Broadcasted ephemeris message data. More...

Data Structures
struct	SvHealth
	Navigation Data Validity and Signal Health Status. More...

Public Member Functions
Corrections	calcClockCorrections (const InsTime &recvTime, double dist, const Frequency &freq) const final
	Calculates clock bias and drift of the satellite.

double	calcSatellitePositionVariance () const final
	Calculates the Variance of the satellite position in [m^2].

	GalileoEphemeris (const GalileoEphemeris &)=default
	Copy constructor.

	GalileoEphemeris (const InsTime &toc)
	Default Constructor.

	GalileoEphemeris (const InsTime &toc, const InsTime &toe, const size_t &IODnav, const std::array< double, 3 > &a, const double &sqrt_A, const double &e, const double &i_0, const double &Omega_0, const double &omega, const double &M_0, const double &delta_n, const double &Omega_dot, const double &i_dot, const double &Cus, const double &Cuc, const double &Cis, const double &Cic, const double &Crs, const double &Crc, const std::bitset< 10 > &dataSource, const double &signalAccuracy, const SvHealth &svHealth, const double &BGD_E1_E5a, const double &BGD_E1_E5b)
	Constructor.

	GalileoEphemeris (GalileoEphemeris &&)=default
	Move constructor.

bool	isHealthy () const final
	Checks whether the signal is healthy.

GalileoEphemeris &	operator= (const GalileoEphemeris &)=delete
	Copy assignment operator.

GalileoEphemeris &	operator= (GalileoEphemeris &&)=delete
	Move assignment operator.

	~GalileoEphemeris () final=default
	Destructor.

Public Member Functions inherited from NAV::SatNavData
SatNavData &	operator= (const SatNavData &)=delete
	Copy assignment operator.

SatNavData &	operator= (SatNavData &&)=delete
	Move assignment operator.

	SatNavData (const SatNavData &)=default
	Copy constructor.

	SatNavData (SatNavData &&)=default
	Move constructor.

	SatNavData (Type type, const InsTime &refTime)
	Constructor.

	~SatNavData () override=default
	Destructor.

Public Member Functions inherited from NAV::Clock
	Clock ()=default
	Default Constructor.

	Clock (Clock &&)=default
	Move constructor.

	Clock (const Clock &)=default
	Copy constructor.

Clock &	operator= (Clock &&)=delete
	Move assignment operator.

Clock &	operator= (const Clock &)=delete
	Copy assignment operator.

virtual	~Clock ()=default
	Destructor.

Public Member Functions inherited from NAV::Orbit
Pos	calcSatellitePos (const InsTime &transTime) const
	Calculates position of the satellite at transmission time.

PosVel	calcSatellitePosVel (const InsTime &transTime) const
	Calculates position and velocity of the satellite at transmission time.

PosVelAccel	calcSatellitePosVelAccel (const InsTime &transTime) const
	Calculates position, velocity and acceleration of the satellite at transmission time.

Orbit &	operator= (const Orbit &)=delete
	Copy assignment operator.

Orbit &	operator= (Orbit &&)=delete
	Move assignment operator.

	Orbit ()=default
	Default Constructor.

	Orbit (const Orbit &)=default
	Copy constructor.

	Orbit (Orbit &&)=default
	Move constructor.

virtual	~Orbit ()=default
	Destructor.

Data Fields
std::array< double, 3 >	a

double	BGD_E1_E5a
	E1-E5a Broadcast Group Delay [s].

double	BGD_E1_E5b
	E1-E5b Broadcast Group Delay [s].

double	Cic
	Amplitude of the cosine harmonic correction term to the angle of inclination [rad].

double	Cis
	Amplitude of the sine harmonic correction term to the angle of inclination [rad].

double	Crc
	Amplitude of the cosine harmonic correction term to the orbit radius [m].

double	Crs
	Amplitude of the sine harmonic correction term to the orbit radius [m].

