def finger_print_characteristic_collector(self):
collected_characteristics_vector = self.collected_burst
collected_labels = self.collected_labels
for key in self.converted_characteristic.keys():
self.converted_characteristic[key] = array(
self.converted_characteristic[key])
if size(self.converted_characteristic[key]) > 1:
self.converted_characteristic[key] = reshape(
self.converted_characteristic[key],
[size(self.converted_characteristic[key], 0), 1])
collected_characteristics_vector = row_stack(
(collected_characteristics_vector,
self.converted_characteristic[key]))
if size(collected_labels) == 0:
collected_labels = {
self.output_label_index: self.output_labels[key]
}
self.output_label_index += 1
else:
collected_labels[
self.output_label_index] = self.output_labels[key]
self.output_label_index += 1
return collected_characteristics_vector, collected_labels
def postProcessor_burst_collector(self):
# saving the whole burst in the data-bank
self.collected_burst = self.collected_burst[1:]
self.collected_burst = reshape(self.collected_burst,
size(self.collected_burst), 1)
if size(self.data_collection) == 0:
self.data_collection = self.collected_burst
else:
self.data_collection = column_stack(
(self.data_collection, self.collected_burst))
self.label_vector = column_stack(
(self.label_vector, self.device_label))
self.collected_burst = 0
def finger_print_burst_collector(self):
# saving the whole burst in the data-bank
self.collected_burst = self.collected_burst[1:]
self.collected_burst = reshape(self.collected_burst,
[size(self.collected_burst, 0), 1])
if size(self.data_collection) == 0:
self.data_collection = self.collected_burst
else:
self.data_collection = column_stack(
(self.data_collection, self.collected_burst))
self.label_vector = column_stack(
(self.label_vector, self.device_label))
self.collected_burst = 0
def power_mean_inner(p, mat, axis=0, dtype=None):
mat_cmplx = mat.astype(np.complex64 if dtype ==
np.float32 else np.complex128)
result_cmplx = np.power(
(np.power(mat_cmplx, p)).sum(axis=axis) / size(mat_cmplx, axis=axis),
1 / p)
return result_cmplx.real.astype(dtype)
def __init__(self, **parameters):
# TODO : check extra parameters dimensions consistancy if enumerates (must match layer height)
# initialize weights
weights = parameters.get(WeightParameters.WEIGHTS.value, None)
# randomize weights if necessary
if weights is None:
currentHeight = parameters.get(
WeightParameters.CURRENT_HEIGHT.value)
previousHeight = parameters.get(
WeightParameters.PREVIOUS_HEIGHT.value)
weightLimit = parameters.get(WeightParameters.WEIGHT_LIMIT.value)
# TODO : compute with spark 'weights'
weights = (rand(currentHeight, previousHeight) -
.5) * 2 * weightLimit
self.weights = weights
height = size(self.weights, 0)
# initialize meta parameters
metaParameters = MetaParameters.defaultValues()
# initialize meta parameters
for name in MetaParameters.enumerate():
value = parameters[name] if name in parameters else metaParameters[
name]
if not isinstance(value, Iterable):
value = [value] * height
metaParameters[name] = value
# set meta parameters has enumerates
for name, value in metaParameters.items():
setattr(self, name, value)
def variance(signal, special_parameters):
# TODO: this 'special_parameters' maybe be useful
signal = signal - mean(signal)
squared_signal = power(signal, 2)
summation = sum(squared_signal)
statistic = (1 / size(signal)) * summation
added_label = "var"
return statistic, added_label
def _pfromz_MA(z, lapse_rate, P_bott, T_bott, z_bott):
"""Pressure given altitude in a constant lapse rate layer.
The dry gas constant is used in calculations requiring the gas
constant. See the docstring for press2alt for references.
Input Arguments:
* z: Geopotential altitude [m].
* lapse_rate: -dT/dz [K/m] over the layer.
* P_bott: Pressure [hPa] at the base of the layer.
* T_bott: Temperature [K] at the base of the layer.
