def add_hwm_winds_and_ecef_vectors(inst,
glat_label='glat',
glong_label='glong',
alt_label='alt'):
"""
Uses HWM (Horizontal Wind Model) model to obtain neutral wind details.
Uses pyglow module to run HWM. Configured to use actual solar parameters to run
model.
Example
-------
# function added velow modifies the inst object upon every inst.load call
inst.custom.add(add_hwm_winds_and_ecef_vectors, 'modify', glat_label='custom_label')
Parameters
----------
inst : pysat.Instrument
Designed with pysat_sgp4 in mind
glat_label : string
label used in inst to identify WGS84 geodetic latitude (degrees)
glong_label : string
label used in inst to identify WGS84 geodetic longitude (degrees)
alt_label : string
label used in inst to identify WGS84 geodetic altitude (km, height above surface)
Returns
-------
inst
Input pysat.Instrument object modified to include HWM winds.
'zonal_wind' for the east/west winds (u in model) in m/s
'meiridional_wind' for the north/south winds (v in model) in m/s
'unit_zonal_wind_ecef_*' (*=x,y,z) is the zonal vector expressed in the ECEF basis
'unit_mer_wind_ecef_*' (*=x,y,z) is the meridional vector expressed in the ECEF basis
'sim_inst_wind_*' (*=x,y,z) is the projection of the total wind vector onto s/c basis
"""
import pyglow
import pysatMagVect
hwm_params = []
for time, lat, lon, alt in zip(inst.data.index, inst[glat_label],
inst[glong_label], inst[alt_label]):
# Point class is instantiated.
# Its parameters are a function of time and spatial location
pt = pyglow.Point(time, lat, lon, alt)
pt.run_hwm()
hwm = {}
hwm['zonal_wind'] = pt.u
hwm['meridional_wind'] = pt.v
hwm_params.append(hwm)
# print 'Complete.'
hwm = pds.DataFrame(hwm_params)
hwm.index = inst.data.index
inst[['zonal_wind',
'meridional_wind']] = hwm[['zonal_wind', 'meridional_wind']]
# calculate zonal unit vector in ECEF
# zonal wind: east - west; positive east
# EW direction is tangent to XY location of S/C in ECEF coordinates
mag = np.sqrt(inst['position_ecef_x']**2 + inst['position_ecef_y']**2)
inst['unit_zonal_wind_ecef_x'] = -inst['position_ecef_y'] / mag
inst['unit_zonal_wind_ecef_y'] = inst['position_ecef_x'] / mag
inst['unit_zonal_wind_ecef_z'] = 0 * inst['position_ecef_x']
# calculate meridional unit vector in ECEF
# meridional wind: north - south; positive north
# mer direction completes RHS of position and zonal vector
unit_pos_x, unit_pos_y, unit_pos_z = \
pysatMagVect.normalize_vector(-inst['position_ecef_x'], -inst['position_ecef_y'], -inst['position_ecef_z'])
# mer = r x zonal
inst['unit_mer_wind_ecef_x'], inst['unit_mer_wind_ecef_y'], inst['unit_mer_wind_ecef_z'] = \
pysatMagVect.cross_product(unit_pos_x, unit_pos_y, unit_pos_z,
inst['unit_zonal_wind_ecef_x'], inst['unit_zonal_wind_ecef_y'], inst['unit_zonal_wind_ecef_z'])
# Adding metadata information
inst.meta['zonal_wind'] = {
'units': 'm/s',
'long_name': 'Zonal Wind',
'desc': 'HWM model zonal wind'
}
inst.meta['meridional_wind'] = {
'units': 'm/s',
'long_name': 'Meridional Wind',
'desc': 'HWM model meridional wind'
}
inst.meta['unit_zonal_wind_ecef_x'] = {
'units': '',
'long_name': 'Zonal Wind Unit ECEF x-vector',
'desc': 'x-value of zonal wind unit vector in ECEF co ordinates'
}
inst.meta['unit_zonal_wind_ecef_y'] = {
'units': '',
'long_name': 'Zonal Wind Unit ECEF y-vector',
'desc': 'y-value of zonal wind unit vector in ECEF co ordinates'
}
inst.meta['unit_zonal_wind_ecef_z'] = {
'units': '',
'long_name': 'Zonal Wind Unit ECEF z-vector',
'desc': 'z-value of zonal wind unit vector in ECEF co ordinates'
}
inst.meta['unit_mer_wind_ecef_x'] = {
'units': '',
'long_name': 'Meridional Wind Unit ECEF x-vector',
'desc': 'x-value of meridional wind unit vector in ECEF co ordinates'
}
inst.meta['unit_mer_wind_ecef_y'] = {
'units': '',
'long_name': 'Meridional Wind Unit ECEF y-vector',
'desc': 'y-value of meridional wind unit vector in ECEF co ordinates'
}
inst.meta['unit_mer_wind_ecef_z'] = {
'units': '',
'long_name': 'Meridional Wind Unit ECEF z-vector',
'desc': 'z-value of meridional wind unit vector in ECEF co ordinates'
}
return
def add_sc_attitude_vectors(inst):
"""
Add attitude vectors for spacecraft assuming ram pointing.
