from sympy import Symbol, symbols, S
from sympy.physics.continuum_mechanics.beam import Beam
from sympy.functions import SingularityFunction, Piecewise, meijerg, Abs, log
from sympy.utilities.pytest import raises
from sympy.physics.units import meter, newton, kilo, giga, milli
from sympy.physics.continuum_mechanics.beam import Beam3D

x = Symbol('x')
y = Symbol('y')
R1, R2 = symbols('R1, R2')


def test_Beam():
    E = Symbol('E')
    E_1 = Symbol('E_1')
    I = Symbol('I')
    I_1 = Symbol('I_1')
    b = Beam(1, E, I)
    assert b.length == 1
    assert b.elastic_modulus == E
    assert b.second_moment == I
    assert b.variable == x

    # Test the length setter
    b.length = 4
    assert b.length == 4

    # Test the E setter
    b.elastic_modulus = E_1
    assert b.elastic_modulus == E_1

    # Test the I setter
    b.second_moment = I_1
    assert b.second_moment is I_1

    # Test the variable setter
    b.variable = y
    assert b.variable is y

    # Test for all boundary conditions.
    b.bc_deflection = [(0, 2)]
    b.bc_slope = [(0, 1)]
    assert b.boundary_conditions == {'deflection': [(0, 2)], 'slope': [(0, 1)]}

    # Test for slope boundary condition method
    b.bc_slope.extend([(4, 3), (5, 0)])
    s_bcs = b.bc_slope
    assert s_bcs == [(0, 1), (4, 3), (5, 0)]

    # Test for deflection boundary condition method
    b.bc_deflection.extend([(4, 3), (5, 0)])
    d_bcs = b.bc_deflection
    assert d_bcs == [(0, 2), (4, 3), (5, 0)]

    # Test for updated boundary conditions
    bcs_new = b.boundary_conditions
    assert bcs_new == {
        'deflection': [(0, 2), (4, 3), (5, 0)],
        'slope': [(0, 1), (4, 3), (5, 0)]}

    b1 = Beam(30, E, I)
    b1.apply_load(-8, 0, -1)
    b1.apply_load(R1, 10, -1)
    b1.apply_load(R2, 30, -1)
    b1.apply_load(120, 30, -2)
    b1.bc_deflection = [(10, 0), (30, 0)]
    b1.solve_for_reaction_loads(R1, R2)

    # Test for finding reaction forces
    p = b1.reaction_loads
    q = {R1: 6, R2: 2}
    assert p == q

    # Test for load distribution function.
    p = b1.load
    q = -8*SingularityFunction(x, 0, -1) + 6*SingularityFunction(x, 10, -1) + 120*SingularityFunction(x, 30, -2) + 2*SingularityFunction(x, 30, -1)
    assert p == q

    # Test for shear force distribution function
    p = b1.shear_force()
    q = -8*SingularityFunction(x, 0, 0) + 6*SingularityFunction(x, 10, 0) + 120*SingularityFunction(x, 30, -1) + 2*SingularityFunction(x, 30, 0)
    assert p == q

    # Test for bending moment distribution function
    p = b1.bending_moment()
    q = -8*SingularityFunction(x, 0, 1) + 6*SingularityFunction(x, 10, 1) + 120*SingularityFunction(x, 30, 0) + 2*SingularityFunction(x, 30, 1)
    assert p == q

    # Test for slope distribution function
    p = b1.slope()
    q = -4*SingularityFunction(x, 0, 2) + 3*SingularityFunction(x, 10, 2) + 120*SingularityFunction(x, 30, 1) + SingularityFunction(x, 30, 2) + 4000/3
    assert p == q/(E*I)

    # Test for deflection distribution function
    p = b1.deflection()
    q = 4000*x/3 - 4*SingularityFunction(x, 0, 3)/3 + SingularityFunction(x, 10, 3) + 60*SingularityFunction(x, 30, 2) + SingularityFunction(x, 30, 3)/3 - 12000
    assert p == q/(E*I)

