- altitude = aoview_pres_to_altitude(state->pres) - aoview_pres_to_altitude(pad_pres);
- accel = (pad_accel - state->accel) / 264.8 * 9.80665;
- velocity_change = (accel + prev_accel) / 2.0;
- ticks = state->tick - prev_tick;
- velocity -= velocity_change * (ticks / 100.0);
-
- prev_accel = accel;
- prev_tick = state->tick;
- printf ("Pad altitude: %dm\n", aoview_pres_to_altitude(pad_pres));
- printf ("AGL: %dm\n", altitude);
- printf ("Acceleration: %gm/s²\n", accel);
- printf ("Velocity: %gm/s\n", velocity);
- printf ("Lat: %g\n", state->lat);
- printf ("Lon: %g\n", state->lon);
- printf ("GPS alt: %d\n", state->alt);
- aoview_great_circle(pad_lat, pad_lon, state->lat, state->lon,
- &dist, &bearing);
- printf ("Course: %gkm %g°\n", dist, bearing);
+ return TRUE;
+}
+
+void
+aoview_state_reset(void)
+{
+ memset(&aostate, '\0', sizeof (aostate));
+}
+
+void
+aoview_state_notify(struct aodata *data)
+{
+ struct aostate *state = &aostate;
+ aoview_state_derive(data, state);
+ aoview_table_start();
+
+ if (state->npad >= MIN_PAD_SAMPLES)
+ aoview_table_add_row("Ground state", "ready");
+ else
+ aoview_table_add_row("Ground state", "waiting for gps (%d)",
+ MIN_PAD_SAMPLES - state->npad);
+ aoview_table_add_row("Rocket state", "%s", state->data.state);
+ aoview_table_add_row("Callsign", "%s", state->data.callsign);
+ aoview_table_add_row("Rocket serial", "%d", state->data.serial);
+
+ aoview_table_add_row("RSSI", "%6ddBm", state->data.rssi);
+ aoview_table_add_row("Height", "%6dm", state->height);
+ aoview_table_add_row("Max height", "%6dm", state->max_height);
+ aoview_table_add_row("Acceleration", "%7.1fm/s²", state->acceleration);
+ aoview_table_add_row("Max acceleration", "%7.1fm/s²", state->max_acceleration);
+ aoview_table_add_row("Speed", "%7.1fm/s", state->ascent ? state->speed : state->baro_speed);
+ aoview_table_add_row("Max Speed", "%7.1fm/s", state->max_speed);
+ aoview_table_add_row("Temperature", "%6.2f°C", state->temperature);
+ aoview_table_add_row("Battery", "%5.2fV", state->battery);
+ aoview_table_add_row("Drogue", "%5.2fV", state->drogue_sense);
+ aoview_table_add_row("Main", "%5.2fV", state->main_sense);
+ aoview_table_add_row("Pad altitude", "%dm", state->ground_altitude);
+ aoview_table_add_row("Satellites", "%d", state->data.nsat);
+ if (state->data.locked) {
+ aoview_state_add_deg("Latitude", state->data.lat, 'N', 'S');
+ aoview_state_add_deg("Longitude", state->data.lon, 'E', 'W');
+ aoview_table_add_row("GPS height", "%d", state->gps_height);
+ aoview_table_add_row("GPS time", "%02d:%02d:%02d",
+ state->data.gps_time.hour,
+ state->data.gps_time.minute,
+ state->data.gps_time.second);
+ aoview_table_add_row("GPS ground speed", "%7.1fm/s %d°",
+ state->data.ground_speed,
+ state->data.course);
+ aoview_table_add_row("GPS climb rate", "%7.1fm/s",
+ state->data.climb_rate);
+ aoview_table_add_row("GPS precision", "%f(hdop) %dm(h) %dm(v)\n",
+ state->data.hdop, state->data.h_error, state->data.v_error);
+ aoview_table_add_row("Distance from pad", "%5.0fm", state->distance);
+ aoview_table_add_row("Direction from pad", "%4.0f°", state->bearing);
+ } else {
+ aoview_table_add_row("GPS", "unlocked");
+ }
+ if (state->npad) {
+ aoview_state_add_deg("Pad latitude", state->pad_lat, 'N', 'S');
+ aoview_state_add_deg("Pad longitude", state->pad_lon, 'E', 'W');
+ aoview_table_add_row("Pad GPS alt", "%gm", state->pad_alt);
+ }
+ aoview_table_finish();
+ aoview_label_show(state);
+ aoview_speak_state(state);
+ if (!aostate_timeout && strcmp(state->data.state, "pad") != 0)
+ aostate_timeout = g_timeout_add_seconds(10, aoview_state_timeout, NULL);
+}
+
+void
+aoview_state_new(void)
+{