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David Hoese authoredDavid Hoese authored
calc.py 4.06 KiB
import math
import numpy as np
try:
import pandas as pd
from pandas import Series
except ImportError:
# expected to use for isinstance
pd = None
Series = np.ndarray
NaN = float('nan')
is_nan = lambda a: a != a
def knots_to_mps(knots):
return knots * 0.51444
def dewpoint(tempC, relhum):
"""
Algorithm from Tom Whittaker tempC is the temperature in degrees Celsius,
relhum is the relative humidity as a percentage.
:param tempC: temperature in celsius
:param relhum: relative humidity as a percentage
"""
if tempC is None or relhum is None:
return NaN
gasconst = 461.5
latheat = 2500800.0
dp = 1.0 / (1.0 / (273.15 + tempC) - gasconst * np.log((0.0 + relhum) / 100) /
(latheat - tempC * 2397.5))
if pd is not None and isinstance(dp, pd.Series):
return pd.concat([dp - 273.15, tempC], axis=1).min(axis=1)
return np.min(dp - 273.15, tempC)
def relhum(airTempK, dewpointTempK):
"""
Algorithm derived by David Hoese from the above
dewpoint(tempC, relhum) function, both parameters are in Kelvin units.
:param airTempK: air temperature in Kelvin
:param dewpointTempK: dewpoint temp in Kelvin
"""
if airTempK == None or dewpointTempK == None:
return NaN
gas_constant = 461.5
latheat = 2500800.0
# Only one section of the equation
latpart = (latheat - (airTempK - 273.15) * 2397.5)
relativehum = 100 * math.e ** ((latpart / airTempK - latpart / dewpointTempK) / gas_constant)
return relativehum
def potentialtemp(airTempK, pressureMB):
"""
Algorithm from David Hoese to calculate potential temperature.
:param airTempK: air temperature in Kelvin
:param pressureMB: air pressure in millibars
"""
if airTempK == None or pressureMB == None:
return NaN
pT = airTempK * (pressureMB.max() / pressureMB) ** .286
return pT
def altimeter(p, alt):
"""Compute altimeter from pressure and altitude.
Converted from code provided by TomW.
:param p: pressure in hPa.
:param alt: altitude of the measurement in meters.
:returns: altimeter in inHg
"""
n = .190284
c1 = .0065 * pow(1013.25, n) / 288.
c2 = alt / pow((p - .3), n)
ff = pow(1. + c1 * c2, 1. / n)
return ((p - .3) * ff * 29.92 / 1013.25)
def dir2txt(val):
"""Convert degrees [0, 360) to a textual representation.
:param val: decimal degrees
>>> dir2txt(0)
'N'
>>> dir2txt(90)
'E'
>>> dir2txt(180)
'S'
>>> dir2txt(270)
'W'
>>> dir2txt(359)
'N'
"""
assert val >= 0 and val < 360, "'%s' out of range" % val
dirs = ("NNE", "NE", "ENE", "E", "ESE", "SE", "SSE", "S", "SSW", "SW", "WSW", "W", "WNW", "NW", "NNW")
if ((val >= 348.75 and val <= 360) or val >= 0 and val < 11.25): return "N"
# 1/2 degree increment between the directions
i = 11.25;
for dir in dirs:
if val >= i and val < (i + 22.5):
return dir
i += 22.5
def wind_vector_components(windspd, winddir):
"""Decompose scalar or list/array polar wind direction and speed data
into the horizontal and vertical vector components and speed vector.
Inputs can be scalar or arrays.
"""
dir_rad = np.deg2rad(winddir)
spd_arr = np.array(windspd)
V_e = spd_arr * np.sin(dir_rad)
V_n = spd_arr * np.cos(dir_rad)
U_spd = np.sqrt(pow(V_e, 2) + pow(V_n, 2))
return V_e, V_n, U_spd
def wind_vector_degrees(vector_east, vector_north):
"""Re-compose horizontal (east/west) and vertical (north/south) vector
components into wind direction in degrees.
Inputs can be scalar or arrays.
"""
rads = np.arctan2(vector_east, vector_north)
winddir = np.rad2deg(rads)
if isinstance(winddir, (np.ndarray, Series)):
winddir[np.less(winddir, 0)] += 360
elif winddir < 0:
winddir += 360
return winddir % 360
def mean_wind_vector(windspd, winddir):
V_e, V_n, V_spd = wind_vector_components(windspd, winddir)
avg_dir = wind_vector_degrees(np.mean(V_e), np.mean(V_n))
return avg_dir, np.mean(V_spd)