Data structure for the GPS model.
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#include <sc_orbit.h>
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double | tc |
| | Satellite clock reference epoch.
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double | a0 |
| | Satellite clock offset.
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double | a1 |
| | Satellite clock drift.
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double | a2 |
| | Satellite clock frequency drift.
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double | te |
| | Ephemerides reference epoch.
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double | t0 |
| | Sidereal time reference epoch.
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double | ecc |
| | Eccentricity.
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double | sqrt_ax |
| | Square root of semi-major axis.
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double | m0 |
| | Mean anomaly at reference epoch [rad].
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double | w0 |
| | Argument of perigee [rad].
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double | i0 |
| | Inclination [rad].
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double | l0 |
| | Longitude of the node at the weekly epoch [rad].
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double | delta_n |
| | Mean motion difference.
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double | i_dot |
| | Rate of inclination angle [rad/s].
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double | omega_dot |
| | Rate of note's right ascension.
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double | cuc |
| | Correction coefficient (argument of perigee).
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double | cus |
| | Correction coefficient (argument of perigee).
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double | crc |
| | Correction coefficient (radius).
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double | crs |
| | Correction coefficient (radius).
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double | cic |
| | Correction coefficient (inclination).
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double | cis |
| | Correction coefficient (inclination).
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double | ta |
| | Ephemerides reference epoch.
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double | w |
| | Argument of perigee (semicircles).
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double | delta_inc |
| | Inclination delta (semicircles).
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double | dm_plane |
| | Right ascension of the ascending node [rad].
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int | satellite |
| | GPS satellite index.
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bool | broadcast_ephem |
| | Whether or not the ephemerides are broadcast.
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Data structure for the GPS model.
