Steal C code from ao-view
[fw/altos] / ao-tools / altosui / AltosState.java
diff --git a/ao-tools/altosui/AltosState.java b/ao-tools/altosui/AltosState.java
new file mode 100644 (file)
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+/*
+ * Copyright © 2010 Keith Packard <keithp@keithp.com>
+ *
+ * This program is free software; you can redistribute it and/or modify
+ * it under the terms of the GNU General Public License as published by
+ * the Free Software Foundation; version 2 of the License.
+ *
+ * This program is distributed in the hope that it will be useful, but
+ * WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
+ * General Public License for more details.
+ *
+ * You should have received a copy of the GNU General Public License along
+ * with this program; if not, write to the Free Software Foundation, Inc.,
+ * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
+ */
+
+/*
+ * Track flight state from telemetry data stream
+ */
+
+package altosui;
+
+import altosui.AltosTelemetry;
+import altosui.AltosGPS;
+
+public class AltosState {
+       AltosTelemetry data;
+       AltosTelemetry prev_data;
+
+       /* derived data */
+
+       double  report_time;
+
+       int     state;
+       boolean ascent; /* going up? */
+
+       double  ground_altitude;
+       double  height;
+       double  speed;
+       double  acceleration;
+       double  battery;
+       double  temperature;
+       double  main_sense;
+       double  drogue_sense;
+       double  baro_speed;
+
+       double  max_height;
+       double  max_acceleration;
+       double  max_speed;
+
+       AltosGPS        gps;
+       AltosGPSTracking        gps_tracking;
+
+       boolean gps_valid;
+       double  pad_lat;
+       double  pad_lon;
+       double  pad_alt;
+       double  pad_lat_total;
+       double  pad_lon_total;
+       double  pad_alt_total;
+       int     npad;
+       int     prev_npad;
+
+       AltosGreatCircle from_pad;
+
+       double  gps_height;
+
+       int     speak_tick;
+       double  speak_altitude;
+
+       static double
+       aoview_time()
+       {
+               return System.currentTimeMillis() / 1000.0;
+       }
+
+       public AltosState (AltosTelemetry cur, AltosTelemetry prev, int prev_npad) {
+               int     i;
+               double  new_height;
+               double  height_change;
+               double  time_change;
+               double  accel_counts_per_mss;
+               int     tick_count;
+
+               data = cur;
+               prev_data = prev;
+               npad = prev_npad;
+               tick_count = data.tick;
+               if (tick_count < prev_data.tick)
+                       tick_count += 65536;
+               time_change = (tick_count - prev_data.tick) / 100.0;
+
+               report_time = aoview_time();
+
+               ground_altitude = AltosConvert.cc_pressure_to_altitude(data.ground_pres);
+               new_height = AltosConvert.cc_pressure_to_altitude(data.flight_pres) - ground_altitude;
+               height_change = new_height - height;
+               height = new_height;
+               if (time_change > 0)
+                       baro_speed = (baro_speed * 3 + (height_change / time_change)) / 4.0;
+               accel_counts_per_mss = ((data.accel_minus_g - data.accel_plus_g) / 2.0) / 9.80665;
+               acceleration = (data.ground_accel - data.flight_accel) / accel_counts_per_mss;
+               speed = data.flight_vel / (accel_counts_per_mss * 100.0);
+               temperature = AltosConvert.cc_thermometer_to_temperature(data.temp);
+               drogue_sense = AltosConvert.cc_ignitor_to_voltage(data.drogue);
+               main_sense = AltosConvert.cc_ignitor_to_voltage(data.main);
+               battery = AltosConvert.cc_battery_to_voltage(data.batt);
+               state = data.state();
+               if (state == AltosTelemetry.ao_flight_pad) {
+                       if (data.gps.gps_locked && data.gps.nsat >= 4) {
+                               npad++;
+                               pad_lat_total += data.gps.lat;
+                               pad_lon_total += data.gps.lon;
+                               pad_alt_total += data.gps.alt;
+                               if (npad > 1) {
+                                       pad_lat = (pad_lat * 31 + data.gps.lat) / 32.0;
+                                       pad_lon = (pad_lon * 31 + data.gps.lon) / 32.0;
+                                       pad_alt = (pad_alt * 31 + data.gps.alt) / 32.0;
+                               } else {
+                                       pad_lat = data.gps.lat;
+                                       pad_lon = data.gps.lon;
+                                       pad_alt = data.gps.alt;
+                               }
+                       }
+               }
+               ascent = (AltosTelemetry.ao_flight_boost <= state &&
+                         state <= AltosTelemetry.ao_flight_coast);
+
+               /* Only look at accelerometer data on the way up */
+               if (ascent && acceleration > max_acceleration)
+                       max_acceleration = acceleration;
+               if (ascent && speed > max_speed)
+                       max_speed = speed;
+
+               if (height > max_height)
+                       max_height = height;
+               gps.gps_locked = data.gps.gps_locked;
+               gps.gps_connected = data.gps.gps_connected;
+               if (data.gps.gps_locked) {
+                       gps = data.gps;
+                       gps_valid = true;
+                       if (npad > 0)
+                               from_pad = new AltosGreatCircle(pad_lat, pad_lon, gps.lat, gps.lon);
+               }
+               if (npad > 0) {
+                       gps_height = gps.alt - pad_alt;
+               } else {
+                       gps_height = 0;
+               }
+       }
+
+       public AltosState(AltosTelemetry cur) {
+               this(cur, cur, 0);
+       }
+
+       public AltosState (AltosTelemetry cur, AltosState prev) {
+               this(cur, prev.data, prev.npad);
+               if (gps == null) {
+                       gps = prev.gps;
+                       gps_valid = prev.gps_valid;
+               }
+               if (gps_tracking == null)
+                       gps_tracking = prev.gps_tracking;
+       }
+}