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libsbp
v2.4.7
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libsbp
v2.4.7
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#include <observation.h>
Data Fields | |
| double | tgd |
| Group delay differential between L1 and L2 [s]. More... | |
| double | c_rs |
| Amplitude of the sine harmonic correction term to the orbit radius [m]. More... | |
| double | c_rc |
| Amplitude of the cosine harmonic correction term to the orbit radius [m]. More... | |
| double | c_uc |
| Amplitude of the cosine harmonic correction term to the argument of latitude [rad]. More... | |
| double | c_us |
| Amplitude of the sine harmonic correction term to the argument of latitude [rad]. More... | |
| double | c_ic |
| Amplitude of the cosine harmonic correction term to the angle of inclination [rad]. More... | |
| double | c_is |
| Amplitude of the sine harmonic correction term to the angle of inclination [rad]. More... | |
| double | dn |
| Mean motion difference [rad/s]. More... | |
| double | m0 |
| Mean anomaly at reference time [rad]. More... | |
| double | ecc |
| Eccentricity of satellite orbit. More... | |
| double | sqrta |
| Square root of the semi-major axis of orbit [m^(1/2)]. More... | |
| double | omega0 |
| Longitude of ascending node of orbit plane at weekly epoch [rad]. More... | |
| double | omegadot |
| Rate of right ascension [rad/s]. More... | |
| double | w |
| Argument of perigee [rad]. More... | |
| double | inc |
| Inclination [rad]. More... | |
| double | inc_dot |
| Inclination first derivative [rad/s]. More... | |
| double | af0 |
| Polynomial clock correction coefficient (clock bias) [s]. More... | |
| double | af1 |
| Polynomial clock correction coefficient (clock drift) [s/s]. More... | |
| double | af2 |
| Polynomial clock correction coefficient (rate of clock drift) [s/s^2]. More... | |
| double | toe_tow |
| Time of week [s]. More... | |
| u16 | toe_wn |
| Week number [week]. More... | |
| double | toc_tow |
| Clock reference time of week [s]. More... | |
| u16 | toc_wn |
| Clock reference week number [week]. More... | |
| u8 | valid |
| Is valid? More... | |
| u8 | healthy |
| Satellite is healthy? More... | |
| u8 | prn |
| PRN being tracked. More... | |
| u8 | iode |
| Issue of ephemeris data. More... | |
Definition at line 578 of file observation.h.
| double af0 |
Polynomial clock correction coefficient (clock bias) [s].
Definition at line 595 of file observation.h.
| double af1 |
Polynomial clock correction coefficient (clock drift) [s/s].
Definition at line 596 of file observation.h.
| double af2 |
Polynomial clock correction coefficient (rate of clock drift) [s/s^2].
Definition at line 597 of file observation.h.
| double c_ic |
Amplitude of the cosine harmonic correction term to the angle of inclination [rad].
Definition at line 584 of file observation.h.
| double c_is |
Amplitude of the sine harmonic correction term to the angle of inclination [rad].
Definition at line 585 of file observation.h.
| double c_rc |
Amplitude of the cosine harmonic correction term to the orbit radius [m].
Definition at line 581 of file observation.h.
| double c_rs |
Amplitude of the sine harmonic correction term to the orbit radius [m].
Definition at line 580 of file observation.h.
| double c_uc |
Amplitude of the cosine harmonic correction term to the argument of latitude [rad].
Definition at line 582 of file observation.h.
| double c_us |
Amplitude of the sine harmonic correction term to the argument of latitude [rad].
Definition at line 583 of file observation.h.
| double dn |
Mean motion difference [rad/s].
Definition at line 586 of file observation.h.
| double ecc |
Eccentricity of satellite orbit.
Definition at line 588 of file observation.h.
| u8 healthy |
Satellite is healthy?
Definition at line 603 of file observation.h.
| double inc |
Inclination [rad].
Definition at line 593 of file observation.h.
| double inc_dot |
Inclination first derivative [rad/s].
Definition at line 594 of file observation.h.
| u8 iode |
Issue of ephemeris data.
Definition at line 605 of file observation.h.
| double m0 |
Mean anomaly at reference time [rad].
Definition at line 587 of file observation.h.
| double omega0 |
Longitude of ascending node of orbit plane at weekly epoch [rad].
Definition at line 590 of file observation.h.
| double omegadot |
Rate of right ascension [rad/s].
Definition at line 591 of file observation.h.
| u8 prn |
PRN being tracked.
Definition at line 604 of file observation.h.
| double sqrta |
Square root of the semi-major axis of orbit [m^(1/2)].
Definition at line 589 of file observation.h.
| double tgd |
Group delay differential between L1 and L2 [s].
Definition at line 579 of file observation.h.
| double toc_tow |
Clock reference time of week [s].
Definition at line 600 of file observation.h.
| u16 toc_wn |
Clock reference week number [week].
Definition at line 601 of file observation.h.
| double toe_tow |
Time of week [s].
Definition at line 598 of file observation.h.
| u16 toe_wn |
Week number [week].
Definition at line 599 of file observation.h.
| u8 valid |
Is valid?
Definition at line 602 of file observation.h.
| double w |
Argument of perigee [rad].
Definition at line 592 of file observation.h.
1.8.9.1 