* z_bott: Geopotential altitude [m] of the base of the layer.
Output:
* Pressure [hPa] for each element given in the input arguments.
All input arguments can be either a scalar or an MA array. All
arguments that are MA arrays, however, are of the same size and
shape. If every input argument is a scalar, the output is a scalar.
If any of the input arguments is an MA array, the output is an MA
array of the same size and shape.
"""
#jfp was import Numeric as N
import numpy as N
#jfp was import MA
import numpy.ma as MA
from atmconst import AtmConst
const = AtmConst()
if MA.size(lapse_rate) == 1:
#jfp was if MA.array(lapse_rate)[0] == 0.0:
if MA.array(lapse_rate) == 0.0:
return P_bott * \
MA.exp( -const.g / (const.R_d*T_bott) * (z-z_bott) )
else:
exponent = const.g / (const.R_d * lapse_rate)
return P_bott * \
( (1.0 - (lapse_rate * (z-z_bott) / T_bott))**exponent )
else:
exponent = const.g / (const.R_d * lapse_rate)
P = P_bott * \
( (1.0 - (lapse_rate * (z-z_bott) / T_bott))**exponent )
P_at_0 = P_bott * \
MA.exp( -const.g / (const.R_d*T_bott) * (z-z_bott) )
zero_lapse_mask = MA.filled(MA.where(lapse_rate == 0., 1, 0), 0)
zero_lapse_mask_indices_flat = N.nonzero(N.ravel(zero_lapse_mask))
P_flat = MA.ravel(P)
MA.put( P_flat, zero_lapse_mask_indices_flat \
, MA.take(MA.ravel(P_at_0), zero_lapse_mask_indices_flat) )
return MA.reshape(P_flat, P.shape)
def _pfromz_MA(z, lapse_rate, P_bott, T_bott, z_bott):
"""Pressure given altitude in a constant lapse rate layer.
The dry gas constant is used in calculations requiring the gas
constant. See the docstring for press2alt for references.
Input Arguments:
* z: Geopotential altitude [m].
* lapse_rate: -dT/dz [K/m] over the layer.
* P_bott: Pressure [hPa] at the base of the layer.
* T_bott: Temperature [K] at the base of the layer.
* z_bott: Geopotential altitude [m] of the base of the layer.
Output:
* Pressure [hPa] for each element given in the input arguments.
All input arguments can be either a scalar or an MA array. All
arguments that are MA arrays, however, are of the same size and
shape. If every input argument is a scalar, the output is a scalar.
If any of the input arguments is an MA array, the output is an MA
array of the same size and shape.
"""
#jfp was import Numeric as N
import numpy as N
#jfp was import MA
import numpy.ma as MA
from atmconst import AtmConst
const = AtmConst()
if MA.size(lapse_rate) == 1:
#jfp was if MA.array(lapse_rate)[0] == 0.0:
if MA.array(lapse_rate) == 0.0:
return P_bott * \
MA.exp( -const.g / (const.R_d*T_bott) * (z-z_bott) )
else:
exponent = const.g / (const.R_d * lapse_rate)
return P_bott * \
( (1.0 - (lapse_rate * (z-z_bott) / T_bott))**exponent )
else:
exponent = const.g / (const.R_d * lapse_rate)
P = P_bott * \
( (1.0 - (lapse_rate * (z-z_bott) / T_bott))**exponent )
P_at_0 = P_bott * \
MA.exp( -const.g / (const.R_d*T_bott) * (z-z_bott) )
zero_lapse_mask = MA.filled(MA.where(lapse_rate == 0., 1, 0), 0)
zero_lapse_mask_indices_flat = N.nonzero(N.ravel(zero_lapse_mask))
P_flat = MA.ravel(P)
MA.put( P_flat, zero_lapse_mask_indices_flat \
, MA.take(MA.ravel(P_at_0), zero_lapse_mask_indices_flat) )
return MA.reshape(P_flat, P.shape)
def normalizer(data_bank, special_input, data_bank_structure):
# TODO: do sth with special_input
# data_bank: dimensions are in 'Rows'
for row_index in range(size(data_bank, 0) - 1):
current_dimension = data_bank[row_index, :]
current_dimension = (current_dimension - mean(current_dimension)) / \
(amax(current_dimension) - amin(current_dimension))
data_bank[row_index, :] = current_dimension
return data_bank
def _zfromp_MA(P, lapse_rate, P_bott, T_bott, z_bott):
"""Altitude given pressure in a constant lapse rate layer.
