}
void write_basic_header() {
- out.printf("acceleration,pressure,altitude,height,accel_speed,baro_speed,temperature,drogue_voltage,main_voltage");
+ out.printf("pressure,thrust");
}
- double acceleration() { return series.value(AltosFlightSeries.accel_name, indices); }
double pressure() { return series.value(AltosFlightSeries.pressure_name, indices); }
- double altitude() { return series.value(AltosFlightSeries.altitude_name, indices); }
- double height() { return series.value(AltosFlightSeries.height_name, indices); }
- double speed() { return series.value(AltosFlightSeries.speed_name, indices); }
- double temperature() { return series.value(AltosFlightSeries.temperature_name, indices); }
- double apogee_voltage() { return series.value(AltosFlightSeries.apogee_voltage_name, indices); }
- double main_voltage() { return series.value(AltosFlightSeries.main_voltage_name, indices); }
+ double thrust() { return series.value(AltosFlightSeries.thrust_name, indices); }
void write_basic() {
- out.printf("%8.2f,%10.2f,%8.2f,%8.2f,%8.2f,%8.2f,%5.1f,%5.2f,%5.2f",
- acceleration(),
+ out.printf("%10.2f,%10.2f",
pressure(),
- altitude(),
- height(),
- speed(),
- speed(),
- temperature(),
- apogee_voltage(),
- main_voltage());
+ thrust());
}
void write_battery_header() {