package altosui;
-import java.awt.*;
-import java.awt.event.*;
-import javax.swing.*;
-import javax.swing.filechooser.FileNameExtensionFilter;
-import javax.swing.table.*;
import java.io.*;
-import java.util.*;
-import java.text.*;
-import java.util.prefs.*;
-import java.util.concurrent.*;
+import org.altusmetrum.altoslib_1.*;
public class AltosFlightStats {
double max_height;
double max_speed;
double max_acceleration;
- double[] state_speed = new double[Altos.ao_flight_invalid + 1];
+ double[] state_accel_speed = new double[Altos.ao_flight_invalid + 1];
double[] state_baro_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];
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;
double landed_time(AltosRecordIterable iterable) {
AltosState state = null;
return landed_time;
}
+ double boost_time(AltosRecordIterable iterable) {
+ double boost_time = -1000;
+
+ AltosState state = null;
+
+ for (AltosRecord record : iterable) {
+ state = new AltosState(record, state);
+
+ if (state.acceleration < 1)
+ boost_time = state.time;
+ if (state.state >= Altos.ao_flight_boost)
+ break;
+ }
+ if (boost_time == -1000)
+ boost_time = state.time;
+ return boost_time;
+ }
+
+
public AltosFlightStats(AltosRecordIterable iterable) throws InterruptedException, IOException {
AltosState state = null;
AltosState new_state = null;
- double boost_time = -1;
+ double boost_time = boost_time(iterable);
double end_time = 0;
double landed_time = landed_time(iterable);
year = month = day = -1;
hour = minute = second = -1;
serial = flight = -1;
+ lat = lon = -1;
+ has_gps = false;
+ has_other_adc = false;
+ has_rssi = false;
for (AltosRecord record : iterable) {
if (serial < 0)
serial = record.serial;
if ((record.seen & AltosRecord.seen_flight) != 0 && flight < 0)
flight = record.flight;
+ if ((record.seen & AltosRecord.seen_temp_volt) != 0)
+ has_other_adc = true;
+ if (record.rssi != 0)
+ has_rssi = true;
new_state = new AltosState(record, state);
end_time = new_state.time;
state = new_state;
+ if (state.time >= boost_time && state.state < Altos.ao_flight_boost)
+ state.state = Altos.ao_flight_boost;
+ if (state.time >= landed_time && state.state < Altos.ao_flight_landed)
+ state.state = Altos.ao_flight_landed;
if (0 <= state.state && state.state < Altos.ao_flight_invalid) {
if (state.state >= Altos.ao_flight_boost) {
- if (boost_time == -1)
- boost_time = state.time;
if (state.gps != null && state.gps.locked &&
year < 0) {
year = state.gps.year;
second = state.gps.second;
}
}
- if (state.time >= landed_time)
- state.state = Altos.ao_flight_landed;
state_accel[state.state] += state.acceleration;
- state_speed[state.state] += state.speed;
+ state_accel_speed[state.state] += state.accel_speed;
state_baro_speed[state.state] += state.baro_speed;
state_count[state.state]++;
if (state_start[state.state] == 0.0)
if (state_end[state.state] < state.time)
state_end[state.state] = state.time;
max_height = state.max_height;
- if (state.max_speed != 0)
- max_speed = state.max_speed;
+ if (state.max_accel_speed != 0)
+ max_speed = state.max_accel_speed;
else
max_speed = state.max_baro_speed;
max_acceleration = state.max_acceleration;
}
+ if (state.gps.locked && state.gps.nsat >= 4) {
+ if (state.state <= 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;
+ }
}
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_speed[s] /= state_count[s];
state_baro_speed[s] /= state_count[s];
state_accel[s] /= state_count[s];
}