The dry gas constant is used in calculations requiring the gas
constant. See the docstring for press2alt for references.
Input Arguments:
* P: Pressure [hPa].
* lapse_rate: -dT/dz [K/m] over the layer.
* P_bott: Pressure [hPa] at the base of the layer.
* T_bott: Temperature [K] at the base of the layer.
* z_bott: Geopotential altitude [m] of the base of the layer.
Output:
* Altitude [m] for each element given in the input arguments.
All input arguments can be either a scalar or an MA array. All
arguments that are MA arrays, however, are of the same size and
shape. If every input argument is a scalar, the output is a scalar.
If any of the input arguments is an MA array, the output is an MA
array of the same size and shape.
"""
import numpy as N
#jfp was import Numeric as N
import numpy.ma as MA
#jfp was import MA
from atmconst import AtmConst
const = AtmConst()
if MA.size(lapse_rate) == 1:
if MA.array(lapse_rate)[0] == 0.0:
return ( (-const.R_d * T_bott / const.g) * MA.log(P/P_bott) ) + \
z_bott
else:
exponent = (const.R_d * lapse_rate) / const.g
return ((T_bott / lapse_rate) * (1. - (P/P_bott)**exponent)) + \
z_bott
else:
exponent = (const.R_d * lapse_rate) / const.g
z = ((T_bott / lapse_rate) * (1. - (P / P_bott)**exponent)) + z_bott
z_at_0 = ( (-const.R_d * T_bott / const.g) * MA.log(P/P_bott) ) + \
z_bott
zero_lapse_mask = MA.filled(MA.where(lapse_rate == 0., 1, 0), 0)
zero_lapse_mask_indices_flat = N.nonzero(N.ravel(zero_lapse_mask))
z_flat = MA.ravel(z)
MA.put( z_flat, zero_lapse_mask_indices_flat \
, MA.take(MA.ravel(z_at_0), zero_lapse_mask_indices_flat) )
return MA.reshape(z_flat, z.shape)
def _zfromp_MA(P, lapse_rate, P_bott, T_bott, z_bott):
"""Altitude given pressure in a constant lapse rate layer.
The dry gas constant is used in calculations requiring the gas
constant. See the docstring for press2alt for references.
Input Arguments:
* P: Pressure [hPa].
* lapse_rate: -dT/dz [K/m] over the layer.
* P_bott: Pressure [hPa] at the base of the layer.
* T_bott: Temperature [K] at the base of the layer.
* z_bott: Geopotential altitude [m] of the base of the layer.
Output:
* Altitude [m] for each element given in the input arguments.
All input arguments can be either a scalar or an MA array. All
arguments that are MA arrays, however, are of the same size and
shape. If every input argument is a scalar, the output is a scalar.
If any of the input arguments is an MA array, the output is an MA
array of the same size and shape.
