Source code for pyrocko.modelling.okada

# https://pyrocko.org - GPLv3
#
# The Pyrocko Developers, 21st Century
# ---|P------/S----------~Lg----------

import numpy as num
import logging

from pyrocko import moment_tensor as mt
from pyrocko.guts import Float, String, Timestamp, Int
from pyrocko.model import Location
from pyrocko.modelling import okada_ext
from pyrocko.util import get_threadpool_limits

guts_prefix = 'modelling'

logger = logging.getLogger(__name__)

d2r = num.pi/180.
r2d = 180./num.pi
km = 1e3


[docs]class AnalyticalSource(Location): ''' Base class for analytical source models. ''' name = String.T( optional=True, default='') time = Timestamp.T( default=0., help='Source origin time', optional=True) vr = Float.T( default=0., help='Rupture velocity [m/s]', optional=True) @property def northing(self): return self.north_shift @property def easting(self): return self.east_shift
[docs]class AnalyticalRectangularSource(AnalyticalSource): ''' Rectangular analytical source model. Coordinates on the source plane are with respect to the origin point given by `(lat, lon, east_shift, north_shift, depth)`. ''' strike = Float.T( default=0.0, help='Strike direction in [deg], measured clockwise from north.') dip = Float.T( default=90.0, help='Dip angle in [deg], measured downward from horizontal.') rake = Float.T( default=0.0, help='Rake angle in [deg], measured counter-clockwise from ' 'right-horizontal in on-plane view.') al1 = Float.T( default=0., help='Left edge source plane coordinate [m].') al2 = Float.T( default=0., help='Right edge source plane coordinate [m].') aw1 = Float.T( default=0., help='Lower edge source plane coordinate [m].') aw2 = Float.T( default=0., help='Upper edge source plane coordinate [m].') slip = Float.T( default=0., help='Slip on the rectangular source area [m].', optional=True) @property def length(self): return abs(-self.al1 + self.al2) @property def width(self): return abs(-self.aw1 + self.aw2) @property def area(self): return self.width * self.length
[docs]class OkadaSource(AnalyticalRectangularSource): ''' Rectangular Okada source model. ''' opening = Float.T( default=0., help='Opening of the plane in [m].', optional=True) poisson__ = Float.T( default=0.25, help='Poisson\'s ratio :math:`\\nu`.', optional=True) lamb__ = Float.T( help='First Lame\' s parameter :math:`\\lambda` [Pa].', optional=True) shearmod__ = Float.T( default=32.0e9, help='Shear modulus along the plane :math:`\\mu` [Pa].', optional=True) @property def poisson(self): ''' Calculation of Poisson\' s ratio :math:`\\nu` (if not given). The Poisson\' s ratio :math:`\\nu` can be calculated from the Lame parameters :math:`\\lambda` and :math:`\\mu` using :math:`\\nu = \\frac{\\lambda}{2(\\lambda + \\mu)}` (e.g. Mueller 2007). ''' if self.poisson__ is not None: return self.poisson__ if self.shearmod__ is None or self.lamb__ is None: raise ValueError('Shearmod and lambda are needed') return (self.lamb__) / (2. * (self.lamb__ + self.shearmod__)) @poisson.setter def poisson(self, poisson): self.poisson__ = poisson @property def lamb(self): ''' Calculation of first Lame\' s parameter (if not given). Poisson\' s ratio :math:`\\nu` and shear modulus :math:`\\mu` must be available. ''' if self.lamb__ is not None: return self.lamb__ if self.shearmod__ is None or self.poisson__ is None: raise ValueError('Shearmod and poisson ratio are needed') return ( 2. * self.poisson__ * self.shearmod__) / (1. - 2. * self.poisson__) @lamb.setter def lamb(self, lamb): self.lamb__ = lamb @property def shearmod(self): ''' Calculation of shear modulus :math:`\\mu` (if not given). Poisson ratio\' s :math:`\\nu` must be available. .. important :: We assume a perfect elastic solid with :math:`K=\\frac{5}{3}\\mu`. Through :math:`\\mu = \\frac{3K(1-2\\nu)}{2(1+\\nu)}` this leads to :math:`\\mu = \\frac{8(1+\\nu)}{1-2\\nu}`. ''' if self.shearmod__ is not None: return self.shearmod__ if self.poisson__ is None: raise ValueError('Poisson ratio is needed') return (8. * (1. + self.poisson__)) / (1. - 2. * self.poisson__) @shearmod.setter def shearmod(self, shearmod): self.shearmod__ = shearmod @property def seismic_moment(self): ''' Scalar Seismic moment :math:`M_0`. Code copied from Kite. It disregards the opening (as for now). We assume :math:`M_0 = mu A D`. .. important :: We assume a perfect elastic solid with :math:`K=\\frac{5}{3}\\mu`. Through :math:`\\mu = \\frac{3K(1-2\\nu)}{2(1+\\nu)}` this leads to :math:`\\mu = \\frac{8(1+\\nu)}{1-2\\nu}`. :return: Seismic moment release. :rtype: float ''' mu = self.shearmod disl = 0. if self.slip: disl = self.slip if self.opening: disl = (disl**2 + self.opening**2)**.5 return mu * self.area * disl @property def moment_magnitude(self): ''' Moment magnitude :math:`M_\\mathrm{w}` from seismic moment. We assume :math:`M_\\mathrm{w} = {\\frac{2}{3}}\\log_{10}(M_0) - 10.7`. :returns: Moment magnitude. :rtype: float ''' return mt.moment_to_magnitude(self.seismic_moment)
[docs] def source_patch(self): ''' Build source information array for okada_ext.okada input. :return: Source data as input for okada_ext.okada. :rtype: :py:class:`~numpy.ndarray`: ``(9, )`` ''' return num.array([ self.northing, self.easting, self.depth, self.strike, self.dip, self.al1, self.al2, self.aw1, self.aw2])
[docs] def source_disloc(self): ''' Build source dislocation for okada_ext.okada input. :return: Source dislocation data as input for okada_ext.okada :rtype: :py:class:`~numpy.ndarray`: ``(3, )`` ''' return num.array([ num.cos(self.rake * d2r) * self.slip, num.sin(self.rake * d2r) * self.slip, self.opening])
[docs] def discretize(self, nlength, nwidth, *args, **kwargs): ''' Discretize fault into rectilinear grid of fault patches. Fault orientation, slip and elastic parameters are passed to the sub-faults unchanged. :param nlength: Number of patches in strike direction. :type nlength: int :param nwidth: Number of patches in down-dip direction. :type nwidth: int :return: Discrete fault patches. :rtype: list of :py:class:`~pyrocko.modelling.okada.OkadaPatch` ''' assert nlength > 0 assert nwidth > 0 il = num.repeat(num.arange(nlength), nwidth) iw = num.tile(num.arange(nwidth), nlength) patch_length = self.length / nlength patch_width = self.width / nwidth al1 = -patch_length / 2. al2 = patch_length / 2. aw1 = -patch_width / 2. aw2 = patch_width / 2. source_points = num.zeros((nlength * nwidth, 3)) source_points[:, 0] = il * patch_length + patch_length / 2. source_points[:, 1] = iw * patch_width + patch_width / 2. source_points[:, 0] += self.al1 source_points[:, 1] -= self.aw2 rotmat = num.asarray( mt.euler_to_matrix(self.dip*d2r, self.strike*d2r, 0.)) source_points_rot = num.dot(rotmat.T, source_points.T).T source_points_rot[:, 0] += self.northing source_points_rot[:, 1] += self.easting source_points_rot[:, 2] += self.depth kwargs = { prop: getattr(self, prop) for prop in self.T.propnames if prop not in [ 'north_shift', 'east_shift', 'depth', 'al1', 'al2', 'aw1', 'aw2']} return ( [OkadaPatch( parent=self, ix=src_point[0], iy=src_point[1], north_shift=coord[0], east_shift=coord[1], depth=coord[2], al1=al1, al2=al2, aw1=aw1, aw2=aw2, **kwargs) for src_point, coord in zip(source_points, source_points_rot)], source_points)
[docs]class OkadaPatch(OkadaSource): ''' Okada source with additional 2D indexes for bookkeeping. ''' ix = Int.T(help='Relative index of the patch in x') iy = Int.T(help='Relative index of the patch in y') def __init__(self, parent=None, *args, **kwargs): OkadaSource.__init__(self, *args, **kwargs) self.parent = parent