double	Cuc
	Amplitude of the cosine harmonic correction term to the argument of latitude [rad].

double	Cus
	Amplitude of the sine harmonic correction term to the argument of latitude [rad].

std::bitset< 10 >	dataSource
	Data sources.

double	delta_n
	Mean motion difference from computed value [rad/s].

double	e
	Eccentricity [-].

double	i_0
	Inclination angle at reference time [rad].

double	i_dot
	Rate of change of inclination [rad/s].

size_t	IODnav
	Issue of Data of the nav batch.

double	M_0
	Mean anomaly at reference time [rad].

double	omega
	Argument of perigee [rad].

double	Omega_0
	Longitude of the ascending node at reference time [rad].

double	Omega_dot
	Rate of change of right ascension [rad/s].

double	signalAccuracy

double	sqrt_A
	Square root of the semi-major axis [m^1/2].

SvHealth	svHealth
	Signal Health.

InsTime	toc
	Time of Clock.

InsTime	toe
	Time of Ephemeris.

Data Fields inherited from NAV::SatNavData
InsTime	refTime
	Reference time of the information.

const Type	type
	Child type (for down-casting)

Private Member Functions
PosVelAccel	calcSatelliteData (const InsTime &transTime, Orbit::Calc calc) const final
	Calculates position, velocity and acceleration of the satellite at transmission time.

Additional Inherited Members
Public Types inherited from NAV::SatNavData
enum	Type : uint8_t { GPSEphemeris , GalileoEphemeris , GLONASSEphemeris , BeiDouEphemeris , QZSSEphemeris , IRNSSEphemeris , SBASEphemeris }
	Child type. More...

Protected Types inherited from NAV::Orbit
enum	Calc : uint8_t { Calc_None , Calc_Position , Calc_Velocity , Calc_Acceleration }
	Calculation flags. More...

Detailed Description

Broadcasted ephemeris message data.

Note: See [13] GAL-ICD-2.0, ch. 5., p. 43ff

Description of the GPS satellite orbits

Definition at line 28 of file GalileoEphemeris.hpp.

Constructor & Destructor Documentation

◆ GalileoEphemeris() [1/4]

NAV::GalileoEphemeris::GalileoEphemeris ( const InsTime & toc )

explicit

Default Constructor.

Parameters

[in] toc Time the Clock information is calculated (Time of Clock)

Definition at line 19 of file GalileoEphemeris.cpp.

◆ GalileoEphemeris() [2/4]

NAV::GalileoEphemeris::GalileoEphemeris	(	const InsTime &	toc,
		const InsTime &	toe,
		const size_t &	IODnav,
		const std::array< double, 3 > &	a,
		const double &	sqrt_A,
		const double &	e,
		const double &	i_0,
		const double &	Omega_0,
		const double &	omega,
		const double &	M_0,
		const double &	delta_n,
		const double &	Omega_dot,
		const double &	i_dot,
		const double &	Cus,
		const double &	Cuc,
		const double &	Cis,
		const double &	Cic,
		const double &	Crs,
		const double &	Crc,
		const std::bitset< 10 > &	dataSource,
		const double &	signalAccuracy,
		const SvHealth &	svHealth,
		const double &	BGD_E1_E5a,
		const double &	BGD_E1_E5b )

Constructor.