"""
import numpy as N
#jfp was import Numeric as N
import numpy.ma as MA
#jfp was import MA
from atmconst import AtmConst
const = AtmConst()
if MA.size(lapse_rate) == 1:
if MA.array(lapse_rate)[0] == 0.0:
return ( (-const.R_d * T_bott / const.g) * MA.log(P/P_bott) ) + \
z_bott
else:
exponent = (const.R_d * lapse_rate) / const.g
return ((T_bott / lapse_rate) * (1. - (P/P_bott)**exponent)) + \
z_bott
else:
exponent = (const.R_d * lapse_rate) / const.g
z = ((T_bott / lapse_rate) * (1. - (P/P_bott)**exponent)) + z_bott
z_at_0 = ( (-const.R_d * T_bott / const.g) * MA.log(P/P_bott) ) + \
z_bott
zero_lapse_mask = MA.filled(MA.where(lapse_rate == 0., 1, 0), 0)
zero_lapse_mask_indices_flat = N.nonzero(N.ravel(zero_lapse_mask))
z_flat = MA.ravel(z)
MA.put( z_flat, zero_lapse_mask_indices_flat \
, MA.take(MA.ravel(z_at_0), zero_lapse_mask_indices_flat) )
return MA.reshape(z_flat, z.shape)
def preProcessor_device_collector(self):
if size(self.data_collection) == 0:
self.data_collection = {}
self.data_collection[self.device_key] = self.device_collection
def press2alt(arg, P0=None, T0=None, missing=1e+20, invert=0):
"""Calculate elevation given pressure (or vice versa).
Calculations are made assuming that the temperature distribution
follows the 1976 Standard Atmosphere. Technically the standard
atmosphere defines temperature distribution as a function of
geopotential altitude, and this routine actually calculates geo-
potential altitude rather than geometric altitude.
Method Positional Argument:
* arg: Numeric floating point vector of any shape and size, or a
Numeric floating point scalar. If invert=0 (the default), arg
is air pressure [hPa]. If invert=1, arg is elevation [m].
Method Keyword Arguments:
* P0: Pressure [hPa] at the surface (altitude equals 0). Numeric
floating point vector of same size and shape as arg or a scalar.
Default of keyword is set to None, in which case the routine
uses the value of instance attribute sea_level_press (converted
to hPa) from the AtmConst class. Keyword value is used if the
keyword is set in the function call. This keyword cannot have
any missing values.
* T0: Temperature [K] at the surface (altitude equals 0). Numeric
floating point vector of same size and shape as arg or a scalar.
Default of keyword is set to None, in which case the routine uses
the value of instance attribute sea_level_temp from the AtmConst
class. Keyword value is used if the keyword is set in the func-
tion call. This keyword cannot have any missing values.
* missing: If arg has missing values, this is the missing value
value. Floating point scalar. Default is 1e+20.
* invert: If set to 1, function calculates pressure [hPa] from
altitude [m]. In that case, positional input variable arg is
altitude [m] and the output is pressure [hPa]. Default value of
invert=0, which means the function calculates altitude given
pressure.
Output:
* If invert=0 (the default), output is elevation [m] at each
element of arg, relative to the surface. If invert=1, output
is the air pressure [hPa]. Numeric floating point array of
the same size and shape as arg.
If there are any missing values in output, those values are set
to the value in argument missing from the input. If there are
missing values in the output due to math errors and missing is
set to None, output will fill those missing values with the MA
default value of 1e+20.
References:
* Carmichael, Ralph (2003): "Definition of the 1976 Standard Atmo-
sphere to 86 km," Public Domain Aeronautical Software (PDAS).
URL: http://www.pdas.com/coesa.htm.
* Wallace, J. M., and P. V. Hobbs (1977): Atmospheric Science:
An Introductory Survey. San Diego, CA: Academic Press, ISBN
0-12-732950-1, pp. 60-61.
Examples:
(1) Calculating altitude given pressure:
>>> from press2alt import press2alt
>>> import Numeric as N
>>> press = N.array([200., 350., 850., 1e+20, 50.])
>>> alt = press2alt(press, missing=1e+20)
>>> ['%.7g' % alt[i] for i in range(5)]
['11783.94', '8117.19', '1457.285', '1e+20', '20575.96']
(2) Calculating pressure given altitude:
>>> alt = N.array([0., 10000., 15000., 20000., 50000.])
>>> press = press2alt(alt, missing=1e+20, invert=1)
>>> ['%.7g' % press[i] for i in range(5)]
['1013.25', '264.3589', '120.443', '54.74718', '0.7593892']
(3) Input is a Numeric floating point scalar, and using a keyword
set surface pressure to a different scalar:
>>> alt = press2alt(N.array(850.), P0=1000.)
