Satellite position data - for determining and storing satellite positions/clocks. More...

Detailed Description

Satellite position data - for determining and storing satellite positions/clocks.

Inheritance diagram for SatPos:

Collaboration diagram for SatPos:

Public Member Functions
	SatPos ()

Data Fields
GTime	posTime

SatSys	Sat = {}

SatNav *	satNav_ptr = nullptr
	‍Satellite ID (system, prn)

SatStat *	satStat_ptr = nullptr
	Pointer to a status object for this satellite.

E_Source	posSource = E_Source::NONE

E_Source	clkSource = E_Source::NONE

VectorEcef	rSatCom
	ECEF based vector of satellite.

VectorEcef	rSatApc
	ECEF based vector of satellite.

VectorEcef	satVel
	ECEF based vector of satellite velocity.

VectorEci	rSatEciDt
	ECI based vector of satellite at transmission time.

VectorEci	vSatEciDt
	ECI based vector of satellite velocity at transmission time.

VectorEci	rSatEci0
	ECI based vector of satellite at nominal epoch.

VectorEci	vSatEci0
	ECI based vector of satellite velocity at nominal epoch.

double	posVar = 0
	Variance of ephemeris derived values.

double	satClk = 0

double	satClkVel = 0

double	satClkVar = 0

bool	sppValid = 0
	Valid satellite flag.

int	iodeClk = -1
	Issue of data ephemeris.

int	iodePos = -1
	Issue of data ephemeris.

bool	ephPosValid = false

bool	ephClkValid = false

double	tof = 0
	Estimated time of flight.

union {

const unsigned int failure = 0

struct {

unsigned failureExclude: 1

unsigned failureNoSatPos: 1

unsigned failureNoSatClock: 1

unsigned failureNoPseudorange: 1

unsigned failureIodeConsistency: 1

unsigned failureBroadcastEph: 1

unsigned failureSSRFail: 1

unsigned failureSsrPosEmpty: 1

unsigned failureSsrClkEmpty: 1

unsigned failureSsrPosTime: 1

unsigned failureSsrClkTime: 1

unsigned failureSsrPosMag: 1

unsigned failureSsrClkMag: 1

unsigned failureSsrPosUdi: 1

unsigned failureSsrClkUdi: 1

unsigned failureGeodist: 1

unsigned failureRSat: 1

unsigned failureElevation: 1

unsigned failurePrange: 1

unsigned failureIonocorr: 1

}

};

Constructor & Destructor Documentation

◆ SatPos()

SatPos::SatPos ( )

inline

Field Documentation

◆ [union]

union { ... } SatPos

◆ clkSource

E_Source SatPos::clkSource = E_Source::NONE

◆ ephClkValid

bool SatPos::ephClkValid = false

◆ ephPosValid

bool SatPos::ephPosValid = false

◆ failure

const unsigned int SatPos::failure = 0

◆ failureBroadcastEph

unsigned SatPos::failureBroadcastEph

◆ failureElevation

unsigned SatPos::failureElevation

◆ failureExclude

unsigned SatPos::failureExclude

◆ failureGeodist

unsigned SatPos::failureGeodist

◆ failureIodeConsistency

unsigned SatPos::failureIodeConsistency

◆ failureIonocorr

unsigned SatPos::failureIonocorr

◆ failureNoPseudorange

unsigned SatPos::failureNoPseudorange

◆ failureNoSatClock

unsigned SatPos::failureNoSatClock

◆ failureNoSatPos

unsigned SatPos::failureNoSatPos

◆ failurePrange

unsigned SatPos::failurePrange

◆ failureRSat

unsigned SatPos::failureRSat

◆ failureSsrClkEmpty

unsigned SatPos::failureSsrClkEmpty

◆ failureSsrClkMag

unsigned SatPos::failureSsrClkMag

◆ failureSsrClkTime

unsigned SatPos::failureSsrClkTime

◆ failureSsrClkUdi

unsigned SatPos::failureSsrClkUdi

◆ failureSSRFail

unsigned SatPos::failureSSRFail

◆ failureSsrPosEmpty

unsigned SatPos::failureSsrPosEmpty

◆ failureSsrPosMag

unsigned SatPos::failureSsrPosMag

◆ failureSsrPosTime

unsigned SatPos::failureSsrPosTime

◆ failureSsrPosUdi

unsigned SatPos::failureSsrPosUdi

◆ iodeClk

int SatPos::iodeClk = -1

Issue of data ephemeris.

◆ iodePos

int SatPos::iodePos = -1

Issue of data ephemeris.

◆ posSource

E_Source SatPos::posSource = E_Source::NONE

◆ posTime

GTime SatPos::posTime

◆ posVar

double SatPos::posVar = 0

Variance of ephemeris derived values.

◆ rSatApc

VectorEcef SatPos::rSatApc

ECEF based vector of satellite.

◆ rSatCom

VectorEcef SatPos::rSatCom

ECEF based vector of satellite.

◆ rSatEci0

VectorEci SatPos::rSatEci0

ECI based vector of satellite at nominal epoch.

◆ rSatEciDt

VectorEci SatPos::rSatEciDt

ECI based vector of satellite at transmission time.

◆ Sat

SatSys SatPos::Sat = {}

◆ satClk

double SatPos::satClk = 0

◆ satClkVar

double SatPos::satClkVar = 0

◆ satClkVel

double SatPos::satClkVel = 0

◆ satNav_ptr

SatNav* SatPos::satNav_ptr = nullptr

‍Satellite ID (system, prn)

Pointer to a navigation object for this satellite

◆ satStat_ptr

SatStat* SatPos::satStat_ptr = nullptr

Pointer to a status object for this satellite.

◆ satVel

VectorEcef SatPos::satVel

ECEF based vector of satellite velocity.

◆ sppValid

bool SatPos::sppValid = 0

Valid satellite flag.

◆ tof

double SatPos::tof = 0

Estimated time of flight.

◆ vSatEci0

VectorEci SatPos::vSatEci0

ECI based vector of satellite velocity at nominal epoch.

◆ vSatEciDt

VectorEci SatPos::vSatEciDt

ECI based vector of satellite velocity at transmission time.

The documentation for this struct was generated from the following file:

/ginan/src/cpp/common/observations.hpp