Parameters

[in]	toc	Time the Clock information is calculated (Time of Clock)
[in]	toe	Time the Orbit information is calculated (Time of Ephemeris)
[in]	IODnav	Issue of Data of the nav batch
[in]	a	Polynomial coefficients for clock correction (a0 bias [s], a1 drift [s/s], a2 drift rate (aging) [s/s^2])
[in]	sqrt_A	Square root of the semi-major axis [m^1/2]
[in]	e	Eccentricity [-]
[in]	i_0	Inclination angle at reference time [rad]
[in]	Omega_0	Longitude of the ascending node at reference time [rad]
[in]	omega	Argument of perigee [rad]
[in]	M_0	Mean anomaly at reference time [rad]
[in]	delta_n	Mean motion difference from computed value [rad/s]
[in]	Omega_dot	Rate of change of right ascension [rad/s]
[in]	i_dot	Rate of change of inclination [rad/s]
[in]	Cus	Amplitude of the sine harmonic correction term to the argument of latitude [rad]
[in]	Cuc	Amplitude of the cosine harmonic correction term to the argument of latitude [rad]
[in]	Cis	Amplitude of the sine harmonic correction term to the angle of inclination [rad]
[in]	Cic	Amplitude of the cosine harmonic correction term to the angle of inclination [rad]
[in]	Crs	Amplitude of the sine harmonic correction term to the orbit radius [m]
[in]	Crc	Amplitude of the cosine harmonic correction term to the orbit radius [m]
[in]	dataSource	Data sources
[in]	signalAccuracy	SISA (Signal in space accuracy) [m]
[in]	svHealth	Signal Health
[in]	BGD_E1_E5a	E1-E5a Broadcast Group Delay [s]
[in]	BGD_E1_E5b	E1-E5b Broadcast Group Delay [s]

Definition at line 22 of file GalileoEphemeris.cpp.

◆ ~GalileoEphemeris()

NAV::GalileoEphemeris::~GalileoEphemeris ( )

finaldefault

Destructor.

◆ GalileoEphemeris() [3/4]

NAV::GalileoEphemeris::GalileoEphemeris ( const GalileoEphemeris & )

default

Copy constructor.

◆ GalileoEphemeris() [4/4]

NAV::GalileoEphemeris::GalileoEphemeris ( GalileoEphemeris && )

default

Move constructor.

Member Function Documentation

◆ calcClockCorrections()

Clock::Corrections NAV::GalileoEphemeris::calcClockCorrections	(	const InsTime &	recvTime,
		double	dist,
		const Frequency &	freq ) const

nodiscardfinalvirtual

Calculates clock bias and drift of the satellite.

Parameters

[in]	recvTime	Receive time of the signal
[in]	dist	Distance between receiver and satellite (normally the pseudorange) [m]
[in]	freq	Signal Frequency

Implements NAV::Clock.

Definition at line 100 of file GalileoEphemeris.cpp.

◆ calcSatelliteData()

Orbit::PosVelAccel NAV::GalileoEphemeris::calcSatelliteData	(	const InsTime &	transTime,
		Orbit::Calc	calc ) const

nodiscardfinalprivatevirtual

Calculates position, velocity and acceleration of the satellite at transmission time.

Parameters

[in]	transTime	Transmit time of the signal
[in]	calc	Flags which determine what should be calculated and returned

Note: See [13] GAL-ICD-2.0, ch. 5.1.1, p. 44f; See [21] IS-GPS-200 ch. 20.3.3.4.3.1 Table 20-IV p.106-109

Implements NAV::Orbit.

Definition at line 174 of file GalileoEphemeris.cpp.

◆ calcSatellitePositionVariance()

double NAV::GalileoEphemeris::calcSatellitePositionVariance ( ) const

nodiscardfinalvirtual

Calculates the Variance of the satellite position in [m^2].

Implements NAV::Orbit.

Definition at line 324 of file GalileoEphemeris.cpp.

◆ isHealthy()

bool NAV::GalileoEphemeris::isHealthy ( ) const

nodiscardfinalvirtual

Checks whether the signal is healthy.

Implements NAV::SatNavData.

Definition at line 314 of file GalileoEphemeris.cpp.

◆ operator=() [1/2]

GalileoEphemeris & NAV::GalileoEphemeris::operator= ( const GalileoEphemeris & )

delete

Copy assignment operator.

◆ operator=() [2/2]

GalileoEphemeris & NAV::GalileoEphemeris::operator= ( GalileoEphemeris && )

delete

Move assignment operator.