>>> ['%.7g' % alt[0]]
['1349.778']
"""
import numpy.ma as MA
import numpy as N
from atmconst import AtmConst
#from is_numeric_float import is_numeric_float
#- Check input is of the correct type:
#if is_numeric_float(arg) != 1:
# raise TypeError, "press2alt: Arg not Numeric floating"
#- Import general constants and set additional constants. h1_std
# is the lower limit of the Standard Atmosphere layer geopoten-
# tial altitude [m], h2_std is the upper limit [m] of the layer,
# and dT/dh is the temperature gradient (i.e. negative of the
# lapse rate) [K/m]:
const = AtmConst()
h1_std = N.array([0., 11., 20., 32., 47., 51., 71.]) * 1000.
h2_std = N.array(MA.concatenate([h1_std[1:], [84.852 * 1000.]]))
dTdh_std = N.array([-6.5, 0.0, 1.0, 2.8, 0.0, -2.8, -2.0]) / 1000.
#- Prep arrays for masked array calculation and set conditions
# at sea-level. Pressures are in hPa and temperatures in K.
# Sea-level conditions arrays are same shape/size as P_or_z.
# If input argument is a scalar, make the local variable used
# for calculations a 1-element vector:
if missing == None: P_or_z = MA.masked_array(arg)
else: P_or_z = MA.masked_values(arg, missing, copy=0)
if P_or_z.shape == ():
P_or_z = MA.reshape(P_or_z, (1, ))
if P0 == None:
P0_use = MA.zeros(P_or_z.shape) \
+ (const.sea_level_press / 100.)
else:
P0_use = MA.zeros(P_or_z.shape) \
+ MA.masked_array(P0)
if T0 == None:
T0_use = MA.zeros(P_or_z.shape) \
+ const.sea_level_temp
else:
T0_use = MA.zeros(P_or_z.shape) \
+ MA.masked_array(T0)
#- Calculate P and T for the boundaries of the 7 layers of the
# Standard Atmosphere for the given P0 and T0 (layer 0 goes from
# P0 to P1, layer 1 from P1 to P2, etc.). These are given as
# 8 element dictionaries P_std and T_std where the key is the
# location (P_std[0] is at the bottom of layer 0, P_std[1] is the
# top of layer 0 and bottom of layer 1, ... and P_std[7] is the
# top of layer 6). Remember P_std and T_std are dictionaries but
# dTdh_std, h1_std, and h2_std are vectors:
P_std = {0: P0_use}
T_std = {0: T0_use}
for i in range(len(h1_std)):
P_std[i+1] = _pfromz_MA( h2_std[i], -dTdh_std[i] \
, P_std[i], T_std[i], h1_std[i] )
T_std[i + 1] = T_std[i] + (dTdh_std[i] * (h2_std[i] - h1_std[i]))
#- Test input is within Standard Atmosphere limits:
if invert == 0:
tmp = MA.where(P_or_z < P_std[len(h1_std)], 1, 0)
if MA.sum(MA.ravel(tmp)) > 0:
raise ValueError, "press2alt: Pressure out-of-range"
else:
tmp = MA.where(P_or_z > MA.maximum(h2_std), 1, 0)
if MA.sum(MA.ravel(tmp)) > 0:
raise ValueError, "press2alt: Altitude out-of-range"
#- What layer number is each element of P_or_z in?
