Use autotools, move altos to src subdir

Signed-off-by: Keith Packard <keithp@keithp.com>

1 files changed, 0 insertions, 192 deletions

diff --git a/make-altitude b/make-altitude
deleted file mode 100644
index ddfab5fc..00000000
--- a/make-altitude
+++ /dev/null
@@ -1,192 +0,0 @@
-#!/usr/bin/nickle -f
-/*
- * Pressure Sensor Model, version 1.1
- *
- * written by Holly Grimes
- *
- * Uses the International Standard Atmosphere as described in
- *   "A Quick Derivation relating altitude to air pressure" (version 1.03)
- *    from the Portland State Aerospace Society, except that the atmosphere
- *    is divided into layers with each layer having a different lapse rate.
- *
- * Lapse rate data for each layer was obtained from Wikipedia on Sept. 1, 2007
- *    at site <http://en.wikipedia.org/wiki/International_Standard_Atmosphere
- *
- * Height measurements use the local tangent plane.  The postive z-direction is up.
- *
- * All measurements are given in SI units (Kelvin, Pascal, meter, meters/second^2).
- *   The lapse rate is given in Kelvin/meter, the gas constant for air is given
- *   in Joules/(kilogram-Kelvin).
- */
-
-const real GRAVITATIONAL_ACCELERATION = -9.80665;
-const real AIR_GAS_CONSTANT = 287.053;
-const int NUMBER_OF_LAYERS = 7;
-const real MAXIMUM_ALTITUDE = 84852;
-const real MINIMUM_PRESSURE = 0.3734;
-const real LAYER0_BASE_TEMPERATURE = 288.15;
-const real LAYER0_BASE_PRESSURE = 101325;
-
-/* lapse rate and base altitude for each layer in the atmosphere */
-const real[NUMBER_OF_LAYERS] lapse_rate = {
-	-0.0065, 0.0, 0.001, 0.0028, 0.0, -0.0028, -0.002
-};
-const int[NUMBER_OF_LAYERS] base_altitude = {
-	0, 11000, 20000, 32000, 47000, 51000, 71000
-};
-
-
-/* outputs atmospheric pressure associated with the given altitude. altitudes
-   are measured with respect to the mean sea level */
-real altitude_to_pressure(real altitude) {
- 
-   real base_temperature = LAYER0_BASE_TEMPERATURE;
-   real base_pressure = LAYER0_BASE_PRESSURE;
-
-   real pressure;
-   real base; /* base for function to determine pressure */
-   real exponent; /* exponent for function to determine pressure */
-   int layer_number; /* identifies layer in the atmosphere */
-   int delta_z; /* difference between two altitudes */
-   
-   if (altitude > MAXIMUM_ALTITUDE) /* FIX ME: use sensor data to improve model */
-      return 0;
-
-   /* calculate the base temperature and pressure for the atmospheric layer
-      associated with the inputted altitude */
-   for(layer_number = 0; layer_number < NUMBER_OF_LAYERS - 1 && altitude > base_altitude[layer_number + 1]; layer_number++) {
-      delta_z = base_altitude[layer_number + 1] - base_altitude[layer_number];
-      if (lapse_rate[layer_number] == 0.0) {
-         exponent = GRAVITATIONAL_ACCELERATION * delta_z 
-              / AIR_GAS_CONSTANT / base_temperature;
-         base_pressure *= exp(exponent);
-      }
-      else {
-         base = (lapse_rate[layer_number] * delta_z / base_temperature) + 1.0;
-         exponent = GRAVITATIONAL_ACCELERATION / 
-              (AIR_GAS_CONSTANT * lapse_rate[layer_number]);
-         base_pressure *= pow(base, exponent);
-      }
-      base_temperature += delta_z * lapse_rate[layer_number];
-   }
-
-   /* calculate the pressure at the inputted altitude */
-   delta_z = altitude - base_altitude[layer_number];
-   if (lapse_rate[layer_number] == 0.0) {
-      exponent = GRAVITATIONAL_ACCELERATION * delta_z 
-           / AIR_GAS_CONSTANT / base_temperature;
