Rename state apogee -> coast

[fw/altos] / src / ao_flight.c

diff --git a/src/ao_flight.c b/src/ao_flight.c
index c0f5683047b4d5e3e37dd6d28d14bb9de71295e2..be9b3bb6f4cfdbf4e55a9681dac98bbec304b471 100644 (file)
--- a/src/ao_flight.c
+++ b/src/ao_flight.c
@@ -216,7 +216,7 @@ ao_flight(void)
                        ao_old_vel = ao_flight_vel;
                        ao_old_vel_tick = ao_flight_tick;
 
-                       /* Go to launchpad state if the nose is pointing up */
+                       /* Go to pad state if the nose is pointing up */
                        ao_config_get();
                        if (ao_flight_accel < ao_config.accel_zero_g - ACCEL_NOSE_UP) {
 
@@ -229,7 +229,7 @@ ao_flight(void)
                                 */
                                ao_telemetry_set_interval(AO_TELEMETRY_INTERVAL_PAD);
 
-                               ao_flight_state = ao_flight_launchpad;
+                               ao_flight_state = ao_flight_pad;
                                ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
                        } else {
                                ao_flight_state = ao_flight_idle;
@@ -242,7 +242,7 @@ ao_flight(void)
                        /* signal successful initialization by turning off the LED */
                        ao_led_off(AO_LED_RED);
                        break;
-               case ao_flight_launchpad:
+               case ao_flight_pad:
 
                        /* Trim velocity
                         *
@@ -283,7 +283,7 @@ ao_flight(void)
                        break;
                case ao_flight_boost:
 
-                       /* boost to coast:
+                       /* boost to fast:
                         *
                         * accelerometer: start to fall at > 1/4 G
                         *              OR
@@ -296,14 +296,14 @@ ao_flight(void)
                        if (ao_flight_accel > ao_ground_accel + (ACCEL_G >> 2) ||
                            (int16_t) (ao_flight_tick - ao_launch_tick) > BOOST_TICKS_MAX)
                        {
-                               ao_flight_state = ao_flight_coast;
+                               ao_flight_state = ao_flight_fast;
                                ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
                                break;
                        }
                        break;
-               case ao_flight_coast:
+               case ao_flight_fast:
 
-                       /* coast to apogee detect:
+                       /* fast to coast:
                         *
                         * accelerometer: integrated velocity < 200 m/s
                         *               OR
@@ -325,13 +325,13 @@ ao_flight(void)
                                 * apogee detect
                                 */
                                ao_min_vel = abs(ao_flight_vel);
-                               ao_flight_state = ao_flight_apogee;
+                               ao_flight_state = ao_flight_coast;
                                ao_wakeup(DATA_TO_XDATA(&ao_flight_state));
                        }
                        break;
-               case ao_flight_apogee:
+               case ao_flight_coast:
 
-                       /* apogee detect to drogue deploy:
+                       /* apogee detect: coast to drogue deploy:
                         *
                         * accelerometer: abs(velocity) > min_velocity + 2m/s
                         *               OR