P_or_z_layer = 0 #MA.zeros(P_or_z.shape)
#if invert == 0:
# for i in range(len(h1_std)):
# tmp = MA.where( MA.logical_and( (P_or_z <= P_std[i]) \
# , (P_or_z > P_std[i+1]) ) \
# , i, 0 )
# P_or_z_layer += tmp
#else:
# for i in range(len(h1_std)):
# tmp = MA.where( MA.logical_and( (P_or_z >= h1_std[i]) \
# , (P_or_z < h2_std[i]) ) \
# , i, 0 )
# P_or_z_layer += tmp
#- Fill in the bottom-of-the-layer variables and the lapse rate
# for the layers that the levels are in. The *_actual variables
# are the values of dTdh, P_bott, etc. for each element in the
# P_or_z_flat array:
P_or_z_flat = MA.ravel(P_or_z)
if P_or_z_flat.mask() == None:
P_or_z_flat_mask = MA.make_mask_none(P_or_z_flat.shape)
else:
P_or_z_flat_mask = P_or_z_flat.mask()
P_or_z_layer_flat = MA.ravel(P_or_z_layer)
dTdh_actual = MA.zeros(P_or_z_flat.shape)
P_bott_actual = MA.zeros(P_or_z_flat.shape)
T_bott_actual = MA.zeros(P_or_z_flat.shape)
z_bott_actual = MA.zeros(P_or_z_flat.shape)
for i in xrange(MA.size(P_or_z_flat)):
if P_or_z_flat_mask[i] != 1:
layer_number = P_or_z_layer_flat[i]
dTdh_actual[i] = dTdh_std[layer_number]
P_bott_actual[i] = MA.ravel(P_std[layer_number])[i]
T_bott_actual[i] = MA.ravel(T_std[layer_number])[i]
z_bott_actual[i] = h1_std[layer_number]
else:
dTdh_actual[i] = MA.masked
P_bott_actual[i] = MA.masked
T_bott_actual[i] = MA.masked
z_bott_actual[i] = MA.masked
#- Calculate pressure/altitude from altitude/pressure (output is
# a flat array):
if invert == 0:
output = _zfromp_MA( P_or_z_flat, -dTdh_actual \
, P_bott_actual, T_bott_actual, z_bott_actual )
else:
output = _pfromz_MA( P_or_z_flat, -dTdh_actual \
, P_bott_actual, T_bott_actual, z_bott_actual )
#- Return output as same shape as input positional argument:
return MA.filled(MA.reshape(output, arg.shape), missing)
def press2alt(arg, P0=None, T0=None, missing=1e+20, invert=0):
"""Calculate elevation given pressure (or vice versa).
Calculations are made assuming that the temperature distribution
follows the 1976 Standard Atmosphere. Technically the standard
atmosphere defines temperature distribution as a function of
geopotential altitude, and this routine actually calculates geo-
potential altitude rather than geometric altitude.
Method Positional Argument:
* arg: Numeric floating point vector of any shape and size, or a
Numeric floating point scalar. If invert=0 (the default), arg
is air pressure [hPa]. If invert=1, arg is elevation [m].
Method Keyword Arguments:
* P0: Pressure [hPa] at the surface (altitude equals 0). Numeric
floating point vector of same size and shape as arg or a scalar.
Default of keyword is set to None, in which case the routine
uses the value of instance attribute sea_level_press (converted
to hPa) from the AtmConst class. Keyword value is used if the
keyword is set in the function call. This keyword cannot have
any missing values.
* T0: Temperature [K] at the surface (altitude equals 0). Numeric
floating point vector of same size and shape as arg or a scalar.
Default of keyword is set to None, in which case the routine uses
the value of instance attribute sea_level_temp from the AtmConst
class. Keyword value is used if the keyword is set in the func-
tion call. This keyword cannot have any missing values.
* missing: If arg has missing values, this is the missing value
value. Floating point scalar. Default is 1e+20.
* invert: If set to 1, function calculates pressure [hPa] from
altitude [m]. In that case, positional input variable arg is
altitude [m] and the output is pressure [hPa]. Default value of
invert=0, which means the function calculates altitude given
pressure.
Output:
* If invert=0 (the default), output is elevation [m] at each
element of arg, relative to the surface. If invert=1, output
is the air pressure [hPa]. Numeric floating point array of
the same size and shape as arg.
If there are any missing values in output, those values are set
to the value in argument missing from the input. If there are
missing values in the output due to math errors and missing is
set to None, output will fill those missing values with the MA
default value of 1e+20.
References:
* Carmichael, Ralph (2003): "Definition of the 1976 Standard Atmo-
sphere to 86 km," Public Domain Aeronautical Software (PDAS).