Field Documentation

◆ a

std::array<double, 3> NAV::GalileoEphemeris::a

Polynomial coefficients for clock correction

a(0) bias [s]
a(1) drift [s/s]
a(2) drift rate (aging) [s/s^2]

Note: See [13] GAL-ICD-2.0, ch. 5.1.3, p. 46

Definition at line 92 of file GalileoEphemeris.hpp.

◆ BGD_E1_E5a

double NAV::GalileoEphemeris::BGD_E1_E5a

E1-E5a Broadcast Group Delay [s].

Note: See [13] GAL-ICD-2.0, ch. 5.1.5, p. 47f

Definition at line 150 of file GalileoEphemeris.hpp.

◆ BGD_E1_E5b

double NAV::GalileoEphemeris::BGD_E1_E5b

E1-E5b Broadcast Group Delay [s].

Note: See [13] GAL-ICD-2.0, ch. 5.1.5, p. 47f

Definition at line 153 of file GalileoEphemeris.hpp.

◆ Cic

double NAV::GalileoEphemeris::Cic

Amplitude of the cosine harmonic correction term to the angle of inclination [rad].

Definition at line 111 of file GalileoEphemeris.hpp.

◆ Cis

double NAV::GalileoEphemeris::Cis

Amplitude of the sine harmonic correction term to the angle of inclination [rad].

Definition at line 110 of file GalileoEphemeris.hpp.

◆ Crc

double NAV::GalileoEphemeris::Crc

Amplitude of the cosine harmonic correction term to the orbit radius [m].

Definition at line 113 of file GalileoEphemeris.hpp.

◆ Crs

double NAV::GalileoEphemeris::Crs

Amplitude of the sine harmonic correction term to the orbit radius [m].

Definition at line 112 of file GalileoEphemeris.hpp.

◆ Cuc

double NAV::GalileoEphemeris::Cuc

Amplitude of the cosine harmonic correction term to the argument of latitude [rad].

Definition at line 109 of file GalileoEphemeris.hpp.

◆ Cus

double NAV::GalileoEphemeris::Cus

Amplitude of the sine harmonic correction term to the argument of latitude [rad].

Definition at line 108 of file GalileoEphemeris.hpp.

◆ dataSource

std::bitset<10> NAV::GalileoEphemeris::dataSource

Data sources.

Bit 0 set: I/NAV E1-B Bit 1 set: F/NAV E5a-I Bit 2 set: I/NAV E5b-I Bits 0 and 2: Both can be set if the navigation messages were merged, however, bits 0-2 cannot all be set, as the I/NAV and F/NAV messages contain different information Bit 3 reserved for Galileo internal use Bit 4 reserved for Galileo internal use Bit 8 set: af0-af2, Toc, SISA are for E5a,E1 Bit 9 set: af0-af2, Toc, SISA are for E5b,E1 Bits 8-9 : exclusive (only one bit can be set)

Note: See [40] RINEX-3.04, ch. A8, p. A25

Definition at line 131 of file GalileoEphemeris.hpp.

◆ delta_n

double NAV::GalileoEphemeris::delta_n

Mean motion difference from computed value [rad/s].

Definition at line 105 of file GalileoEphemeris.hpp.

◆ e

double NAV::GalileoEphemeris::e

Eccentricity [-].

Definition at line 97 of file GalileoEphemeris.hpp.

◆ i_0

double NAV::GalileoEphemeris::i_0

Inclination angle at reference time [rad].

Definition at line 98 of file GalileoEphemeris.hpp.

◆ i_dot

double NAV::GalileoEphemeris::i_dot

Rate of change of inclination [rad/s].

Definition at line 107 of file GalileoEphemeris.hpp.

◆ IODnav

size_t NAV::GalileoEphemeris::IODnav

Issue of Data of the nav batch.

