Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
Propagation models. More...
Variables | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_NOT_INITIALIZED = -1 |
Propagator not initialized. | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_MEAN_KEPL = 0 |
Propagation using Mean Keplerian OSV model. | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_SPOT = 1 |
Propagation using Spot model. | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_TLE = 2 |
Propagation using TLE model. | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_PRECISE = 3 |
Propagation using COWELL propagator. | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_GEO = 4 |
Propagation for geostationary satellites (ANR-353). | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_AUTO = 10 |
Propagation using Auto initialization model. | |
static long | EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_DOUBLE = 100 |
Propagation using double initialization model. |
Propagation models.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_AUTO = 10 [static, inherited] |
Propagation using Auto initialization model.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_DOUBLE = 100 [static, inherited] |
Propagation using double initialization model.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_GEO = 4 [static, inherited] |
Propagation for geostationary satellites (ANR-353).
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_MEAN_KEPL = 0 [static, inherited] |
Propagation using Mean Keplerian OSV model.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_NOT_INITIALIZED = -1 [static, inherited] |
Propagator not initialized.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_PRECISE = 3 [static, inherited] |
Propagation using COWELL propagator.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_SPOT = 1 [static, inherited] |
Propagation using Spot model.
long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_TLE = 2 [static, inherited] |
Propagation using TLE model.