libsbp
v2.4.7
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#include <observation.h>
Data Fields | |
almanac_common_content_t | common |
Values common for all almanac types. 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 | af0 |
Polynomial clock correction coefficient (clock bias) [s]. More... | |
double | af1 |
Polynomial clock correction coefficient (clock drift) [s/s]. More... | |
Definition at line 974 of file observation.h.
double af0 |
Polynomial clock correction coefficient (clock bias) [s].
Definition at line 983 of file observation.h.
double af1 |
Polynomial clock correction coefficient (clock drift) [s/s].
Definition at line 984 of file observation.h.
almanac_common_content_t common |
Values common for all almanac types.
Definition at line 975 of file observation.h.
double ecc |
Eccentricity of satellite orbit.
Definition at line 977 of file observation.h.
double inc |
Inclination [rad].
Definition at line 982 of file observation.h.
double m0 |
Mean anomaly at reference time [rad].
Definition at line 976 of file observation.h.
double omega0 |
Longitude of ascending node of orbit plane at weekly epoch [rad].
Definition at line 979 of file observation.h.
double omegadot |
Rate of right ascension [rad/s].
Definition at line 980 of file observation.h.
double sqrta |
Square root of the semi-major axis of orbit [m^(1/2)].
Definition at line 978 of file observation.h.
double w |
Argument of perigee [rad].
Definition at line 981 of file observation.h.