Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
Extra choice modes for getExtraData. More...
Variables | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_NO_RESULTS = 0 |
To calculate no extra results. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION = 1 |
To calculate the geolocation data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_D = 2 |
To calculate the geolocation rate data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_2D = 4 |
To calculate the geolocation rate rate data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_EXTRA = 8 |
To calculate the geolocation extra data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_D = 16 |
To calculate the earth-fixed velocity data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_2D = 32 |
To calculate the earth-fixed acceleration data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_SUN = 64 |
To calculate the sun data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_MOON = 128 |
To calculate the moon data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_OSCULATING_KEPLER = 256 |
To calculate the osculating Kepler data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_INERTIAL_AUX = 512 |
To calculate the inertial auxiliary data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_ANX_TIMING = 1024 |
To calculate ANX timing data set. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPLER = 2048 |
To calculate the mean keplerian elements. | |
static long | EECFI::EnumOrbit.XOCFI_ORBIT_EXTRA_ALL_RESULTS = 4095 |
To calculate all extra results. |
Extra choice modes for getExtraData.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_ALL_RESULTS = 4095 [static, inherited] |
To calculate all extra results.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_ANX_TIMING = 1024 [static, inherited] |
To calculate ANX timing data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEP_MEAN_KEPLER = 2048 [static, inherited] |
To calculate the mean keplerian elements.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_2D = 32 [static, inherited] |
To calculate the earth-fixed acceleration data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_FIXED_D = 16 [static, inherited] |
To calculate the earth-fixed velocity data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION = 1 [static, inherited] |
To calculate the geolocation data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_2D = 4 [static, inherited] |
To calculate the geolocation rate rate data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_D = 2 [static, inherited] |
To calculate the geolocation rate data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOLOCATION_EXTRA = 8 [static, inherited] |
To calculate the geolocation extra data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_INERTIAL_AUX = 512 [static, inherited] |
To calculate the inertial auxiliary data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MOON = 128 [static, inherited] |
To calculate the moon data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_NO_RESULTS = 0 [static, inherited] |
To calculate no extra results.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSCULATING_KEPLER = 256 [static, inherited] |
To calculate the osculating Kepler data set.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_SUN = 64 [static, inherited] |
To calculate the sun data set.