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Diffstat (limited to 'altosui/AltosFlightStats.java')
| -rw-r--r-- | altosui/AltosFlightStats.java | 189 |
1 files changed, 0 insertions, 189 deletions
diff --git a/altosui/AltosFlightStats.java b/altosui/AltosFlightStats.java deleted file mode 100644 index d02a518d..00000000 --- a/altosui/AltosFlightStats.java +++ /dev/null @@ -1,189 +0,0 @@ -/* - * Copyright © 2011 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. - */ - -package altosui; - -import java.io.*; -import org.altusmetrum.altoslib_3.*; - -public class AltosFlightStats { - double max_height; - double max_gps_height; - double max_speed; - double max_acceleration; - double[] state_speed = new double[Altos.ao_flight_invalid + 1]; - double[] state_accel = new double[Altos.ao_flight_invalid + 1]; - int[] state_count = new int[Altos.ao_flight_invalid + 1]; - double[] state_start = new double[Altos.ao_flight_invalid + 1]; - double[] state_end = new double[Altos.ao_flight_invalid + 1]; - int serial; - int flight; - int year, month, day; - int hour, minute, second; - double lat, lon; - double pad_lat, pad_lon; - boolean has_gps; - boolean has_other_adc; - boolean has_rssi; - boolean has_imu; - boolean has_mag; - boolean has_orient; - int num_ignitor; - - double landed_time(AltosStateIterable states) { - AltosState state = null; - - for (AltosState s : states) { - state = s; - if (state.state == Altos.ao_flight_landed) - break; - } - - if (state == null) - return 0; - - double landed_height = state.height(); - - state = null; - - boolean above = true; - - double landed_time = -1000; - - for (AltosState s : states) { - state = s; - - if (state.height() > landed_height + 10) { - above = true; - } else { - if (above && state.height() < landed_height + 2) { - above = false; - landed_time = state.time; - } - } - } - if (landed_time == -1000) - landed_time = state.time; - return landed_time; - } - - double boost_time(AltosStateIterable states) { - double boost_time = AltosLib.MISSING; - AltosState state = null; - - for (AltosState s : states) { - state = s; - if (state.acceleration() < 1) - boost_time = state.time; - if (state.state >= AltosLib.ao_flight_boost && state.state <= AltosLib.ao_flight_landed) - break; - } - if (state == null) - return 0; - - if (boost_time == AltosLib.MISSING) - boost_time = state.time; - return boost_time; - } - - - public AltosFlightStats(AltosStateIterable states) throws InterruptedException, IOException { - double boost_time = boost_time(states); - double end_time = 0; - double landed_time = landed_time(states); - - year = month = day = AltosLib.MISSING; - hour = minute = second = AltosLib.MISSING; - serial = flight = AltosLib.MISSING; - lat = lon = AltosLib.MISSING; - has_gps = false; - has_other_adc = false; - has_rssi = false; - has_imu = false; - has_mag = false; - has_orient = false; - for (AltosState state : states) { - if (serial == AltosLib.MISSING && state.serial != AltosLib.MISSING) - serial = state.serial; - if (flight == AltosLib.MISSING && state.flight != AltosLib.MISSING) - flight = state.flight; - if (state.battery_voltage != AltosLib.MISSING) - has_other_adc = true; - if (state.rssi != AltosLib.MISSING) - has_rssi = true; - end_time = state.time; - - int state_id = state.state; - if (state.time >= boost_time && state_id < Altos.ao_flight_boost) - state_id = Altos.ao_flight_boost; - if (state.time >= landed_time && state_id < Altos.ao_flight_landed) - state_id = Altos.ao_flight_landed; - if (state.gps != null && state.gps.locked) { - year = state.gps.year; - month = state.gps.month; - day = state.gps.day; - hour = state.gps.hour; - minute = state.gps.minute; - second = state.gps.second; - } - if (0 <= state_id && state_id < Altos.ao_flight_invalid) { - double acceleration = state.acceleration(); - double speed = state.speed(); - if (acceleration != AltosLib.MISSING && speed != AltosLib.MISSING) { - state_accel[state_id] += acceleration; - state_speed[state_id] += speed; - state_count[state_id]++; - } - if (state_start[state_id] == 0.0) - state_start[state_id] = state.time; - if (state_end[state_id] < state.time) - state_end[state_id] = state.time; - max_height = state.max_height(); - max_speed = state.max_speed(); - max_acceleration = state.max_acceleration(); - max_gps_height = state.max_gps_height(); - } - if (state.gps != null && state.gps.locked && state.gps.nsat >= 4) { - if (state_id <= Altos.ao_flight_pad) { - pad_lat = state.gps.lat; - pad_lon = state.gps.lon; - } - lat = state.gps.lat; - lon = state.gps.lon; - has_gps = true; - } - if (state.imu != null) - has_imu = true; - if (state.mag != null) - has_mag = true; - if (state.orient() != AltosLib.MISSING) - has_orient = true; - if (state.ignitor_voltage != null && state.ignitor_voltage.length > num_ignitor) - num_ignitor = state.ignitor_voltage.length; - } - for (int s = Altos.ao_flight_startup; s <= Altos.ao_flight_landed; s++) { - if (state_count[s] > 0) { - state_speed[s] /= state_count[s]; - state_accel[s] /= state_count[s]; - } - if (state_start[s] == 0) - state_start[s] = end_time; - if (state_end[s] == 0) - state_end[s] = end_time; - } - } -} |