Transmit computed ground pressure and acceleration values
[fw/altos] / ao_monitor.c
index 6aed581a69b1f6d71a1b597923860f31428c728e..5997d427a4388536687bf1a0c3a4c93238d655bb 100644 (file)
@@ -36,19 +36,24 @@ ao_monitor(void)
                if (state > ao_flight_invalid)
                        state = ao_flight_invalid;
                if (recv.status & PKT_APPEND_STATUS_1_CRC_OK) {
-                       printf ("CALL %s SERIAL %3d RSSI %3d STATUS %02x STATE %7s ",
+                       printf ("CALL %s SERIAL %3d RSSI %4d STATUS %02x STATE %7s ",
                                callsign,
                                recv.telemetry.addr,
                                (int) recv.rssi - 74, recv.status,
                                ao_state_names[state]);
-                       printf("%5u a: %5d p: %5d t: %5d v: %5d d: %5d m: %5d ",
+                       printf("%5u a: %5d p: %5d t: %5d v: %5d d: %5d m: %5d fa: %5d ga: %d fv: %7ld fp: %5d gp: %5d ",
                               recv.telemetry.adc.tick,
                               recv.telemetry.adc.accel,
                               recv.telemetry.adc.pres,
                               recv.telemetry.adc.temp,
                               recv.telemetry.adc.v_batt,
                               recv.telemetry.adc.sense_d,
-                              recv.telemetry.adc.sense_m);
+                              recv.telemetry.adc.sense_m,
+                              recv.telemetry.flight_accel,
+                              recv.telemetry.ground_accel,
+                              recv.telemetry.flight_vel,
+                              recv.telemetry.flight_pres,
+                              recv.telemetry.ground_pres);
                        ao_gps_print(&recv.telemetry.gps);
                        ao_rssi_set((int) recv.rssi - 74);
                } else {