@@ -745,36 +745,36 @@ float cn0_est(cn0_est_state_t *s, float I, float Q)
745745 return s -> log_bw - 10.f * log10f (s -> nsr );
746746}
747747
748- void calc_navigation_measurement (u8 n_channels , channel_measurement_t meas [],
749- navigation_measurement_t nav_meas [],
748+ void calc_navigation_measurement (u8 n_channels , const channel_measurement_t * meas [],
749+ navigation_measurement_t * nav_meas [],
750750 double nav_time , const ephemeris_t * e [])
751751{
752752 double TOTs [n_channels ];
753753 double min_TOF = - DBL_MAX ;
754754 double clock_err [n_channels ], clock_rate_err [n_channels ];
755755
756756 for (u8 i = 0 ; i < n_channels ; i ++ ) {
757- TOTs [i ] = 1e-3 * meas [i ]. time_of_week_ms ;
758- TOTs [i ] += meas [i ]. code_phase_chips / 1.023e6 ;
759- TOTs [i ] += (nav_time - meas [i ]. receiver_time ) * meas [i ]. code_phase_rate / 1.023e6 ;
757+ TOTs [i ] = 1e-3 * meas [i ]-> time_of_week_ms ;
758+ TOTs [i ] += meas [i ]-> code_phase_chips / 1.023e6 ;
759+ TOTs [i ] += (nav_time - meas [i ]-> receiver_time ) * meas [i ]-> code_phase_rate / 1.023e6 ;
760760
761761 /** \todo Maybe keep track of week number in tracking channel
762762 state or derive it from system time. */
763- nav_meas [i ]. tot .tow = TOTs [i ];
764- gps_time_match_weeks (& nav_meas [i ]. tot , & e [i ]-> toe );
763+ nav_meas [i ]-> tot .tow = TOTs [i ];
764+ gps_time_match_weeks (& nav_meas [i ]-> tot , & e [i ]-> toe );
765765
766- nav_meas [i ]. raw_doppler = meas [i ]. carrier_freq ;
767- nav_meas [i ]. snr = meas [i ]. snr ;
768- nav_meas [i ]. sid = meas [i ]. sid ;
766+ nav_meas [i ]-> raw_doppler = meas [i ]-> carrier_freq ;
767+ nav_meas [i ]-> snr = meas [i ]-> snr ;
768+ nav_meas [i ]-> sid = meas [i ]-> sid ;
769769
770- nav_meas [i ]. carrier_phase = meas [i ]. carrier_phase ;
771- nav_meas [i ]. carrier_phase += (nav_time - meas [i ]. receiver_time ) * meas [i ]. carrier_freq ;
770+ nav_meas [i ]-> carrier_phase = meas [i ]-> carrier_phase ;
771+ nav_meas [i ]-> carrier_phase += (nav_time - meas [i ]-> receiver_time ) * meas [i ]-> carrier_freq ;
772772
773- nav_meas [i ]. lock_counter = meas [i ]. lock_counter ;
773+ nav_meas [i ]-> lock_counter = meas [i ]-> lock_counter ;
774774
775775 /* calc sat clock error */
776- calc_sat_state (e [i ], nav_meas [i ]. tot ,
777- nav_meas [i ]. sat_pos , nav_meas [i ]. sat_vel ,
776+ calc_sat_state (e [i ], nav_meas [i ]-> tot ,
777+ nav_meas [i ]-> sat_pos , nav_meas [i ]-> sat_vel ,
778778 & clock_err [i ], & clock_rate_err [i ]);
779779
780780 /* remove clock error to put all tots within the same time window */
@@ -783,14 +783,14 @@ void calc_navigation_measurement(u8 n_channels, channel_measurement_t meas[],
783783 }
784784
785785 for (u8 i = 0 ; i < n_channels ; i ++ ) {
786- nav_meas [i ]. raw_pseudorange = (min_TOF - TOTs [i ])* GPS_C + GPS_NOMINAL_RANGE ;
786+ nav_meas [i ]-> raw_pseudorange = (min_TOF - TOTs [i ])* GPS_C + GPS_NOMINAL_RANGE ;
787787
788- nav_meas [i ]. pseudorange = nav_meas [i ]. raw_pseudorange \
788+ nav_meas [i ]-> pseudorange = nav_meas [i ]-> raw_pseudorange \
789789 + clock_err [i ]* GPS_C ;
790- nav_meas [i ]. doppler = nav_meas [i ]. raw_doppler + clock_rate_err [i ]* GPS_L1_HZ ;
790+ nav_meas [i ]-> doppler = nav_meas [i ]-> raw_doppler + clock_rate_err [i ]* GPS_L1_HZ ;
791791
792- nav_meas [i ]. tot .tow -= clock_err [i ];
793- nav_meas [i ]. tot = normalize_gps_time (nav_meas [i ]. tot );
792+ nav_meas [i ]-> tot .tow -= clock_err [i ];
793+ nav_meas [i ]-> tot = normalize_gps_time (nav_meas [i ]-> tot );
794794 }
795795}
796796
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