Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |
Extra data model independent result vector. More...
Extra data model independent result vector.
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_AZ_ACC = 19 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_AZ_VEL = 15 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_DEC_SAT = 42 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EARTH_ROTATION_ANGLE = 43 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EAST_ACC = 17 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_EAST_VEL = 13 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOC_LONG = 0 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOC_LONG_2D = 6 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOC_LONG_D = 3 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOD_ALT = 2 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOD_ALT_2D = 8 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOD_ALT_D = 5 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOD_LAT = 1 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOD_LAT_2D = 7 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GEOD_LAT_D = 4 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_GROUNDTRACK_ACC = 18 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MAG_VEL = 14 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MLST = 22 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MOON_AREA_LIT = 30 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MOON_DEC = 28 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MOON_RA = 27 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_MOON_SEMI_DIAM = 29 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_NORTH_ACC = 16 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_NORTH_VEL = 12 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_NUM_INDEP_ELEMENTS = 49 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_ORB_VEL_MAG = 40 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_ORBIT_RAD = 37 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_KEPL_A = 31 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_KEPL_E = 32 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_KEPL_I = 33 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_KEPL_M = 36 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_KEPL_RA = 34 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_KEPL_W = 35 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_TRUE_LAT = 46 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_TRUE_LAT_2D = 48 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_OSC_TRUE_LAT_D = 47 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RA_SAT = 41 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RA_SAT_2D = 45 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RA_SAT_D = 44 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RAD_CUR_ALONG_GROUNDTRACK = 11 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RAD_CUR_ORTHO_MERIDIAN = 10 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RAD_CUR_PARALLEL_MERIDIAN = 9 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_RADIAL_ORB_VEL = 38 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_SAT_ECLIPSE_FLAG = 20 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_SZA = 21 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_TLST = 23 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_TRANS_ORB_VEL = 39 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_TRUE_SUN_DEC = 25 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_TRUE_SUN_RA = 24 [static, inherited] |
long EECFI.EnumOrbit.XOCFI_ORBIT_EXTRA_TRUE_SUN_SEMIDIAM = 26 [static, inherited] |