static int compute_new_state_vect( const tle_t *tle, double *state_vect, const int ephem) { double sat_params[N_SAT_PARAMS]; int rval = 0; switch( ephem) { case 0: SGP_init( sat_params, tle); rval = SGP( 0., tle, sat_params, state_vect, state_vect + 3); break; case 1: SGP4_init( sat_params, tle); rval = SGP4( 0., tle, sat_params, state_vect, state_vect + 3); break; case 2: SGP8_init( sat_params, tle); rval = SGP8( 0., tle, sat_params, state_vect, state_vect + 3); break; case 3: SDP4_init( sat_params, tle); rval = SDP4( 0., tle, sat_params, state_vect, state_vect + 3); break; case 4: SDP8_init( sat_params, tle); rval = SDP8( 0., tle, sat_params, state_vect, state_vect + 3); break; default: printf( "??? ephem = %d\n", ephem); rval = -99; break; } // if( rval) // printf( "??? rval = %d; ecc = %.6lf\n", rval, tle->eo); return( rval); }
/* Main program */ int main( const int argc, const char **argv) { const char *tle_filename = ((argc == 1) ? "test.tle" : argv[1]); FILE *ifile = fopen( tle_filename, "rb"); tle_t tle; /* Pointer to two-line elements set for satellite */ char line1[100], line2[100]; int ephem = 1; /* default to SGP4 */ int i; /* Index for loops etc */ int n_failures = 0, n_simple = 0, n_simplex = 0; bool failures_only = false; for( i = 2; i < argc; i++) if( argv[i][0] == '-') switch( argv[i][1]) { case 'f': failures_only = true; break; case 'v': verbose = 1; break; case 'd': dist_offset = atof( argv[i] + 2); break; case 's': vel_offset = atof( argv[i] + 2); break; default: printf( "Option '%s' unrecognized\n", argv[i]); break; } if( !ifile) { printf( "Couldn't open input TLE file %s\n", tle_filename); exit( -1); } *line1 = '\0'; while( fgets( line2, sizeof( line2), ifile)) { int got_data = 0; double state_vect[6]; set_tle_defaults( &tle); if( strlen( line2) > 110 && line2[7] == '.' && line2[18] == '.' && line2[0] == '2' && line2[1] == '4') { got_data = 3; /* Find_Orb state vector ephemeris */ tle.epoch = atof( line2); sscanf( line2 + 13, "%lf %lf %lf %lf %lf %lf", state_vect + 0, state_vect + 1, state_vect + 2, state_vect + 3, state_vect + 4, state_vect + 5); } else if( strlen( line1) > 55 && !memcmp( line1 + 50, " (TDB)", 6)) { /* JPL Horizons vector */ const double obliq_2000 = 23.4392911 * PI / 180.; tle.epoch = atof( line1); /* get JD epoch from header... */ strcpy( line1, line2); if( fgets( line2, sizeof( line2), ifile)) got_data = 1; sscanf( line1, "%lf %lf %lf", state_vect + 0, state_vect + 1, state_vect + 2); sscanf( line2, "%lf %lf %lf", state_vect + 3, state_vect + 4, state_vect + 5); /* Cvt ecliptic to equatorial 2000: */ rotate_vector( state_vect , obliq_2000, 0); rotate_vector( state_vect + 3, obliq_2000, 0); } else if( parse_elements( line1, line2, &tle) >= 0) got_data = 2; if( got_data == 1 || got_data == 3) tle.epoch -= 68.00 / 86400.; /* rough convert TDT to UTC */ if( got_data) /* hey! we got a TLE! */ { double sat_params[N_SAT_PARAMS], trial_state[6]; int simple_rval; bool failed = false; tle_t new_tle; if( got_data == 1 || got_data == 3) { ephem = 3; /* Use SDP4 for JPL Horizons vectors */ for( i = 0; i < 6 && fabs( state_vect[i]) < 1.; i++) ; if( i == 6) /* all small quantities, must be in AU & AU/day : */ { for( i = 0; i < 6; i++) state_vect[i] *= AU_IN_KM; for( i = 3; i < 6; i++) state_vect[i] /= seconds_per_day; } for( i = 3; i < 6; i++) /* cvt km/sec to km/min */ state_vect[i] *= seconds_per_minute; if( !failures_only) show_results( "Before:", NULL, state_vect); } else { int is_deep = select_ephemeris( &tle); if( is_deep && (ephem == 1 || ephem == 2)) ephem += 2; /* switch to an SDx */ if( !is_deep && (ephem == 3 || ephem == 4)) ephem -= 2; /* switch to an SGx */ /* Calling of NORAD routines */ /* Each NORAD routine (SGP, SGP4, SGP8, SDP4, SDP8) */ /* will be called in turn with the appropriate TLE set */ switch( ephem) { case 0: SGP_init( sat_params, &tle); SGP( 0., &tle, sat_params, state_vect, state_vect + 3); break; case 1: SGP4_init( sat_params, &tle); SGP4( 0., &tle, sat_params, state_vect, state_vect + 3); break; case 2: SGP8_init( sat_params, &tle); SGP8( 0., &tle, sat_params, state_vect, state_vect + 3); break; case 3: SDP4_init( sat_params, &tle); SDP4( 0., &tle, sat_params, state_vect, state_vect + 3); break; case 4: SDP8_init( sat_params, &tle); SDP8( 0., &tle, sat_params, state_vect, state_vect + 3); break; } if( !failures_only) show_results( "Before:", &tle, state_vect); } new_tle = tle; simple_rval = compute_tle_from_state_vector( &new_tle, state_vect, ephem, trial_state); if( simple_rval) { n_simplex++; find_tle_via_simplex_method( &new_tle, state_vect, trial_state, ephem); } else n_simple++; compute_new_state_vect( &new_tle, trial_state, ephem); for( i = 0; i < 6; i++) { trial_state[i] -= state_vect[i]; if( fabs( trial_state[i]) > 1e-6) failed = true; } if( failed && failures_only) show_results( "Before:", &tle, state_vect); if( failed || !failures_only) show_results( (simple_rval ? "Simplex result:" : "Simplest method:"), &new_tle, trial_state); if( failed) n_failures++; } strcpy( line1, line2); } fclose( ifile); printf( "%d solved with simple method; %d with simplex\n", n_simple, n_simplex); if( n_failures) printf( "%d failures\n", n_failures); return(0); } /* End of main() */
int main( const int argc, const char **argv) { const char *tle_file_name = "ALL_TLE.TXT"; FILE *ifile = fopen( argv[1], "rb"), *tle_file; FILE *stations; char line1[100], line2[100], buff[90]; double search_radius = .2; /* default to .2-degree search */ double lon = 0., rho_sin_phi = 0., rho_cos_phi = 0.; char curr_mpc_code[4]; int i, debug_level = 0, show_non_mpc_report_lines = 0; char prev_obj[20]; double prev_jd = 0., prev_ra = 0., prev_dec = 0.; if( argc == 1) error_exit( -2); if( !ifile) { printf( "Couldn't open input file %s\n", argv[1]); exit( -1); } stations = fopen( "ObsCodes.html", "rb"); if( !stations) /* perhaps stored with truncated extension? */ stations = fopen( "ObsCodes.htm", "rb"); if( !stations) /* Or as a text file? */ stations = fopen( "stations.txt", "rb"); if( !stations) { printf( "Failed to find MPC station list 'ObsCodes.html'\n"); printf( "This can be downloaded at:\n\n"); printf( "http://www.minorplanetcenter.org/iau/lists/ObsCodes.html\n"); exit( -1); } curr_mpc_code[0] = curr_mpc_code[3] = '\0'; for( i = 1; i < argc; i++) if( argv[i][0] == '-') switch( argv[i][1]) { case 'r': search_radius = atof( argv[i] + 2); break; case 't': tle_file_name = argv[i] + 2; break; break; case 'd': debug_level = atoi( argv[i] + 2); break; case 'a': show_non_mpc_report_lines = 1; break; default: printf( "Unrecognized command-line option '%s'\n", argv[i]); exit( -2); break; } tle_file = fopen( tle_file_name, "rb"); if( !tle_file) { printf( "Couldn't open TLE file %s\n", tle_file_name); exit( -1); } *prev_obj = '\0'; while( fgets( buff, sizeof( buff), ifile)) { double target_ra, target_dec, jd; if( !get_mpc_data( buff, &jd, &target_ra, &target_dec)) { char preceding_line[80], line0[100]; double observer_loc[3], observer_loc2[3]; printf( "\n%s", buff); if( !memcmp( prev_obj, buff, 12) && fabs( jd - prev_jd) < .3) { double motion, posn_ang; if( !compute_motion( jd - prev_jd, (target_ra - prev_ra) * cos( (prev_dec + target_dec) / 2.), (target_dec - prev_dec), &motion, &posn_ang)) printf( " Object motion is %.3lf'/sec at PA %.1lf\n", motion, posn_ang); } memcpy( prev_obj, buff, 12); prev_ra = target_ra; prev_dec = target_dec; prev_jd = jd; if( memcmp( curr_mpc_code, buff + 77, 3)) { char tbuff[100]; int got_it = 0; memcpy( curr_mpc_code, buff + 77, 3); fseek( stations, 0L, SEEK_SET); while( !got_it && fgets( tbuff, sizeof( tbuff), stations)) got_it = !memcmp( tbuff, curr_mpc_code, 3); if( got_it) sscanf( tbuff + 3, "%lf %lf %lf", &lon, &rho_cos_phi, &rho_sin_phi); if( !got_it) printf( "FAILED to find MPC code %s\n", curr_mpc_code); } if( debug_level) printf( "lon = %.5lf rho cos phi = %.5lf rho sin phi = %.5lf\n", lon, rho_cos_phi, rho_sin_phi); observer_cartesian_coords( jd, lon * PI / 180., rho_cos_phi, rho_sin_phi, observer_loc); observer_cartesian_coords( jd + TIME_EPSILON, lon * PI / 180., rho_cos_phi, rho_sin_phi, observer_loc2); fseek( tle_file, 0L, SEEK_SET); *line0 = '\0'; if( fgets( line1, sizeof( line1), tle_file)) while( fgets( line2, sizeof( line2), tle_file)) { tle_t tle; /* Structure for two-line elements set for satellite */ if( parse_elements( line1, line2, &tle) >= 0) { /* hey! we got a TLE! */ int is_deep = select_ephemeris( &tle); double sat_params[N_SAT_PARAMS], radius, d_ra, d_dec; double ra, dec, dist_to_satellite, t_since; double pos[3]; /* Satellite position vector */ double unused_delta2; if( debug_level > 1) printf( "%s", line1); t_since = (jd - tle.epoch) * 1440.; if( is_deep) { SDP4_init( sat_params, &tle); SDP4( t_since, &tle, sat_params, pos, NULL); } else { SGP4_init( sat_params, &tle); SGP4( t_since, &tle, sat_params, pos, NULL); } if( debug_level > 1) printf( "%s", line2); if( debug_level > 2) printf( " %.5lf %.5lf %.5lf\n", pos[0], pos[1], pos[2]); get_satellite_ra_dec_delta( observer_loc, pos, &ra, &dec, &dist_to_satellite); if( debug_level > 3) printf( "RA: %.5lf dec: %.5lf\n", ra * 180. / PI, dec * 180. / PI); epoch_of_date_to_j2000( jd, &ra, &dec); d_ra = (ra - target_ra + PI * 4.); while( d_ra > PI) d_ra -= PI + PI; d_dec = dec - target_dec; radius = sqrt( d_ra * d_ra + d_dec * d_dec) * 180. / PI; if( radius < search_radius) /* good enough for us! */ { double arcmin_per_sec, posn_ang; /* Compute position one second later, so we */ /* can show speed/PA of motion: */ t_since += TIME_EPSILON * 