/* AO_LOG_FLIGHT elements */
public int flight() { return data16(0); }
- public int idle_pres() { return data16(2); }
- public int idle_thrust() { return data16(4); }
/* AO_LOG_STATE elements */
public int state() { return data16(0); }
if (v < 0.5) v = 0.5;
if (v > 4.5) v = 4.5;
- double psi = (v - 0.5) / 4.0 * 1600.0;
+ double psi = (v - 0.5) / 4.0 * 2500.0;
return AltosConvert.psi_to_pa(psi);
}
return AltosConvert.lb_to_n(v * 298 * 9.807);
}
- public void update_state(AltosState state) {
- super.update_state(state);
+ public void provide_data(AltosDataListener listener, AltosCalData cal_data) {
+ super.provide_data(listener, cal_data);
switch (cmd()) {
case AltosLib.AO_LOG_FLIGHT:
- state.set_flight(flight());
- state.set_ground_pressure(adc_to_pa(idle_pres()));
- state.set_accel_g(0, -1);
+ cal_data.set_flight(flight());
break;
case AltosLib.AO_LOG_STATE:
- state.set_state(state());
+ listener.set_state(state());
break;
case AltosLib.AO_LOG_SENSOR:
- state.set_pressure(adc_to_pa(pres()));
- state.set_accel(adc_to_n(thrust()));
+ listener.set_pressure(adc_to_pa(pres()));
+ listener.set_thrust(adc_to_n(thrust()));
break;
}
}