URL: http://www.pdas.com/coesa.htm.
* Wallace, J. M., and P. V. Hobbs (1977): Atmospheric Science:
An Introductory Survey. San Diego, CA: Academic Press, ISBN
0-12-732950-1, pp. 60-61.
Examples:
(1) Calculating altitude given pressure:
>>> from press2alt import press2alt
>>> import Numeric as N
>>> press = N.array([200., 350., 850., 1e+20, 50.])
>>> alt = press2alt(press, missing=1e+20)
>>> ['%.7g' % alt[i] for i in range(5)]
['11783.94', '8117.19', '1457.285', '1e+20', '20575.96']
(2) Calculating pressure given altitude:
>>> alt = N.array([0., 10000., 15000., 20000., 50000.])
>>> press = press2alt(alt, missing=1e+20, invert=1)
>>> ['%.7g' % press[i] for i in range(5)]
['1013.25', '264.3589', '120.443', '54.74718', '0.7593892']
(3) Input is a Numeric floating point scalar, and using a keyword
set surface pressure to a different scalar:
>>> alt = press2alt(N.array(850.), P0=1000.)
>>> ['%.7g' % alt[0]]
['1349.778']
"""
import numpy as N
import numpy.ma as MA
#jfp was import MA
#jfp was import Numeric as N
from atmconst import AtmConst
from is_numeric_float import is_numeric_float
#- Check input is of the correct type:
if is_numeric_float(arg) != 1:
raise TypeError, "press2alt: Arg not Numeric floating"
#- Import general constants and set additional constants. h1_std
# is the lower limit of the Standard Atmosphere layer geopoten-
# tial altitude [m], h2_std is the upper limit [m] of the layer,
# and dT/dh is the temperature gradient (i.e. negative of the
# lapse rate) [K/m]:
const = AtmConst()
h1_std = N.array([0., 11., 20., 32., 47., 51., 71.]) * 1000.
h2_std = N.array( MA.concatenate([h1_std[1:], [84.852*1000.]]) )
dTdh_std = N.array([-6.5, 0.0, 1.0, 2.8, 0.0, -2.8, -2.0]) / 1000.
#- Prep arrays for masked array calculation and set conditions
# at sea-level. Pressures are in hPa and temperatures in K.
# Sea-level conditions arrays are same shape/size as P_or_z.
# If input argument is a scalar, make the local variable used
# for calculations a 1-element vector:
if missing == None: P_or_z = MA.masked_array(arg)
else: P_or_z = MA.masked_values(arg, missing, copy=0)
if P_or_z.shape == ():
P_or_z = MA.reshape(P_or_z, (1,))
if P0 == None:
#jfp was P0_use = MA.zeros(P_or_z.shape, typecode=MA.Float) \
P0_use = MA.zeros(P_or_z.shape) \
+ (const.sea_level_press / 100.)
else:
#jfp was P0_use = MA.zeros(P_or_z.shape, typecode=MA.Float) \
P0_use = MA.zeros(P_or_z.shape) \
+ MA.masked_array(P0)
if T0 == None:
#jfp was T0_use = MA.zeros(P_or_z.shape, typecode=MA.Float) \
T0_use = MA.zeros(P_or_z.shape) \
+ const.sea_level_temp
else:
#jfp was T0_use = MA.zeros(P_or_z.shape, typecode=MA.Float) \
T0_use = MA.zeros(P_or_z.shape) \
+ MA.masked_array(T0)
#- Calculate P and T for the boundaries of the 7 layers of the
# Standard Atmosphere for the given P0 and T0 (layer 0 goes from
# P0 to P1, layer 1 from P1 to P2, etc.). These are given as
# 8 element dictionaries P_std and T_std where the key is the
# location (P_std[0] is at the bottom of layer 0, P_std[1] is the
# top of layer 0 and bottom of layer 1, ... and P_std[7] is the
# top of layer 6). Remember P_std and T_std are dictionaries but
# dTdh_std, h1_std, and h2_std are vectors:
P_std = {0:P0_use}
T_std = {0:T0_use}
for i in range(len(h1_std)):
P_std[i+1] = _pfromz_MA( h2_std[i], -dTdh_std[i] \
, P_std[i], T_std[i], h1_std[i] )
T_std[i+1] = T_std[i] + ( dTdh_std[i] * (h2_std[i]-h1_std[i]) )
#- Test input is within Standard Atmosphere limits:
if invert == 0:
tmp = MA.where(P_or_z < P_std[len(h1_std)], 1, 0)
if MA.sum(MA.ravel(tmp)) > 0:
raise ValueError, "press2alt: Pressure out-of-range"
else:
tmp = MA.where(P_or_z > MA.maximum(h2_std), 1, 0)
if MA.sum(MA.ravel(tmp)) > 0:
raise ValueError, "press2alt: Altitude out-of-range"
#- What layer number is each element of P_or_z in?