[docs]def make_okada_coefficient_matrix( source_patches_list, pure_shear=False, rotate_sdn=True, nthreads=1, variant='normal'): ''' Build coefficient matrix for given fault patches. The boundary element method (BEM) for a discretized fault and the determination of the slip distribution from stress drop is based on the relation :math:`stress = coefmat \\cdot displ`. Here the coefficient matrix is built, based on the displacements from Okada's solution and their partial derivatives. :param source_patches_list: Source patches, to be used in BEM. :type source_patches_list: list of :py:class:`~pyrocko.modelling.okada.OkadaSource`. :param pure_shear: If ``True``, only shear forces are taken into account. :type pure_shear: optional, bool :param rotate_sdn: If ``True``, rotate to strike, dip, normal. :type rotate_sdn: optional, bool :param nthreads: Number of threads. :type nthreads: optional, int :return: Coefficient matrix for all source combinations. :rtype: :py:class:`~numpy.ndarray`: ``(len(source_patches_list) * 3, len(source_patches_list) * 3)`` ''' if variant == 'slow': return _make_okada_coefficient_matrix_slow( source_patches_list, pure_shear, rotate_sdn, nthreads) source_patches = num.array([ src.source_patch() for src in source_patches_list]) receiver_coords = source_patches[:, :3].copy() npoints = len(source_patches_list) if pure_shear: n_eq = 2 else: n_eq = 3 coefmat = num.zeros((npoints * 3, npoints * 3)) lambda_mean = num.mean([src.lamb for src in source_patches_list]) mu_mean = num.mean([src.shearmod for src in source_patches_list]) unit_disl = 1. disl_cases = { 'strikeslip': { 'slip': unit_disl, 'opening': 0., 'rake': 0.}, 'dipslip': { 'slip': unit_disl, 'opening': 0., 'rake': 90.}, 'tensileslip': { 'slip': 0., 'opening': unit_disl, 'rake': 0.} } diag_ind = [0, 4, 8] kron = num.zeros(9) kron[diag_ind] = 1. if variant == 'normal': kron = kron[num.newaxis, num.newaxis, :] else: kron = kron[num.newaxis, :] for idisl, case_type in enumerate([ 'strikeslip', 'dipslip', 'tensileslip'][:n_eq]): case = disl_cases[case_type] source_disl = num.array([ case['slip'] * num.cos(case['rake'] * d2r), case['slip'] * num.sin(case['rake'] * d2r), case['opening']]) if variant == 'normal': results = okada_ext.okada( source_patches, num.tile(source_disl, npoints).reshape(-1, 3), receiver_coords, lambda_mean, mu_mean, nthreads=nthreads, rotate_sdn=int(rotate_sdn), stack_sources=int(variant != 'normal')) eps = 0.5 * ( results[:, :, 3:] + results[:, :, (3, 6, 9, 4, 7, 10, 5, 8, 11)]) dilatation \ = eps[:, :, diag_ind].sum(axis=-1)[:, :, num.newaxis] stress_sdn = kron*lambda_mean*dilatation + 2.*mu_mean*eps coefmat[:, idisl::3] = stress_sdn[:, :, (2, 5, 8)]\ .reshape(-1, npoints*3).T else: for isrc, source in enumerate(source_patches): results = okada_ext.okada( source[num.newaxis, :], source_disl[num.newaxis, :], receiver_coords, lambda_mean, mu_mean, nthreads=nthreads, rotate_sdn=int(rotate_sdn)) eps = 0.5 * ( results[:, 3:] + results[:, (3, 6, 9, 4, 7, 10, 5, 8, 11)]) dilatation \ = num.sum(eps[:, diag_ind], axis=1)[:, num.newaxis] stress_sdn \ = kron * lambda_mean * dilatation+2. * mu_mean * eps coefmat[:, isrc*3 + idisl] \ = stress_sdn[:, (2, 5, 8)].ravel() if pure_shear: coefmat[2::3, :] = 0. return -coefmat / unit_disl
def _make_okada_coefficient_matrix_slow( source_patches_list, pure_shear=False, rotate_sdn=True, nthreads=1): source_patches = num.array([ src.source_patch() for src in source_patches_list]) receiver_coords = source_patches[:, :3].copy() npoints = len(source_patches_list) if pure_shear: n_eq = 2 else: n_eq = 3 coefmat = num.zeros((npoints * 3, npoints * 3)) def ned2sdn_rotmat(strike, dip): rotmat = mt.euler_to_matrix( (dip + 180.) * d2r, strike * d2r, 0.).A return rotmat lambda_mean = num.mean([src.lamb for src in source_patches_list]) shearmod_mean = num.mean([src.shearmod for src in source_patches_list]) unit_disl = 1. disl_cases = { 'strikeslip': { 'slip': unit_disl, 'opening': 0., 'rake': 0.}, 'dipslip': { 'slip': unit_disl, 'opening': 0., 'rake': 90.}, 'tensileslip': { 'slip': 0., 'opening': unit_disl, 'rake': 0.} } for idisl, case_type in enumerate([ 'strikeslip', 'dipslip', 'tensileslip'][:n_eq]): case = disl_cases[case_type] source_disl = num.array([ case['slip'] * num.cos(case['rake'] * d2r), case['slip'] * num.sin(case['rake'] * d2r), case['opening']]) for isource, source in enumerate(source_patches): results = okada_ext.okada( source[num.newaxis, :].copy(), source_disl[num.newaxis, :].copy(), receiver_coords, lambda_mean, shearmod_mean, nthreads=nthreads, rotate_sdn=int(rotate_sdn)) for irec in range(receiver_coords.shape[0]): eps = num.zeros((3, 3)) for m in range(3): for n in range(3): eps[m, n] = 0.5 * ( results[irec][m * 3 + n + 3] + results[irec][n * 3 + m + 3]) stress = num.zeros((3, 3)) dilatation = num.sum([eps[i, i] for i in range(3)]) for m, n in zip([0, 0, 0, 1, 1, 2], [0, 1, 2, 1, 2, 2]): if m == n: stress[m, n] = \ lambda_mean * \ dilatation + \ 2. * shearmod_mean * \ eps[m, n] else: stress[m, n] = \ 2. * shearmod_mean * \ eps[m, n] stress[n, m] = stress[m, n] normal = num.array([0., 0., -1.]) for isig in range(3): tension = num.sum(stress[isig, :] * normal) coefmat[irec * n_eq + isig, isource * n_eq + idisl] = \ tension / unit_disl return coefmat
[docs]def invert_fault_dislocations_bem( stress_field, coef_mat=None, source_list=None, pure_shear=False, epsilon=None, nthreads=1, **kwargs): ''' BEM least squares inversion to get fault dislocations given stress field. Follows least squares inversion approach by Menke (1989) to calculate dislocations on a fault with several segments from a given stress field. The coefficient matrix connecting stresses and displacements of the fault patches can either be specified by the user (``coef_mat``) or it is calculated using the solution of Okada (1992) for a rectangular fault in a homogeneous half space (``source_list``). :param stress_field: Stress change [Pa] for each source patch (as ``stress_field[isource, icomponent]`` where isource indexes the source patch and ``icomponent`` indexes component, ordered (strike, dip, tensile). :type stress_field: :py:class:`~numpy.ndarray`: ``(nsources, 3)`` :param coef_mat: Coefficient matrix connecting source patch dislocations and the stress field. :type coef_mat: optional, :py:class:`~numpy.ndarray`: ``(len(source_list) * 3, len(source_list) * 3)`` :param source_list: Source patches to be used for BEM. :type source_list: optional, list of :py:class:`~pyrocko.modelling.okada.OkadaSource` :param epsilon: If given, values in ``coef_mat`` smaller than ``epsilon`` are set to zero. :type epsilon: optional, float :param nthreads: Number of threads allowed. :type nthreads: int :return: Inverted displacements as ``displacements[isource, icomponent]`` where isource indexes the source patch and ``icomponent`` indexes component, ordered (strike, dip, tensile). :rtype: :py:class:`~numpy.ndarray`: ``(nsources, 3)`` ''' if source_list is not None and coef_mat is None: coef_mat = make_okada_coefficient_matrix( source_list, pure_shear=pure_shear, nthreads=nthreads, **kwargs) if epsilon is not None: coef_mat[coef_mat < epsilon] = 0. idx = num.arange(0, coef_mat.shape[0]) if pure_shear: idx = idx[idx % 3 != 2] coef_mat_in = coef_mat[idx, :][:, idx] disloc_est = num.zeros(coef_mat.shape[0]) if stress_field.ndim == 2: stress_field = stress_field.ravel() threadpool_limits = get_threadpool_limits() with threadpool_limits(limits=nthreads, user_api='blas'): try: disloc_est[idx] = num.linalg.multi_dot([ num.linalg.inv(num.dot(coef_mat_in.T, coef_mat_in)), coef_mat_in.T, stress_field[idx]]) except num.linalg.LinAlgError as e: logger.warning('Linear inversion failed!') logger.warning( 'coef_mat: %s\nstress_field: %s', coef_mat_in, stress_field[idx]) raise e return disloc_est.reshape(-1, 3)
__all__ = [ 'AnalyticalSource', 'AnalyticalRectangularSource', 'OkadaSource', 'OkadaPatch', 'make_okada_coefficient_matrix', 'invert_fault_dislocations_bem']