1440.; if( is_deep) SDP4( t_since, &tle, sat_params, pos, NULL); else SGP4( t_since, &tle, sat_params, pos, NULL); get_satellite_ra_dec_delta( observer_loc2, pos, &d_ra, &d_dec, &unused_delta2); epoch_of_date_to_j2000( jd, &d_ra, &d_dec); d_ra -= ra; d_dec -= dec; while( d_ra > PI) d_ra -= PI + PI; while( d_ra < -PI) d_ra += PI + PI; /* Put RA into 0 to 2pi range: */ if( !compute_motion( TIME_EPSILON, d_ra * cos( dec), d_dec, &arcmin_per_sec, &posn_ang)) { line1[8] = line1[16] = '\0'; memcpy( line1 + 30, line1 + 11, 6); line1[11] = '\0'; printf( " %s = %s%s-%s", line1 + 2, (line1[9] >= '6' ? "19" : "20"), line1 + 9, line1 + 30); printf( " e=%.2lf; P=%.1lf min; i=%.1lf", tle.eo, 2. * PI / tle.xno, tle.xincl * 180. / PI); if( strlen( line0) < 30) /* object name given... */ printf( ": %s\n", line0); /* not all TLEs do this */ else printf( "\n"); printf( " delta=%8.1lf km; offset=%5.2lf degrees; motion %6.3lf'/sec at PA=%.1lf\n", dist_to_satellite, radius, arcmin_per_sec, posn_ang); /* "Speed" is displayed in arcminutes/second, or in degrees/minute */ } } } strcpy( preceding_line, line1); strcpy( line0, line1); strcpy( line1, line2); for( i = 0; line0[i] >= ' '; i++) ; line0[i] = '\0'; /* remove trailing CR/LF */ } } else if( show_non_mpc_report_lines) printf( "%s", buff); } fclose( tle_file); fclose( stations); fclose( ifile); return( 0); } /* End of main() */
int main( const int argc, const char **argv) { FILE *ifile = fopen( argv[1], "rb"); char line1[100], line2[100]; const char *intl_id = NULL; double step_size = .1; int i, n_steps = 100; if( !ifile) { printf( "Couldn't open input file\n"); exit( -1); } for( i = 1; i < argc; i++) if( argv[i][0] == '-') switch( argv[i][1]) { case 'i': intl_id = argv[i] + 2; break; case 'n': n_steps = atoi( argv[i] + 2); break; default: printf( "Unrecognized option '%s'\n", argv[i]); break; } *line1 = '\0'; sxpx_set_implementation_param( SXPX_DUNDEE_COMPLIANCE, 1); while( fgets( line2, sizeof( line2), ifile)) { tle_t tle; /* Pointer to two-line elements set for satellite */ int err_val; if( (!intl_id || !memcmp( intl_id, line1 + 9, 6)) && (err_val = parse_elements( line1, line2, &tle)) >= 0) { /* hey! we got a TLE! */ int is_deep = select_ephemeris( &tle); double sat_params[N_SAT_PARAMS], observer_loc[3]; if( err_val) printf( "WARNING: TLE parsing error %d\n", err_val); for( i = 0; i < 3; i++) observer_loc[i] = '\0'; if( is_deep) SDP4_init( sat_params, &tle); else SGP4_init( sat_params, &tle); for( i = 0; i < n_steps; i++) { double ra, dec, dist_to_satellite; double pos[3]; /* Satellite position vector */ double t_since = (double)( i - n_steps / 2) * step_size; double jd = tle.epoch + t_since; t_since *= 1440.; if( is_deep) err_val = SDP4( t_since, &tle, sat_params, pos, NULL); else err_val = SGP4( t_since, &tle, sat_params, pos, NULL); if( err_val) printf( "Ephemeris error %d\n", err_val); get_satellite_ra_dec_delta( observer_loc, pos, &ra, &dec, &dist_to_satellite); epoch_of_date_to_j2000( jd, &ra, &dec); printf( "%-14sC%13.5f %08.4f %+08.4f", intl_id, jd, ra * 180. / PI, dec * 180. / PI); printf( " TLEs 500\n"); } } strcpy( line1, line2); } fclose( ifile); return( 0); } /* End of main() */