Presumes spacecraft is pointed along the velocity vector (x), z is
generally nadir pointing (positive towards Earth), and y completes the
right handed system (generally southward).
Notes
-----
Expects velocity and position of spacecraft in Earth Centered
Earth Fixed (ECEF) coordinates to be in the instrument object
and named velocity_ecef_* (*=x,y,z) and position_ecef_* (*=x,y,z)
Adds attitude vectors for spacecraft in the ECEF basis by calculating the scalar
product of each attitude vector with each component of ECEF.
Parameters
----------
inst : pysat.Instrument
Instrument object
Returns
-------
None
Modifies pysat.Instrument object in place to include S/C attitude unit
vectors, expressed in ECEF basis. Vectors are named sc_(x,y,z)hat_ecef_(x,y,z).
sc_xhat_ecef_x is the spacecraft unit vector along x (positive along velocity vector)
reported in ECEF, ECEF x-component.
"""
import pysatMagVect
# ram pointing is along velocity vector
inst['sc_xhat_ecef_x'], inst['sc_xhat_ecef_y'], inst['sc_xhat_ecef_z'] = \
pysatMagVect.normalize_vector(inst['velocity_ecef_x'], inst['velocity_ecef_y'], inst['velocity_ecef_z'])
# begin with z along Nadir (towards Earth)
# if orbit isn't perfectly circular, then the s/c z vector won't
# point exactly along nadir. However, nadir pointing is close enough
# to the true z (in the orbital plane) that we can use it to get y,
# and use x and y to get the real z
inst['sc_zhat_ecef_x'], inst['sc_zhat_ecef_y'], inst['sc_zhat_ecef_z'] = \
pysatMagVect.normalize_vector(-inst['position_ecef_x'], -inst['position_ecef_y'], -inst['position_ecef_z'])
# get y vector assuming right hand rule
# Z x X = Y
inst['sc_yhat_ecef_x'], inst['sc_yhat_ecef_y'], inst['sc_yhat_ecef_z'] = \
pysatMagVect.cross_product(inst['sc_zhat_ecef_x'], inst['sc_zhat_ecef_y'], inst['sc_zhat_ecef_z'],
inst['sc_xhat_ecef_x'], inst['sc_xhat_ecef_y'], inst['sc_xhat_ecef_z'])
# normalize since Xhat and Zhat from above may not be orthogonal
inst['sc_yhat_ecef_x'], inst['sc_yhat_ecef_y'], inst['sc_yhat_ecef_z'] = \
pysatMagVect.normalize_vector(inst['sc_yhat_ecef_x'], inst['sc_yhat_ecef_y'], inst['sc_yhat_ecef_z'])
# strictly, need to recalculate Zhat so that it is consistent with RHS
# just created
# Z = X x Y
inst['sc_zhat_ecef_x'], inst['sc_zhat_ecef_y'], inst['sc_zhat_ecef_z'] = \
pysatMagVect.cross_product(inst['sc_xhat_ecef_x'], inst['sc_xhat_ecef_y'], inst['sc_xhat_ecef_z'],
inst['sc_yhat_ecef_x'], inst['sc_yhat_ecef_y'], inst['sc_yhat_ecef_z'])
# Adding metadata
inst.meta['sc_xhat_ecef_x'] = {
'units':
'',
'desc':
'S/C attitude (x-direction, ram) unit vector, expressed in ECEF basis, x-component'
}
inst.meta['sc_xhat_ecef_y'] = {
'units':
'',
'desc':
'S/C attitude (x-direction, ram) unit vector, expressed in ECEF basis, y-component'
}
inst.meta['sc_xhat_ecef_z'] = {
'units':
'',
'desc':
'S/C attitude (x-direction, ram) unit vector, expressed in ECEF basis, z-component'
}
inst.meta['sc_zhat_ecef_x'] = {
'units':
'',
'desc':
'S/C attitude (z-direction, generally nadir) unit vector, expressed in ECEF basis, x-component'
}
inst.meta['sc_zhat_ecef_y'] = {
'units':
'',
'desc':
'S/C attitude (z-direction, generally nadir) unit vector, expressed in ECEF basis, y-component'
}
inst.meta['sc_zhat_ecef_z'] = {
'units':
'',
'desc':
'S/C attitude (z-direction, generally nadir) unit vector, expressed in ECEF basis, z-component'
}
inst.meta['sc_yhat_ecef_x'] = {
'units':
'',
'desc':
'S/C attitude (y-direction, generally south) unit vector, expressed in ECEF basis, x-component'
}
inst.meta['sc_yhat_ecef_y'] = {
'units':
'',
'desc':
'S/C attitude (y-direction, generally south) unit vector, expressed in ECEF basis, y-component'
}
inst.meta['sc_yhat_ecef_z'] = {
'units':
'',
'desc':
'S/C attitude (y-direction, generally south) unit vector, expressed in ECEF basis, z-component'
}
# check what magnitudes we get
mag = np.sqrt(inst['sc_zhat_ecef_x']**2 + inst['sc_zhat_ecef_y']**2 +
inst['sc_zhat_ecef_z']**2)
idx, = np.where((mag < .999999999) | (mag > 1.000000001))
if len(idx) > 0:
print(mag[idx])
raise RuntimeError(
'Unit vector generation failure. Not sufficently orthogonal.')
return