static final private AltosUILineStyle mag_through_color = new AltosUILineStyle();
static final private AltosUILineStyle mag_total_color = new AltosUILineStyle();
+ static final private AltosUILineStyle motor_pressure_color = new AltosUILineStyle();
+
static AltosUnits dop_units = null;
static AltosUnits tick_units = null;
AltosUIFlightSeries flight_series;
+ boolean enable_axis(int product_id, String label) {
+ switch (product_id) {
+ case AltosLib.product_easymotor:
+ return(label.equals(AltosUIFlightSeries.motor_pressure_name) ||
+ label.equals(AltosUIFlightSeries.accel_name));
+ default:
+ return true;
+ }
+ }
+
AltosUITimeSeries[] setup(AltosFlightStats stats, AltosUIFlightSeries flight_series) {
AltosCalData cal_data = flight_series.cal_data();
+ int product_id = cal_data.device_type;
AltosUIAxis height_axis, speed_axis, accel_axis, voltage_axis, temperature_axis, nsat_axis, dbm_axis;
AltosUIAxis pressure_axis, thrust_axis;
AltosUIAxis gyro_axis, orient_axis, mag_axis;
AltosUIAxis course_axis, dop_axis, tick_axis;
+ AltosUIAxis motor_pressure_axis;
if (stats != null && stats.serial != AltosLib.MISSING && stats.product != null && stats.flight != AltosLib.MISSING)
setName(String.format("%s %d flight %d\n", stats.product, stats.serial, stats.flight));
course_axis = newAxis("Course", AltosConvert.orient, gps_course_color, 0);
dop_axis = newAxis("Dilution of Precision", dop_units, gps_pdop_color, 0);
+ motor_pressure_axis = newAxis("Motor Pressure", AltosConvert.pressure, motor_pressure_color, 0);
+
flight_series.register_axis("default",
speed_color,
false,
flight_series.register_marker(AltosUIFlightSeries.state_name,
state_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.state_name),
plot,
true);
flight_series.register_axis(AltosUIFlightSeries.accel_name,
accel_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.accel_name),
accel_axis);
flight_series.register_axis(AltosUIFlightSeries.vert_accel_name,
vert_accel_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.vert_accel_name),
accel_axis);
flight_series.register_axis(AltosUIFlightSeries.kalman_accel_name,
flight_series.register_axis(AltosUIFlightSeries.speed_name,
speed_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.speed_name),
speed_axis);
flight_series.register_axis(AltosUIFlightSeries.kalman_speed_name,
kalman_speed_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.kalman_speed_name),
speed_axis);
flight_series.register_axis(AltosUIFlightSeries.pressure_name,
flight_series.register_axis(AltosUIFlightSeries.height_name,
height_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.height_name),
height_axis);
flight_series.register_axis(AltosUIFlightSeries.altitude_name,
flight_series.register_axis(AltosUIFlightSeries.thrust_name,
accel_color,
- true,
+ enable_axis(product_id, AltosUIFlightSeries.thrust_name),
thrust_axis);
for (int channel = 0; channel < 8; channel++) {
voltage_axis);
}
+ flight_series.register_axis(AltosUIFlightSeries.motor_pressure_name,
+ motor_pressure_color,
+ enable_axis(product_id, AltosUIFlightSeries.motor_pressure_name),
+ motor_pressure_axis);
+
flight_series.check_axes();
return flight_series.series(cal_data);