private static final double GRAVITATIONAL_ACCELERATION = -gravity;
private static final double AIR_GAS_CONSTANT = 287.053;
- private static final double NUMBER_OF_LAYERS = 7;
- private static final double MAXIMUM_ALTITUDE = 84852.0;
- private static final double MINIMUM_PRESSURE = 0.3734;
+ private static final double MAXIMUM_ALTITUDE = 100000.0;
+ private static final double MINIMUM_PRESSURE = 0.023439;
private static final double LAYER0_BASE_TEMPERATURE = 288.15;
private static final double LAYER0_BASE_PRESSURE = 101325;
/* lapse rate and base altitude for each layer in the atmosphere */
private static final double[] lapse_rate = {
- -0.0065, 0.0, 0.001, 0.0028, 0.0, -0.0028, -0.002
+ -0.0065, 0.0, 0.001, 0.0028, 0.0, -0.0028, -0.002, 0,
};
- private static final int[] base_altitude = {
- 0, 11000, 20000, 32000, 47000, 51000, 71000
+ private static final double[] base_altitude = {
+ 0, 11000, 20000, 32000, 47000, 51000, 71000, 84852,
};
+ private static final int NUMBER_OF_LAYERS = base_altitude.length;
/* outputs atmospheric pressure associated with the given altitude.
* altitudes are measured with respect to the mean sea level
*/
double next_base_pressure = LAYER0_BASE_PRESSURE;
double altitude;
- double base_pressure;
- double base_temperature;
+ double base_pressure = 0;
+ double base_temperature = 0;
double base; /* base for function to determine base pressure of next layer */
double exponent; /* exponent for function to determine base pressure
of next layer */
double coefficient;
int layer_number; /* identifies layer in the atmosphere */
- int delta_z; /* difference between two altitudes */
+ double delta_z; /* difference between two altitudes */
- if (pressure < 0) /* illegal pressure */
- return -1;
if (pressure < MINIMUM_PRESSURE) /* FIX ME: use sensor data to improve model */
- return MAXIMUM_ALTITUDE;
+ pressure = MINIMUM_PRESSURE;
/* calculate the base temperature and pressure for the atmospheric layer
associated with the inputted pressure. */
- layer_number = -1;
- do {
- layer_number++;
+ for (layer_number = 0; layer_number < NUMBER_OF_LAYERS - 1; layer_number++) {
base_pressure = next_base_pressure;
base_temperature = next_base_temperature;
delta_z = base_altitude[layer_number + 1] - base_altitude[layer_number];
next_base_pressure *= Math.pow(base, exponent);
}
next_base_temperature += delta_z * lapse_rate[layer_number];
+ if (pressure >= next_base_pressure)
+ break;
}
- while(layer_number < NUMBER_OF_LAYERS - 1 && pressure < next_base_pressure);
/* calculate the altitude associated with the inputted pressure */
if (lapse_rate[layer_number] == 0.0) {
+ coefficient * (Math.pow(base, exponent) - 1);
}
+ if (altitude > MAXIMUM_ALTITUDE)
+ altitude = MAXIMUM_ALTITUDE;
+
return altitude;
}