The navigation data is disseminated in data batches each one identified by an Issue of Data. In nominal operation the navigation data (ephemeris, satellite clock correction and SISA) have limited validity duration depending on the data type. The identification of each batch by an Issue of Data (IOD) value enables:

the users to distinguish the data in different batches received from each satellite
to indicate to the user receiver the validity of the data (which have to be updated using new issue of navigation data)
the user receiver to compute the full batch of data even if it misses some pages or start receiving the data somewhere during the transmission

Note: See [13] GAL-ICD-2.0, ch. 5.1.9.2, p. 51

Definition at line 84 of file GalileoEphemeris.hpp.

◆ M_0

double NAV::GalileoEphemeris::M_0

Mean anomaly at reference time [rad].

Definition at line 101 of file GalileoEphemeris.hpp.

◆ omega

double NAV::GalileoEphemeris::omega

Argument of perigee [rad].

Definition at line 100 of file GalileoEphemeris.hpp.

◆ Omega_0

double NAV::GalileoEphemeris::Omega_0

Longitude of the ascending node at reference time [rad].

Definition at line 99 of file GalileoEphemeris.hpp.

◆ Omega_dot

double NAV::GalileoEphemeris::Omega_dot

Rate of change of right ascension [rad/s].

Definition at line 106 of file GalileoEphemeris.hpp.

◆ signalAccuracy

double NAV::GalileoEphemeris::signalAccuracy

SISA (Signal in space accuracy) [m]

Signal - In - Space Accuracy (SISA) is a prediction of the minimum standard deviation (1-sigma) of the unbiased Gaussian distribution which overbounds the Signal - In - Space Error (SISE) predictable distribution for all possible user locations within the satellite coverage area. When no accurate prediction is available (SISA = NAPA), this is an indicator of a potential anomalous SIS.

Note: See [13] GAL-ICD-2.0, ch. 5.1.12, p.58

Definition at line 142 of file GalileoEphemeris.hpp.

◆ sqrt_A

double NAV::GalileoEphemeris::sqrt_A

Square root of the semi-major axis [m^1/2].

Definition at line 96 of file GalileoEphemeris.hpp.

◆ svHealth

SvHealth NAV::GalileoEphemeris::svHealth

Signal Health.

Note: See [13] GAL-ICD-2.0, ch. 5.1.9.3, p. 52

Definition at line 146 of file GalileoEphemeris.hpp.

◆ toc

InsTime NAV::GalileoEphemeris::toc

Time of Clock.

Definition at line 66 of file GalileoEphemeris.hpp.

◆ toe

InsTime NAV::GalileoEphemeris::toe

Time of Ephemeris.

Definition at line 69 of file GalileoEphemeris.hpp.

The documentation for this class was generated from the following files:

/home/runner/work/INSTINCT/INSTINCT/src/Navigation/GNSS/Satellite/Ephemeris/GalileoEphemeris.hpp
/home/runner/work/INSTINCT/INSTINCT/src/Navigation/GNSS/Satellite/Ephemeris/GalileoEphemeris.cpp

Data Structures

Public Member Functions

Data Fields

Private Member Functions

Additional Inherited Members

Detailed Description

Constructor & Destructor Documentation

◆ GalileoEphemeris() [1/4]

◆ GalileoEphemeris() [2/4]

◆ ~GalileoEphemeris()

◆ GalileoEphemeris() [3/4]

◆ GalileoEphemeris() [4/4]

Member Function Documentation

◆ calcClockCorrections()

◆ calcSatelliteData()

◆ calcSatellitePositionVariance()

◆ isHealthy()

◆ operator=() [1/2]

◆ operator=() [2/2]

Field Documentation

◆ a

◆ BGD_E1_E5a

◆ BGD_E1_E5b

◆ Cic

◆ Cis

◆ Crc

◆ Crs

◆ Cuc

◆ Cus

◆ dataSource

◆ delta_n

◆ e

◆ i_0

◆ i_dot

◆ IODnav

◆ M_0

◆ omega

◆ Omega_0

◆ Omega_dot

◆ signalAccuracy

◆ sqrt_A

◆ svHealth

◆ toc

◆ toe