def get_weights(self, closePoint, nodes):
# TODO: new weights?
#(n1, n2, n3) = list(setNodes)
#n = piercedPoint
#(w1, w2, w3) = getTriangleWeights(n, n1, n2, n3)
weights = shepard_weight(closePoint, nodes)
return weights
def map_deflections(self, deflections, aeroNode):
"""
determines the mapped x,y,z deflections of the aero node
deflections - deflections at p0,p1,p2,p3
aeroNode - node to find the deflections at
Solves Ax=b where A is the nodes, x is the abc coeffs,
b is the deflection at the tet node points (x,y,z)
then uses x to find the deflection at an arbitrary point m (aeroNode)
"""
A = array([[1.]+list(self.p0),
[1.]+list(self.p1),
[1.]+list(self.p2),
[1.]+list(self.p3)])
#print("m1 = ", m)
(d1, d2, d3, d4) = deflections
log.info('d1=%s' % d1)
log.info('d2=%s' % d2)
log.info('d3=%s' % d3)
log.info('d4=%s' % d4)
#log.info("A = \n%s" % (A))
#condA = cond(A,2)
#log.info("A cond=%g; A=\n%s" % (condA, printMatrix(A)))
#print("ID = ",self.ID)
#condMax = 1E6 # max allowable condition number before alternate approach
if 1:
nodes = [self.p0, self.p1, self.p2, self.p3]
weights = shepard_weight(aeroNode, nodes)
du = array([0.,0.,0.])
for (node, weight) in zip(nodes, weights):
du += weight * node
else:
ux = self.map_deflection(A, d1, d2, d3, d4, 0, aeroNode, 'x')
uy = self.map_deflection(A, d1, d2, d3, d4, 1, aeroNode, 'y')
uz = self.map_deflection(A, d1, d2, d3, d4, 2, aeroNode, 'z')
du = array([ux, uy, uz])
log.info("vol = %s" % self.volume())
log.info("du = %s" % du)
return aeroNode + du
def mapDeflections(self, deflections, aeroNode):
"""
determines the mapped x,y,z deflections of the aero node
deflections - deflections at p0,p1,p2,p3
aeroNode - node to find the deflections at
Solves Ax=b where A is the nodes, x is the abc coeffs,
b is the deflection at the tet node points (x,y,z)
then uses x to find the deflection at an arbitrary point m (aeroNode)
"""
A = array([[1.] + list(self.p0), [1.] + list(self.p1),
[1.] + list(self.p2), [1.] + list(self.p3)])
#print "m1 = ",m
(d1, d2, d3, d4) = deflections
log.info('d1=%s' % (d1))
log.info('d2=%s' % (d2))
log.info('d3=%s' % (d3))
log.info('d4=%s' % (d4))
#log.info("A = \n%s" %(A))
#condA = cond(A,2)
#log.info("A cond=%g; A=\n%s" %(condA,printMatrix(A)))
#print "ID = ",self.ID
#condMax = 1E6 # max allowable condition number before alternate approach
if 1:
nodes = [self.p0, self.p1, self.p2, self.p3]
weights = shepard_weight(aeroNode, nodes)
du = array([0., 0., 0.])
for (node, weight) in zip(nodes, weights):
du += weight * node
else:
ux = self.mapDeflection(A, d1, d2, d3, d4, 0, aeroNode, 'x')
uy = self.mapDeflection(A, d1, d2, d3, d4, 1, aeroNode, 'y')
uz = self.mapDeflection(A, d1, d2, d3, d4, 2, aeroNode, 'z')
du = array([ux, uy, uz])
log.info("vol = %s" % (self.volume()))
log.info("du = %s" % (du))
return aeroNode + du