P_or_z_layer = MA.zeros(P_or_z.shape)
if invert == 0:
for i in range(len(h1_std)):
tmp = MA.where( MA.logical_and( (P_or_z <= P_std[i]) \
, (P_or_z > P_std[i+1]) ) \
, i, 0 )
P_or_z_layer += tmp
else:
for i in range(len(h1_std)):
tmp = MA.where( MA.logical_and( (P_or_z >= h1_std[i]) \
, (P_or_z < h2_std[i]) ) \
, i, 0 )
P_or_z_layer += tmp
#- Fill in the bottom-of-the-layer variables and the lapse rate
# for the layers that the levels are in. The *_actual variables
# are the values of dTdh, P_bott, etc. for each element in the
# P_or_z_flat array:
P_or_z_flat = MA.ravel(P_or_z)
P_or_z_flat_mask = P_or_z_flat.mask
if P_or_z_flat.mask==False:
P_or_z_flat_mask = MA.make_mask_none(P_or_z_flat.shape)
#jfp was:
#if P_or_z_flat.mask() == None:
# P_or_z_flat_mask = MA.make_mask_none(P_or_z_flat.shape)
#else:
# P_or_z_flat_mask = P_or_z_flat.mask()
P_or_z_layer_flat = MA.ravel(P_or_z_layer)
#jfp was dTdh_actual = MA.zeros(P_or_z_flat.shape, typecode=MA.Float)
#jfp was P_bott_actual = MA.zeros(P_or_z_flat.shape, typecode=MA.Float)
#jfp was T_bott_actual = MA.zeros(P_or_z_flat.shape, typecode=MA.Float)
#jfp was z_bott_actual = MA.zeros(P_or_z_flat.shape, typecode=MA.Float)
dTdh_actual = MA.zeros(P_or_z_flat.shape)
P_bott_actual = MA.zeros(P_or_z_flat.shape)
T_bott_actual = MA.zeros(P_or_z_flat.shape)
z_bott_actual = MA.zeros(P_or_z_flat.shape)
for i in xrange(MA.size(P_or_z_flat)):
if P_or_z_flat_mask[i] != 1:
layer_number = P_or_z_layer_flat[i]
dTdh_actual[i] = dTdh_std[layer_number]
P_bott_actual[i] = MA.ravel(P_std[layer_number])[i]
T_bott_actual[i] = MA.ravel(T_std[layer_number])[i]
z_bott_actual[i] = h1_std[layer_number]
else:
dTdh_actual[i] = MA.masked
P_bott_actual[i] = MA.masked
T_bott_actual[i] = MA.masked
z_bott_actual[i] = MA.masked
#- Calculate pressure/altitude from altitude/pressure (output is
# a flat array):
if invert == 0:
output = _zfromp_MA( P_or_z_flat, -dTdh_actual \
, P_bott_actual, T_bott_actual, z_bott_actual )
else:
output = _pfromz_MA( P_or_z_flat, -dTdh_actual \
, P_bott_actual, T_bott_actual, z_bott_actual )
#- Return output as same shape as input positional argument:
return MA.filled( MA.reshape(output, arg.shape), missing )
