git.gag.com Git - fw/altos/blob - altoslib/AltosFlightStats.java

   1 /*
   2  * Copyright © 2011 Keith Packard <keithp@keithp.com>
   3  *
   4  * This program is free software; you can redistribute it and/or modify
   5  * it under the terms of the GNU General Public License as published by
   6  * the Free Software Foundation; either version 2 of the License, or
   7  * (at your option) any later version.
   8  *
   9  * This program is distributed in the hope that it will be useful, but
  10  * WITHOUT ANY WARRANTY; without even the implied warranty of
  11  * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
  12  * General Public License for more details.
  13  *
  14  * You should have received a copy of the GNU General Public License along
  15  * with this program; if not, write to the Free Software Foundation, Inc.,
  16  * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA.
  17  */
  18
  19 package org.altusmetrum.altoslib_12;
  20
  21 import java.io.*;
  22
  23 public class AltosFlightStats {
  24         public double           max_height;
  25         public double           max_gps_height;
  26         public double           max_speed;
  27         public double           max_acceleration;
  28         public double[]         state_speed = new double[AltosLib.ao_flight_invalid + 1];
  29         public double[]         state_enter_speed = new double[AltosLib.ao_flight_invalid + 1];
  30         public double[]         state_accel = new double[AltosLib.ao_flight_invalid + 1];
  31         public double[]         state_time = new double[AltosLib.ao_flight_invalid + 1];
  32         public String           product;
  33         public String           firmware_version;
  34         public int              serial;
  35         public int              flight;
  36         public int              year, month, day;
  37         public int              hour, minute, second;
  38         public double           boost_time;
  39         public double           landed_time;
  40         public double           lat, lon;
  41         public double           pad_lat, pad_lon;
  42         public boolean          has_flight_data;
  43         public boolean          has_gps;
  44         public boolean          has_gps_sats;
  45         public boolean          has_gps_detail;
  46         public boolean          has_flight_adc;
  47         public boolean          has_battery;
  48         public boolean          has_rssi;
  49         public boolean          has_imu;
  50         public boolean          has_mag;
  51         public boolean          has_orient;
  52         public int              num_igniter;
  53
  54         double landed_time(AltosFlightSeries series) {
  55                 double  landed_state_time = AltosLib.MISSING;
  56
  57                 double  prev_state_time = AltosLib.MISSING;
  58                 if (series.state_series != null) {
  59                         for (AltosTimeValue state : series.state_series) {
  60                                 if (state.value == AltosLib.ao_flight_landed) {
  61                                         landed_state_time = state.time;
  62                                         break;
  63                                 } else {
  64                                         prev_state_time = state.time;
  65                                 }
  66                         }
  67                 }
  68
  69                 if (landed_state_time == AltosLib.MISSING && series.height_series != null)
  70                         landed_state_time = series.height_series.get(series.height_series.size()-1).time;
  71
  72                 double landed_height = AltosLib.MISSING;
  73
  74                 if (series.height_series != null) {
  75                         for (AltosTimeValue height : series.height_series) {
  76                                 landed_height = height.value;
  77                                 if (height.time >= landed_state_time)
  78                                         break;
  79                         }
  80                 }
  81
  82                 if (landed_height == AltosLib.MISSING)
  83                         return AltosLib.MISSING;
  84
  85                 boolean above = true;
  86
  87                 double  landed_time = AltosLib.MISSING;
  88
  89                 if (series.height_series != null) {
  90                         for (AltosTimeValue height : series.height_series) {
  91                                 if (height.value > landed_height + 10) {
  92                                         above = true;
  93                                 } else {
  94                                         if (above && Math.abs(height.value - landed_height) < 2) {
  95                                                 above = false;
  96                                                 landed_time = height.time;
  97                                         }
  98                                 }
  99                         }
 100                 }
 101
 102                 if (landed_time == AltosLib.MISSING || (prev_state_time != AltosLib.MISSING && landed_time < prev_state_time))
 103                         landed_time = landed_state_time;
 104                 return landed_time;
 105         }
 106
 107         double boost_time(AltosFlightSeries series) {
 108                 double          boost_time = AltosLib.MISSING;
 109                 double          boost_state_time = AltosLib.MISSING;
 110
 111                 if (series.state_series != null) {
 112                         for (AltosTimeValue state : series.state_series) {
 113                                 if (state.value >= AltosLib.ao_flight_boost && state.value <= AltosLib.ao_flight_landed) {
 114                                         boost_state_time = state.time;
 115                                         break;
 116                                 }
 117                         }
 118                 }
 119                 if (series.accel_series != null) {
 120                         for (AltosTimeValue accel : series.accel_series) {
 121                                 if (accel.value < 1)
 122                                         boost_time = accel.time;
 123                                 if (boost_state_time != AltosLib.MISSING && accel.time >= boost_state_time)
 124                                         break;
 125                         }
 126                 }
 127                 if (boost_time == AltosLib.MISSING)
 128                         boost_time = boost_state_time;
 129                 return boost_time;
 130         }
 131
 132         private void add_times(AltosFlightSeries series, int state, double start_time, double end_time) {
 133                 double delta_time = end_time - start_time;
 134                 if (0 <= state && state <= AltosLib.ao_flight_invalid && delta_time > 0) {
 135                         if (state_enter_speed[state] == AltosLib.MISSING)
