altos: Switch all tick variables to AO_TICK_TYPE/AO_TICK_SIGNED
[fw/altos] / src / kernel / ao_log_motor.c
index 18d6b79e3069f8b7becffd5995c718bbf06a5c77..4af8bd7818579ead1287f53f8d1f057487a1e28e 100644 (file)
@@ -48,6 +48,9 @@ ao_log(void)
        ao_log_data.type = AO_LOG_FLIGHT;
        ao_log_data.tick = ao_sample_tick;
        ao_log_data.u.flight.ground_accel = ao_ground_accel;
+       ao_log_data.u.flight.ground_accel_along = ao_ground_accel_along;
+       ao_log_data.u.flight.ground_accel_through = ao_ground_accel_through;
+       ao_log_data.u.flight.ground_motor_pressure = ao_ground_motor_pressure;
        ao_log_data.u.flight.flight = ao_flight_number;
        ao_log_write(&ao_log_data);
 
@@ -60,10 +63,11 @@ ao_log(void)
        for (;;) {
                /* Write samples to EEPROM */
                while (ao_log_data_pos != ao_data_head) {
-                       ao_log_data.tick = ao_data_ring[ao_log_data_pos].tick;
-                       if ((int16_t) (ao_log_data.tick - next_sensor) >= 0) {
+                       AO_TICK_TYPE tick = ao_data_ring[ao_log_data_pos].tick;
+                       ao_log_data.tick = tick;
+                       if ((AO_TICK_SIGNED) (tick - next_sensor) >= 0) {
                                ao_log_data.type = AO_LOG_SENSOR;
-                               ao_log_data.u.sensor.pressure = ao_data_ring[ao_log_data_pos].adc.pressure;
+                               ao_log_data.u.sensor.pressure = ao_data_motor_pressure(&ao_data_ring[ao_log_data_pos]);
                                ao_log_data.u.sensor.v_batt = ao_data_ring[ao_log_data_pos].adc.v_batt;
                                ao_log_data.u.sensor.accel = ao_data_accel(&ao_data_ring[ao_log_data_pos]);
                                ao_log_data.u.sensor.accel_across = ao_data_across(&ao_data_ring[ao_log_data_pos]);
@@ -71,9 +75,9 @@ ao_log(void)
                                ao_log_data.u.sensor.accel_through = ao_data_through(&ao_data_ring[ao_log_data_pos]);
                                ao_log_write(&ao_log_data);
                                if (ao_log_state <= ao_flight_coast)
-                                       next_sensor = ao_log_data.tick + AO_SENSOR_INTERVAL_ASCENT;
+                                       next_sensor = tick + AO_SENSOR_INTERVAL_ASCENT;
                                else
-                                       next_sensor = ao_log_data.tick + AO_SENSOR_INTERVAL_DESCENT;
+                                       next_sensor = tick + AO_SENSOR_INTERVAL_DESCENT;
                        }
                        ao_log_data_pos = ao_data_ring_next(ao_log_data_pos);
                }