Record average accelerometer value in flight start log record

[fw/altos] / ao_log.c

diff --git a/ao_log.c b/ao_log.c
index c74893f87af9a61b11d4343ae6a21b0b69630e5a..47d960d4e517c85507cbcbeae8cf8ac5cefc73c9 100644 (file)
--- a/ao_log.c
+++ b/ao_log.c
@@ -121,19 +121,13 @@ ao_log(void)
        
        log.type = AO_LOG_FLIGHT;
        log.tick = ao_flight_tick;
-       log.u.flight.serial = 0;
+       log.u.flight.ground_accel = ao_ground_accel;
        log.u.flight.flight = ao_log_dump_flight + 1;
        ao_log_data(&log);
        for (;;) {
-               /* Write state change to EEPROM */
-               if (ao_flight_state != ao_log_state) {
-                       ao_log_state = ao_flight_state;
-                       log.type = AO_LOG_STATE;
-                       log.tick = ao_flight_tick;
-                       log.u.state.state = ao_log_state;
-                       log.u.state.reason = 0;
-                       ao_log_data(&log);
-               }
+               while (!ao_log_running)
+                       ao_sleep(&ao_log_running);
+
                /* Write samples to EEPROM */
                while (ao_log_adc_pos != ao_adc_head) {
                        log.type = AO_LOG_SENSOR;
@@ -155,6 +149,18 @@ ao_log(void)
                        }
                        ao_log_adc_pos = ao_adc_ring_next(ao_log_adc_pos);
                }
+               /* Write state change to EEPROM */
+               if (ao_flight_state != ao_log_state) {
+                       ao_log_state = ao_flight_state;
+                       log.type = AO_LOG_STATE;
+                       log.tick = ao_flight_tick;
+                       log.u.state.state = ao_log_state;
+                       log.u.state.reason = 0;
+                       ao_log_data(&log);
+
+                       if (ao_log_state == ao_flight_landed)
+                               ao_log_stop();
+               }
                
                /* Wait for a while */
                ao_delay(AO_MS_TO_TICKS(100));