0.2.0
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Broadcasted ephemeris message data. 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]. | |
GLONASSEphemeris (const GLONASSEphemeris &)=default | |
Copy constructor. | |
GLONASSEphemeris (const InsTime &toc, double tau_c, double tau_n, double gamma_n, bool health, Eigen::Vector3d pos, Eigen::Vector3d vel, Eigen::Vector3d accelLuniSolar, int8_t frequencyNumber) | |
Constructor. | |
GLONASSEphemeris (GLONASSEphemeris &&)=default | |
Move constructor. | |
bool | isHealthy () const final |
Checks whether the signal is healthy. | |
GLONASSEphemeris & | operator= (const GLONASSEphemeris &)=delete |
Copy assignment operator. | |
GLONASSEphemeris & | operator= (GLONASSEphemeris &&)=delete |
Move assignment operator. | |
~GLONASSEphemeris () 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. | |
Public Attributes | |
const int8_t | frequencyNumber |
Frequency number (-7 ... +13) (-7 ...+6 (ICD 5.1)) | |
const double | gamma_n |
SV relative frequency bias. | |
const bool | health |
Health. | |
const Eigen::Vector3d | PZ90_accelLuniSolar |
Accelerations due to lunar-solar gravitational perturbation in PZ90 frame [m/s^2]. | |
const Eigen::Vector3d | PZ90_pos |
Position at reference time in PZ90 frame [m]. | |
const Eigen::Vector3d | PZ90_vel |
Velocity at reference time in PZ90 frame [m/s]. | |
const double | tau_c |
Coefficient of linear polynomial of time system difference [s]. | |
const double | tau_n |
SV clock bias [s]. | |
const InsTime | toc |
Toe Time of clock [s] (Reference time, ephemeris parameters) | |
Public Attributes inherited from NAV::SatNavData | |
InsTime | refTime |
Reference time of the information. | |
const Type | type |
Child type (for down-casting) | |
Additional Inherited Members | |
Public Types inherited from NAV::SatNavData | |
enum | Type { GPSEphemeris , GalileoEphemeris , GLONASSEphemeris , BeiDouEphemeris , QZSSEphemeris , IRNSSEphemeris , SBASEphemeris } |
Child type. More... | |
Protected Types inherited from NAV::Orbit | |
enum | Calc { Calc_None , Calc_Position , Calc_Velocity , Calc_Acceleration } |
Calculation flags. More... | |
Broadcasted ephemeris message data.
NAV::GLONASSEphemeris::GLONASSEphemeris | ( | const InsTime & | toc, |
double | tau_c, | ||
double | tau_n, | ||
double | gamma_n, | ||
bool | health, | ||
Eigen::Vector3d | pos, | ||
Eigen::Vector3d | vel, | ||
Eigen::Vector3d | accelLuniSolar, | ||
int8_t | frequencyNumber ) |
Constructor.
[in] | toc | Time the Clock information is calculated (Time of Clock) |
[in] | tau_c | Coefficient of linear polynomial of time system difference [s] |
[in] | tau_n | SV clock bias [s] |
[in] | gamma_n | SV relative frequency bias |
[in] | health | Health flag |
[in] | pos | Position at reference time in PZ90 frame [m] |
[in] | vel | Velocity at reference time in PZ90 frame [m/s] |
[in] | accelLuniSolar | Accelerations due to lunar-solar gravitational perturbation in PZ90 frame [m/s^2] |
[in] | frequencyNumber | Frequency number (-7 ... +13) (-7 ...+6 (ICD 5.1)) |
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finalvirtual |
Calculates clock bias and drift of the satellite.
[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.