    # Test using symbols
    l = Symbol('l')
    w0 = Symbol('w0')
    w2 = Symbol('w2')
    a1 = Symbol('a1')
    c = Symbol('c')
    c1 = Symbol('c1')
    d = Symbol('d')
    e = Symbol('e')
    f = Symbol('f')

    b2 = Beam(l, E, I)

    b2.apply_load(w0, a1, 1)
    b2.apply_load(w2, c1, -1)

    b2.bc_deflection = [(c, d)]
    b2.bc_slope = [(e, f)]

    # Test for load distribution function.
    p = b2.load
    q = w0*SingularityFunction(x, a1, 1) + w2*SingularityFunction(x, c1, -1)
    assert p == q

    # Test for shear force distribution function
    p = b2.shear_force()
    q = w0*SingularityFunction(x, a1, 2)/2 + w2*SingularityFunction(x, c1, 0)
    assert p == q

    # Test for bending moment distribution function
    p = b2.bending_moment()
    q = w0*SingularityFunction(x, a1, 3)/6 + w2*SingularityFunction(x, c1, 1)
    assert p == q

    # Test for slope distribution function
    p = b2.slope()
    q = (w0*SingularityFunction(x, a1, 4)/24 + w2*SingularityFunction(x, c1, 2)/2)/(E*I) + (E*I*f - w0*SingularityFunction(e, a1, 4)/24 - w2*SingularityFunction(e, c1, 2)/2)/(E*I)
    assert p == q

    # Test for deflection distribution function
    p = b2.deflection()
    q = x*(E*I*f - w0*SingularityFunction(e, a1, 4)/24 - w2*SingularityFunction(e, c1, 2)/2)/(E*I) + (w0*SingularityFunction(x, a1, 5)/120 + w2*SingularityFunction(x, c1, 3)/6)/(E*I) + (E*I*(-c*f + d) + c*w0*SingularityFunction(e, a1, 4)/24 + c*w2*SingularityFunction(e, c1, 2)/2 - w0*SingularityFunction(c, a1, 5)/120 - w2*SingularityFunction(c, c1, 3)/6)/(E*I)
    assert p == q

    b3 = Beam(9, E, I)
    b3.apply_load(value=-2, start=2, order=2, end=3)
    b3.bc_slope.append((0, 2))
    C3 = symbols('C3')
    C4 = symbols('C4')
    p = b3.load
    q = - 2*SingularityFunction(x, 2, 2) + 2*SingularityFunction(x, 3, 0) + 2*SingularityFunction(x, 3, 2)
    assert p == q

    p = b3.slope()
    q = 2 + (-SingularityFunction(x, 2, 5)/30 + SingularityFunction(x, 3, 3)/3 + SingularityFunction(x, 3, 5)/30)/(E*I)
    assert p == q

    p = b3.deflection()
    q = 2*x + (-SingularityFunction(x, 2, 6)/180 + SingularityFunction(x, 3, 4)/12 + SingularityFunction(x, 3, 6)/180)/(E*I)
    assert p == q + C4

    b4 = Beam(4, E, I)
    b4.apply_load(-3, 0, 0, end=3)

    p = b4.load
    q = -3*SingularityFunction(x, 0, 0) + 3*SingularityFunction(x, 3, 0)
    assert p == q

    p = b4.slope()
    q = -3*SingularityFunction(x, 0, 3)/6 + 3*SingularityFunction(x, 3, 3)/6
    assert p == q/(E*I) + C3

    p = b4.deflection()
    q = -3*SingularityFunction(x, 0, 4)/24 + 3*SingularityFunction(x, 3, 4)/24
    assert p == q/(E*I) + C3*x + C4

    raises(ValueError, lambda: b4.apply_load(-3, 0, -1, end=3))
    with raises(TypeError):
        b4.variable = 1


def test_insufficient_bconditions():
    # Test cases when required number of boundary conditions
    # are not provided to solve the integration constants.
    L = symbols('L', positive=True)
    E, I, P, a3, a4 = symbols('E I P a3 a4')

    b = Beam(L, E, I, base_char='a')
    b.apply_load(R2, L, -1)
    b.apply_load(R1, 0, -1)
    b.apply_load(-P, L/2, -1)
    b.solve_for_reaction_loads(R1, R2)

    p = b.slope()
    q = P*SingularityFunction(x, 0, 2)/4 - P*SingularityFunction(x, L/2, 2)/2 + P*SingularityFunction(x, L, 2)/4
    assert p == q/(E*I) + a3

