/* 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); }
switch (cmd()) {
case AltosLib.AO_LOG_FLIGHT:
state.set_flight(flight());
- state.set_ground_pressure(adc_to_pa(idle_pres()));
+ state.set_ground_pressure(0.0);
state.set_accel_g(0, -1);
break;
case AltosLib.AO_LOG_STATE: