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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 | |
| ephemeris_common_content_t | common |
| Values common for all ephemeris types. More... | |
| float | tgd1 |
| Group delay differential for B1 [s]. More... | |
| float | tgd2 |
| Group delay differential for B2 [s]. More... | |
| float | c_rs |
| Amplitude of the sine harmonic correction term to the orbit radius [m]. More... | |
| float | c_rc |
| Amplitude of the cosine harmonic correction term to the orbit radius [m]. More... | |
| float | c_uc |
| Amplitude of the cosine harmonic correction term to the argument of latitude [rad]. More... | |
| float | c_us |
| Amplitude of the sine harmonic correction term to the argument of latitude [rad]. More... | |
| float | c_ic |
| Amplitude of the cosine harmonic correction term to the angle of inclination [rad]. More... | |
| float | 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... | |
| float | af1 |
| Polynomial clock correction coefficient (clock drift) [s/s]. More... | |
| float | af2 |
| Polynomial clock correction coefficient (rate of clock drift) [s/s^2]. More... | |
| gps_time_sec_t | toc |
| Clock reference. More... | |
| u8 | iode |
| Issue of ephemeris data. More... | |
| u16 | iodc |
| Issue of clock data. More... | |
Definition at line 294 of file observation.h.
| double af0 |
Polynomial clock correction coefficient (clock bias) [s].
Definition at line 313 of file observation.h.
| float af1 |
Polynomial clock correction coefficient (clock drift) [s/s].
Definition at line 314 of file observation.h.
| float af2 |
Polynomial clock correction coefficient (rate of clock drift) [s/s^2].
Definition at line 315 of file observation.h.
| float c_ic |
Amplitude of the cosine harmonic correction term to the angle of inclination [rad].
Definition at line 302 of file observation.h.
| float c_is |
Amplitude of the sine harmonic correction term to the angle of inclination [rad].
Definition at line 303 of file observation.h.
| float c_rc |
Amplitude of the cosine harmonic correction term to the orbit radius [m].
Definition at line 299 of file observation.h.
| float c_rs |
Amplitude of the sine harmonic correction term to the orbit radius [m].
Definition at line 298 of file observation.h.
| float c_uc |
Amplitude of the cosine harmonic correction term to the argument of latitude [rad].
Definition at line 300 of file observation.h.
| float c_us |
Amplitude of the sine harmonic correction term to the argument of latitude [rad].
Definition at line 301 of file observation.h.
| ephemeris_common_content_t common |
Values common for all ephemeris types.
Definition at line 295 of file observation.h.
| double dn |
Mean motion difference [rad/s].
Definition at line 304 of file observation.h.
| double ecc |
Eccentricity of satellite orbit.
Definition at line 306 of file observation.h.
| double inc |
Inclination [rad].
Definition at line 311 of file observation.h.
| double inc_dot |
Inclination first derivative [rad/s].
Definition at line 312 of file observation.h.
| u16 iodc |
Issue of clock data.
Definition at line 318 of file observation.h.
| u8 iode |
Issue of ephemeris data.
Definition at line 317 of file observation.h.
| double m0 |
Mean anomaly at reference time [rad].
Definition at line 305 of file observation.h.
| double omega0 |
Longitude of ascending node of orbit plane at weekly epoch [rad].
Definition at line 308 of file observation.h.
| double omegadot |
Rate of right ascension [rad/s].
Definition at line 309 of file observation.h.
| double sqrta |
Square root of the semi-major axis of orbit [m^(1/2)].
Definition at line 307 of file observation.h.
| float tgd1 |
Group delay differential for B1 [s].
Definition at line 296 of file observation.h.
| float tgd2 |
Group delay differential for B2 [s].
Definition at line 297 of file observation.h.
| gps_time_sec_t toc |
Clock reference.
Definition at line 316 of file observation.h.
| double w |
Argument of perigee [rad].
Definition at line 310 of file observation.h.
1.8.9.1 
