public boolean has_imu;
public boolean has_mag;
public boolean has_orient;
- public int num_ignitor;
+ public int num_igniter;
double landed_time(AltosFlightSeries series) {
double landed_state_time = AltosLib.MISSING;
}
if (landed_state_time == AltosLib.MISSING)
- return AltosLib.MISSING;
+ landed_state_time = series.height_series.get(series.height_series.size()-1).time;
double landed_height = AltosLib.MISSING;
for (AltosTimeValue height : series.height_series) {
}
- public AltosFlightStats(AltosFlightSeries series) throws InterruptedException, IOException {
+ public AltosFlightStats(AltosFlightSeries series) {
AltosCalData cal_data = series.cal_data;
double boost_time = boost_time(series);
double end_time = 0;
double landed_time = landed_time(series);
- System.out.printf("flight stats %s\n", series.toString());
+ series.finish();
year = month = day = AltosLib.MISSING;
hour = minute = second = AltosLib.MISSING;
for (int s = AltosLib.ao_flight_startup; s <= AltosLib.ao_flight_landed; s++) {
state_count[s] = 0;
- state_speed[s] = 0.0;
- state_accel[s] = 0.0;
+
+ if (s == AltosLib.ao_flight_boost)
+ state_start[s] = boost_time;
+ else
+ state_start[s] = series.state_series.time_of(s);
+ if (s == AltosLib.ao_flight_main)
+ state_end[s] = landed_time;
+ else
+ state_end[s] = series.state_series.time_of(s+1);
+
+ if (series.speed_series != null)
+ state_speed[s] = series.speed_series.average(state_start[s], state_end[s]);
+
+ if (series.accel_series != null)
+ state_accel[s] = series.accel_series.average(state_start[s], state_end[s]);
}
serial = cal_data.serial;
has_rssi = series.rssi_series != null;
has_flight_data = series.pressure_series != null;
- if (series.gps_series != null) {
- AltosGPS gps = series.gps_series.get(0).gps;
+ AltosGPS gps = series.cal_data.gps_pad;
+ if (gps != null) {
year = gps.year;
month = gps.month;
day = gps.day;
hour = gps.hour;
minute = gps.minute;
second = gps.second;
+ has_gps = true;
+ lat = pad_lat = gps.lat;
+ lon = pad_lon = gps.lon;
+ for (AltosGPSTimeValue gtv : series.gps_series) {
+ gps = gtv.gps;
+ if (gps.locked && gps.nsat >= 4) {
+ lat = gps.lat;
+ lon = gps.lon;
+ }
+ }
+
}
max_height = AltosLib.MISSING;
if (series.height_series != null)
max_height = series.height_series.max();
max_speed = AltosLib.MISSING;
- if (series.speed_series != null)
- max_speed = series.speed_series.max();
- else
- System.out.printf("missing speed series\n");
+ if (series.speed_series != null) {
+ max_speed = series.speed_series.max(state_start[AltosLib.ao_flight_boost], state_start[AltosLib.ao_flight_drogue]);
+ if (max_speed == AltosLib.MISSING)
+ max_speed = series.speed_series.max();
+ }
max_acceleration = AltosLib.MISSING;
- if (series.accel_series != null)
- max_acceleration = series.accel_series.max();
+ if (series.accel_series != null) {
+ max_acceleration = series.accel_series.max(state_start[AltosLib.ao_flight_boost], state_start[AltosLib.ao_flight_drogue]);
+ if (max_acceleration == AltosLib.MISSING)
+ max_acceleration = series.accel_series.max();
+ }
max_gps_height = AltosLib.MISSING;
if (series.gps_height != null)
max_gps_height = series.gps_height.max();
-/*
- for (AltosState state : states) {
- end_time = state.time;
-
- int state_id = state.state();
- if (boost_time != AltosLib.MISSING && state.time >= boost_time && state_id < AltosLib.ao_flight_boost) {
- state_id = AltosLib.ao_flight_boost;
- }
- if (landed_time != AltosLib.MISSING && state.time >= landed_time && state_id < AltosLib.ao_flight_landed) {
- state_id = AltosLib.ao_flight_landed;
- }
-
- if (0 <= state_id && state_id < AltosLib.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;
- }
- if (state.pad_lat != AltosLib.MISSING) {
- pad_lat = state.pad_lat;
- pad_lon = state.pad_lon;
- }
- if (state.gps != null && state.gps.locked && state.gps.nsat >= 4) {
- lat = state.gps.lat;
- lon = state.gps.lon;
- has_gps = true;
- if (state.gps.cc_gps_sat != null)
- has_gps_sats = true;
- if (state.gps.course != AltosLib.MISSING)
- has_gps_detail = 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 = AltosLib.ao_flight_startup; s <= AltosLib.ao_flight_landed; s++) {
- if (state_count[s] > 0) {
- state_speed[s] /= state_count[s];
- state_accel[s] /= state_count[s];
- } else {
- state_speed[s] = AltosLib.MISSING;
- state_accel[s] = AltosLib.MISSING;
- }
- if (state_start[s] == 0)
- state_start[s] = end_time;
- if (state_end[s] == 0)
- state_end[s] = end_time;
- }
}
}