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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 | tgd |
| Group delay differential between L1 and L2 [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... | |
| float | 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 259 of file observation.h.
| float af0 |
Polynomial clock correction coefficient (clock bias) [s].
Definition at line 277 of file observation.h.
| float af1 |
Polynomial clock correction coefficient (clock drift) [s/s].
Definition at line 278 of file observation.h.
| float af2 |
Polynomial clock correction coefficient (rate of clock drift) [s/s^2].
Definition at line 279 of file observation.h.
| float c_ic |
Amplitude of the cosine harmonic correction term to the angle of inclination [rad].
Definition at line 266 of file observation.h.
| float c_is |
Amplitude of the sine harmonic correction term to the angle of inclination [rad].
Definition at line 267 of file observation.h.
| float c_rc |
Amplitude of the cosine harmonic correction term to the orbit radius [m].
Definition at line 263 of file observation.h.
| float c_rs |
Amplitude of the sine harmonic correction term to the orbit radius [m].
Definition at line 262 of file observation.h.
| float c_uc |
Amplitude of the cosine harmonic correction term to the argument of latitude [rad].
Definition at line 264 of file observation.h.
| float c_us |
Amplitude of the sine harmonic correction term to the argument of latitude [rad].
Definition at line 265 of file observation.h.
| ephemeris_common_content_t common |
Values common for all ephemeris types.
Definition at line 260 of file observation.h.
| double dn |
Mean motion difference [rad/s].
Definition at line 268 of file observation.h.
| double ecc |
Eccentricity of satellite orbit.
Definition at line 270 of file observation.h.
| double inc |
Inclination [rad].
Definition at line 275 of file observation.h.
| double inc_dot |
Inclination first derivative [rad/s].
Definition at line 276 of file observation.h.
| u16 iodc |
Issue of clock data.
Definition at line 282 of file observation.h.
| u8 iode |
Issue of ephemeris data.
Definition at line 281 of file observation.h.
| double m0 |
Mean anomaly at reference time [rad].
Definition at line 269 of file observation.h.
| double omega0 |
Longitude of ascending node of orbit plane at weekly epoch [rad].
Definition at line 272 of file observation.h.
| double omegadot |
Rate of right ascension [rad/s].
Definition at line 273 of file observation.h.
| double sqrta |
Square root of the semi-major axis of orbit [m^(1/2)].
Definition at line 271 of file observation.h.
| float tgd |
Group delay differential between L1 and L2 [s].
Definition at line 261 of file observation.h.
| gps_time_sec_t toc |
Clock reference.
Definition at line 280 of file observation.h.
| double w |
Argument of perigee [rad].
Definition at line 274 of file observation.h.