 136                                 state_enter_speed[state] = series.speed_series.value(start_time);
 137                         speeds[state].value += series.speed_series.average(start_time, end_time) * delta_time;
 138                         speeds[state].time += delta_time;
 139                         accels[state].value += series.accel_series.average(start_time, end_time) * delta_time;
 140                         accels[state].time += delta_time;
 141                         state_time[state] += delta_time;
 142
 143                         if (state == AltosLib.ao_flight_boost) {
 144                                 AltosTimeValue tv_speed = series.speed_series.max(start_time, end_time);
 145                                 if (tv_speed != null && (max_speed == AltosLib.MISSING || tv_speed.value > max_speed))
 146                                         max_speed = tv_speed.value;
 147                                 AltosTimeValue tv_accel = series.accel_series.max(start_time, end_time);
 148                                 if (tv_accel != null && (max_acceleration == AltosLib.MISSING || tv_accel.value > max_acceleration))
 149                                         max_acceleration = tv_accel.value;
 150                         }
 151                 }
 152         }
 153
 154         AltosTimeValue[]        speeds = new AltosTimeValue[AltosLib.ao_flight_invalid + 1];
 155         AltosTimeValue[]        accels = new AltosTimeValue[AltosLib.ao_flight_invalid + 1];
 156
 157         public AltosFlightStats(AltosFlightSeries series) {
 158                 AltosCalData    cal_data = series.cal_data();
 159
 160                 series.finish();
 161
 162                 boost_time = boost_time(series);
 163                 landed_time = landed_time(series);
 164
 165                 if (series.state_series != null){
 166                         boolean fixed_boost = false;
 167                         boolean fixed_landed = false;
 168                         for (AltosTimeValue state : series.state_series) {
 169                                 if ((int) state.value == AltosLib.ao_flight_boost)
 170                                         if (boost_time != AltosLib.MISSING && !fixed_boost) {
 171                                                 state.time = boost_time;
 172                                                 fixed_boost = true;
 173                                         }
 174                                 if ((int) state.value == AltosLib.ao_flight_landed)
 175                                         if (landed_time != AltosLib.MISSING && !fixed_landed) {
 176                                                 state.time = landed_time;
 177                                                 fixed_landed = true;
 178                                         }
 179                         }
 180                 }
 181
 182                 year = month = day = AltosLib.MISSING;
 183                 hour = minute = second = AltosLib.MISSING;
 184                 serial = flight = AltosLib.MISSING;
 185                 lat = lon = AltosLib.MISSING;
 186                 has_flight_data = false;
 187                 has_gps = false;
 188                 has_gps_sats = false;
 189                 has_flight_adc = false;
 190                 has_battery = false;
 191                 has_rssi = false;
 192                 has_imu = false;
 193                 has_mag = false;
 194                 has_orient = false;
 195
 196                 for (int s = 0; s < AltosLib.ao_flight_invalid + 1; s++) {
 197                         state_speed[s] = AltosLib.MISSING;
 198                         state_enter_speed[s] = AltosLib.MISSING;
 199                         state_accel[s] = AltosLib.MISSING;
 200                         state_time[s] = 0;
 201                         speeds[s] = new AltosTimeValue(0, 0);
 202                         accels[s] = new AltosTimeValue(0, 0);
 203                 }
 204
 205                 max_speed = AltosLib.MISSING;
 206                 max_acceleration = AltosLib.MISSING;
 207
 208                 if (series.state_series != null) {
 209                         AltosTimeValue prev = null;
 210                         for (AltosTimeValue state : series.state_series) {
 211                                 if (prev != null)
 212                                         add_times(series, (int) prev.value, prev.time, state.time);
 213                                 prev = state;
 214                         }
 215                         if (prev != null)
 216                                 add_times(series, (int) prev.value, prev.time, series.accel_series.last().time);
 217                 }
 218
 219                 for (int s = 0; s <= AltosLib.ao_flight_invalid; s++) {
 220                         if (speeds[s].time > 0)
 221                                 state_speed[s] = speeds[s].value / speeds[s].time;
 222                         if (accels[s].time > 0)
 223                                 state_accel[s] = accels[s].value / accels[s].time;
 224                 }
 225
 226                 product = cal_data.product;
 227                 firmware_version = cal_data.firmware_version;
 228                 serial = cal_data.serial;
 229                 flight = cal_data.flight;
 230
 231                 has_battery = series.battery_voltage_series != null;
 232                 has_flight_adc = series.main_voltage_series != null;
 233                 has_rssi = series.rssi_series != null;
 234                 has_flight_data = series.pressure_series != null;
 235
 236                 AltosGPS gps = series.cal_data().gps_pad;
 237
 238                 if (gps != null) {
 239                         year = gps.year;
 240                         month = gps.month;
 241                         day = gps.day;
 242                         hour = gps.hour;
 243                         minute = gps.minute;
 244                         second = gps.second;
 245                         has_gps = true;
 246                         lat = pad_lat = gps.lat;
 247                         lon = pad_lon = gps.lon;
 248                         for (AltosGPSTimeValue gtv : series.gps_series) {
 249                                 gps = gtv.gps;
 250                                 if (gps.locked && gps.nsat >= 4) {
 251                                         lat = gps.lat;
 252                                         lon = gps.lon;
 253                                 }
 254                         }
 255
 256                 }
 257
 258                 max_height = AltosLib.MISSING;
 259                 if (series.height_series != null)
 260                         max_height = series.height_series.max().value;
 261                 max_gps_height = AltosLib.MISSING;
 262                 if (series.gps_height != null) {
 263                         AltosTimeValue tv = series.gps_height.max();
 264                         if (tv != null)
 265                                 max_gps_height = tv.value;
 266                 }
 267         }
 268 }