public double max_gps_height;
public double max_speed;
public double max_acceleration;
- public double[] state_speed = new double[AltosLib.ao_flight_invalid + 1];
- public double[] state_accel = new double[AltosLib.ao_flight_invalid + 1];
- public int[] state_count = new int[AltosLib.ao_flight_invalid + 1];
- public double[] state_start = new double[AltosLib.ao_flight_invalid + 1];
- public double[] state_end = new double[AltosLib.ao_flight_invalid + 1];
+ public double[] state_speed = new double[AltosLib.ao_flight_invalid + 1];
+ public double[] state_accel = new double[AltosLib.ao_flight_invalid + 1];
+ public double[] state_start = new double[AltosLib.ao_flight_invalid + 1];
+ public double[] state_end = new double[AltosLib.ao_flight_invalid + 1];
public String product;
public String firmware_version;
public int serial;
fixed_landed = true;
}
}
- if (!fixed_boost && boost_time != AltosLib.MISSING)
- series.state_series.add(boost_time, AltosLib.ao_flight_boost);
- if (!fixed_landed && landed_time != AltosLib.MISSING)
- series.state_series.add(landed_time, AltosLib.ao_flight_landed);
}
- System.out.printf("boost time %g landed %g\n", boost_time, landed_time);
-
year = month = day = AltosLib.MISSING;
hour = minute = second = AltosLib.MISSING;
serial = flight = AltosLib.MISSING;
has_mag = false;
has_orient = false;
- for (int s = AltosLib.ao_flight_startup; s <= AltosLib.ao_flight_landed; s++) {
- state_count[s] = 0;
+ for (int s = 0; s < AltosLib.ao_flight_invalid + 1; s++)
+ state_speed[s] = state_accel[s] = state_start[s] = state_end[s] = AltosLib.MISSING;
- if (s == AltosLib.ao_flight_boost)
- state_start[s] = boost_time;
- else if (series.state_series != null)
- state_start[s] = series.state_series.time_of(s);
- else
- state_start[s] = AltosLib.MISSING;
+ if (series.state_series != null) {
+ for (AltosTimeValue state : series.state_series) {
+ int s = (int) state.value;
- if (s == AltosLib.ao_flight_main)
- state_end[s] = landed_time;
- else if (series.state_series != null)
- state_end[s] = series.state_series.time_of(s+1);
- else
- state_end[s] = AltosLib.MISSING;
+ if (s < AltosLib.ao_flight_startup && AltosLib.ao_flight_landed < s)
+ continue;
- System.out.printf("state %s start %g end %g\n", AltosLib.state_name(s), state_start[s], state_end[s]);
+ if (s == AltosLib.ao_flight_boost)
+ state_start[s] = boost_time;
+ else
+ state_start[s] = series.state_series.time_of(s);
- if (state_end[s] > landed_time)
- state_end[s] = landed_time;
+ 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.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]);
+ if (series.accel_series != null)
+ state_accel[s] = series.accel_series.average(state_start[s], state_end[s]);
+ }
}
product = cal_data.product;
max_acceleration = tv.value;
}
max_gps_height = AltosLib.MISSING;
- if (series.gps_height != null)
- max_gps_height = series.gps_height.max().value;
-
+ if (series.gps_height != null) {
+ AltosTimeValue tv = series.gps_height.max();
+ if (tv != null)
+ max_gps_height = tv.value;
+ }
}
}