-      pressure = base_pressure * exp(exponent);
-   }
-   else {
-      base = (lapse_rate[layer_number] * delta_z / base_temperature) + 1.0;
-      exponent = GRAVITATIONAL_ACCELERATION /
-           (AIR_GAS_CONSTANT * lapse_rate[layer_number]);
-      pressure = base_pressure * pow(base, exponent);
-   } 
-
-   return pressure;
-}
-
-
-/* outputs the altitude associated with the given pressure. the altitude
-   returned is measured with respect to the mean sea level */
-real pressure_to_altitude(real pressure) {
-
-   real next_base_temperature = LAYER0_BASE_TEMPERATURE;
-   real next_base_pressure = LAYER0_BASE_PRESSURE;
-
-   real altitude;
-   real base_pressure;
-   real base_temperature;
-   real base; /* base for function to determine base pressure of next layer */
-   real exponent; /* exponent for function to determine base pressure
-                             of next layer */
-   real coefficient;
-   int layer_number; /* identifies layer in the atmosphere */
-   int 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;
-
-   /* calculate the base temperature and pressure for the atmospheric layer
-      associated with the inputted pressure. */
-   layer_number = -1;
-   do {
-      layer_number++;
-      base_pressure = next_base_pressure;
-      base_temperature = next_base_temperature;
-      delta_z = base_altitude[layer_number + 1] - base_altitude[layer_number];
-      if (lapse_rate[layer_number] == 0.0) {
-         exponent = GRAVITATIONAL_ACCELERATION * delta_z 
-              / AIR_GAS_CONSTANT / base_temperature;
-         next_base_pressure *= exp(exponent);
-      }
-      else {
-         base = (lapse_rate[layer_number] * delta_z / base_temperature) + 1.0;
-         exponent = GRAVITATIONAL_ACCELERATION / 
-              (AIR_GAS_CONSTANT * lapse_rate[layer_number]);
-         next_base_pressure *= pow(base, exponent);
-      }
-      next_base_temperature += delta_z * lapse_rate[layer_number];
-   }
-   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 = (AIR_GAS_CONSTANT / GRAVITATIONAL_ACCELERATION) 
-                                                    * base_temperature;
-      altitude = base_altitude[layer_number]
-                    + coefficient * log(pressure / base_pressure);
-   }
-   else {
-      base = pressure / base_pressure;
-      exponent = AIR_GAS_CONSTANT * lapse_rate[layer_number] 
-                                       / GRAVITATIONAL_ACCELERATION;
-      coefficient = base_temperature / lapse_rate[layer_number];
-      altitude = base_altitude[layer_number]
-                      + coefficient * (pow(base, exponent) - 1);
-   }
-
-   return altitude;
-}
-
-real feet_to_meters(real feet)
-{
-    return feet * (12 * 2.54 / 100);
-}
-
-real meters_to_feet(real meters)
-{
-    return meters / (12 * 2.54 / 100);
-}
-
-/*
- * Values for our MP3H6115A pressure sensor
- *
- * From the data sheet:
- *
- * Pressure range: 15-115 kPa
- * Voltage at 115kPa: 2.82
- * Output scale: 27mV/kPa
- *
- * 
- * 27 mV/kPa * 2047 / 3300 counts/mV = 16.75 counts/kPa
- * 2.82V * 2047 / 3.3 counts/V = 1749 counts/115 kPa
- */
-
-real counts_per_kPa = 27 * 2047 / 3300;
-real counts_at_101_3kPa = 1674;
-
-real count_to_kPa(real count)
-{
-	return (count / 2047 + 0.095) / 0.009;
-}
-
-for (real count = 0; count <= 2047; count++) {
-	real	kPa = count_to_kPa(count);
-	real	meters = pressure_to_altitude(kPa * 1000);
-	printf ("	%d,	/* %6.2g kPa %d count */\n",
-		floor (meters + 0.5), kPa, count);
-}