |
Mean anomaly (rad) More... | |
double | OMEGA0 |
Longitude of ascending node at weekly epoch (rad) More... | |
double | OMEGAdot |
Rate of Rt ascension (rad/sec) More... | |
CommonTime | Toc |
Clock epoch. More... | |
CommonTime | Toe |
Orbit epoch. More... | |
double | w |
Argument of perigee (rad) More... | |
CommonTime | xmitTime |
Time of transmission of the start of the data. More... | |
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NavMessageID | signal |
Source signal identification for this navigation message data. More... | |
CommonTime | timeStamp |
std::string | weekFmt |
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CommonTime | beginFit |
Time at beginning of fit interval. More... | |
CommonTime | endFit |
Time at end of fit interval. More... | |
Additional Inherited Members | |
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static gnsstk::SatMetaDataStore * | getSatMetaDataStore () |
Accessor for python. More... | |
static void | setSatMetaDataStore (gnsstk::SatMetaDataStore *smds) |
Accessor for python. More... | |
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static const GNSSTK_EXPORT double | refAGPS = 26559710 |
static const GNSSTK_EXPORT double | refAQZSS = 42164200 |
static const GNSSTK_EXPORT double | refdeltaiGPS = 0.0056 * PI |
static const GNSSTK_EXPORT double | refdeltaiQZSS = 0.0056 * PI |
static const GNSSTK_EXPORT double | refEccGPS = 0 |
static const GNSSTK_EXPORT double | refEccQZSS = 0.075 |
static const GNSSTK_EXPORT double | refi0GPS = 0.3 * PI |
static const GNSSTK_EXPORT double | refi0QZSS = 0.25 * PI |
static const GNSSTK_EXPORT double | refOMEGAdotEphGPS = -2.6e-9 * PI |
static const GNSSTK_EXPORT double | refOMEGAdotEphQZSS = -2.6e-9 * PI |
Ephemeris OMEGA dot reference value for QZSS (radians). More... | |
static const GNSSTK_EXPORT double | refOMEGAdotRedAlmGPS = -2.6e-9 * PI |
static const GNSSTK_EXPORT double | refOMEGAdotRedAlmQZSS = -8.7e-10 * PI |
Reduced almanac OMEGA dot reference value for QZSS (radians). More... | |
static const GNSSTK_EXPORT double | refwGPS = 0 |
Argument of perigee reference value (radians, guessed at). More... | |
static const GNSSTK_EXPORT double | refwQZSS = 2.0 * PI * 270.0 / 360.0 |
Argument of perigee reference value in IS-QZSS (radians). More... | |
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static const size_t | fw = 16 |
Field width of floating point numbers (precision + 8). More... | |
static const size_t | precision = 8 |
Precision used when printing floating point numbers. More... | |
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static const GNSSTK_EXPORT std::string | dumpTimeFmt |
Time format used for the dump method (Full). More... | |
static const GNSSTK_EXPORT std::string | dumpTimeFmtBrief |
Time format used for the dump method (Brief). More... | |
static GNSSTK_EXPORT gnsstk::SatMetaDataStore * | satMetaDataStore = nullptr |
Set this to a valid store to get PRN->SVN translations in dump(). More... | |
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double | msgLenSec |
gnsstk::GPSCNavEph::GPSCNavEph | ( | ) |
Sets the nav message type and all other data members to 0.
Definition at line 48 of file GPSCNavEph.cpp.
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inlineoverridevirtual |
Create a deep copy of this object.
Implements gnsstk::NavData.
Definition at line 58 of file GPSCNavEph.hpp.
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overridevirtual |
Dump SV status information (e.g. health).
[in,out] | s | The stream to write the data to. |
Reimplemented from gnsstk::OrbitDataKepler.
Definition at line 129 of file GPSCNavEph.cpp.
void gnsstk::GPSCNavEph::fixFit | ( | ) |
Fill the beginFit and endFit values for this object.
Definition at line 91 of file GPSCNavEph.cpp.
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overridevirtual |
Returns the time when the navigation message would have first been available to the user equipment, i.e. the time at which the final bit of a given broadcast navigation message is received. This is used by NavDataFactoryWithStore::find() in User mode.
Reimplemented from gnsstk::NavData.
Definition at line 81 of file GPSCNavEph.cpp.
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overridevirtual |
Checks the contents of this message against known validity rules as defined in the appropriate ICD.
Reimplemented from gnsstk::GPSCNavData.
Definition at line 73 of file GPSCNavEph.cpp.
bool gnsstk::GPSCNavEph::alert11 |
Alert flag from message type 11.
Definition at line 96 of file GPSCNavEph.hpp.
bool gnsstk::GPSCNavEph::alertClk |
Alert flag from the clock message.
Definition at line 97 of file GPSCNavEph.hpp.
double gnsstk::GPSCNavEph::deltaA |
Semi-major axis relative to reference (Aref).
Definition at line 100 of file GPSCNavEph.hpp.
double gnsstk::GPSCNavEph::dOMEGAdot |
Rate of right ascension relative to -2.6e-9*pi.
Definition at line 101 of file GPSCNavEph.hpp.
bool gnsstk::GPSCNavEph::healthL1 |
L1 signal health from message type 10.
Definition at line 89 of file GPSCNavEph.hpp.
bool gnsstk::GPSCNavEph::healthL2 |
L2 signal health from message type 10.
Definition at line 90 of file GPSCNavEph.hpp.
bool gnsstk::GPSCNavEph::healthL5 |
L5 signal health from message type 10.
Definition at line 91 of file GPSCNavEph.hpp.
bool gnsstk::GPSCNavEph::integStat |
Integrity status flag.
Definition at line 98 of file GPSCNavEph.hpp.
bool gnsstk::GPSCNavEph::phasingL2C |
L2C phasing.
Definition at line 99 of file GPSCNavEph.hpp.
uint32_t gnsstk::GPSCNavEph::pre11 |
The preamble from the start of message type 11.
Definition at line 86 of file GPSCNavEph.hpp.
uint32_t gnsstk::GPSCNavEph::preClk |
The preamble from the start of the clock message.
Definition at line 87 of file GPSCNavEph.hpp.
CommonTime gnsstk::GPSCNavEph::top |
Time of prediction.
Definition at line 102 of file GPSCNavEph.hpp.
int8_t gnsstk::GPSCNavEph::uraED |
5-bit URA index from message type 10.
Definition at line 92 of file GPSCNavEph.hpp.
int8_t gnsstk::GPSCNavEph::uraNED0 |
non-elevation dependent URA from clock message.
Definition at line 93 of file GPSCNavEph.hpp.
uint8_t gnsstk::GPSCNavEph::uraNED1 |
non-elevation dependent URA from clock message.
Definition at line 94 of file GPSCNavEph.hpp.
uint8_t gnsstk::GPSCNavEph::uraNED2 |
non-elevation dependent URA from clock message.
Definition at line 95 of file GPSCNavEph.hpp.
CommonTime gnsstk::GPSCNavEph::xmit11 |
Transmit time for message 11.
Definition at line 103 of file GPSCNavEph.hpp.
CommonTime gnsstk::GPSCNavEph::xmitClk |
Transmit time for the clock message.
Definition at line 104 of file GPSCNavEph.hpp.