public class AltosInfoTable extends JTable implements AltosFlightDisplay, HierarchyListener {
private AltosFlightInfoTableModel model;
- static final int info_columns = 3;
- static final int info_rows = 17;
+ static final int info_columns = 4;
+ static final int info_rows = 18;
private AltosState last_state;
private AltosListenerState last_listener_state;
if (state.gps.lon != AltosLib.MISSING)
info_add_deg(1, "Longitude", state.gps.lon, 'E', 'W');
if (state.gps.alt != AltosLib.MISSING)
- info_add_row(1, "GPS altitude", "%8.1f", state.gps.alt);
+ info_add_row(1, "GPS altitude", "%8.1f m", state.gps.alt);
if (state.gps_height != AltosLib.MISSING)
- info_add_row(1, "GPS height", "%8.1f", state.gps_height);
+ info_add_row(1, "GPS height", "%8.1f m", state.gps_height);
if (state.gps.ground_speed != AltosLib.MISSING && state.gps.course != AltosLib.MISSING)
info_add_row(1, "GPS ground speed", "%6.1f m/s %3d°",
}
}
}
+
+ if (state != null && state.accel_along() != AltosLib.MISSING) {
+ info_add_row(3, "Accel along", "%8.1f m/s²", state.accel_along());
+ info_add_row(3, "Accel across", "%8.1f m/s²", state.accel_across());
+ info_add_row(3, "Accel through", "%8.1f m/s²", state.accel_through());
+ info_add_row(3, "Gyro roll", "%8.1f °/s", state.gyro_roll());
+ info_add_row(3, "Gyro pitch", "%8.1f °/s", state.gyro_pitch());
+ info_add_row(3, "Gyro yaw", "%8.1f °/s", state.gyro_yaw());
+ if (state.mag_along() != AltosLib.MISSING) {
+ /* Report mag in nanoteslas (1 G = 100000 nT (or γ)) */
+ info_add_row(3, "Mag along", "%8.1f γ", state.mag_along() * 100000.0);
+ info_add_row(3, "Mag across", "%8.1f γ", state.mag_across() * 100000.0);
+ info_add_row(3, "Mag Through", "%8.1f γ", state.mag_through() * 100000.0);
+ }
+ }
+
+ if (state != null && state.igniter_voltage != null) {
+ for (int i = 0; i < state.igniter_voltage.length; i++)
+ info_add_row(3, AltosLib.igniter_name(i), "%9.2f V", state.igniter_voltage[i]);
+ }
+
info_finish();
}
}