    p = b.deflection()
    q = P*SingularityFunction(x, 0, 3)/12 - P*SingularityFunction(x, L/2, 3)/6 + P*SingularityFunction(x, L, 3)/12
    assert p == q/(E*I) + a3*x + a4

    b.bc_deflection = [(0, 0)]
    p = b.deflection()
    q = a3*x + P*SingularityFunction(x, 0, 3)/12 - P*SingularityFunction(x, L/2, 3)/6 + P*SingularityFunction(x, L, 3)/12
    assert p == q/(E*I)

    b.bc_deflection = [(0, 0), (L, 0)]
    p = b.deflection()
    q = -L**2*P*x/16 + P*SingularityFunction(x, 0, 3)/12 - P*SingularityFunction(x, L/2, 3)/6 + P*SingularityFunction(x, L, 3)/12
    assert p == q/(E*I)


def test_statically_indeterminate():
    E = Symbol('E')
    I = Symbol('I')
    M1, M2 = symbols('M1, M2')
    F = Symbol('F')
    l = Symbol('l', positive=True)

    b5 = Beam(l, E, I)
    b5.bc_deflection = [(0, 0),(l, 0)]
    b5.bc_slope = [(0, 0),(l, 0)]

    b5.apply_load(R1, 0, -1)
    b5.apply_load(M1, 0, -2)
    b5.apply_load(R2, l, -1)
    b5.apply_load(M2, l, -2)
    b5.apply_load(-F, l/2, -1)

    b5.solve_for_reaction_loads(R1, R2, M1, M2)
    p = b5.reaction_loads
    q = {R1: F/2, R2: F/2, M1: -F*l/8, M2: F*l/8}
    assert p == q


def test_beam_units():
    E = Symbol('E')
    I = Symbol('I')
    R1, R2 = symbols('R1, R2')

    b = Beam(8*meter, 200*giga*newton/meter**2, 400*1000000*(milli*meter)**4)
    b.apply_load(5*kilo*newton, 2*meter, -1)
    b.apply_load(R1, 0*meter, -1)
    b.apply_load(R2, 8*meter, -1)
    b.apply_load(10*kilo*newton/meter, 4*meter, 0, end=8*meter)
    b.bc_deflection = [(0*meter, 0*meter), (8*meter, 0*meter)]
    b.solve_for_reaction_loads(R1, R2)
    assert b.reaction_loads == {R1: -13750*newton, R2: -31250*newton}

    b = Beam(3*meter, E*newton/meter**2, I*meter**4)
    b.apply_load(8*kilo*newton, 1*meter, -1)
    b.apply_load(R1, 0*meter, -1)
    b.apply_load(R2, 3*meter, -1)
    b.apply_load(12*kilo*newton*meter, 2*meter, -2)
    b.bc_deflection = [(0*meter, 0*meter), (3*meter, 0*meter)]
    b.solve_for_reaction_loads(R1, R2)
    assert b.reaction_loads == {R1: -28000*newton/3, R2: 4000*newton/3}
    assert b.deflection().subs(x, 1*meter) == 62000*meter/(9*E*I)


def test_variable_moment():
    E = Symbol('E')
    I = Symbol('I')

    b = Beam(4, E, 2*(4 - x))
    b.apply_load(20, 4, -1)
    R, M = symbols('R, M')
    b.apply_load(R, 0, -1)
    b.apply_load(M, 0, -2)
    b.bc_deflection = [(0, 0)]
    b.bc_slope = [(0, 0)]
    b.solve_for_reaction_loads(R, M)
    assert b.slope().expand() == ((10*x*SingularityFunction(x, 0, 0)
        - 10*(x - 4)*SingularityFunction(x, 4, 0))/E).expand()
    assert b.deflection().expand() == ((5*x**2*SingularityFunction(x, 0, 0)
        - 10*Piecewise((0, Abs(x)/4 < 1), (16*meijerg(((3, 1), ()), ((), (2, 0)), x/4), True))
        + 40*SingularityFunction(x, 4, 1))/E).expand()

    b = Beam(4, E - x, I)
    b.apply_load(20, 4, -1)
    R, M = symbols('R, M')
    b.apply_load(R, 0, -1)
    b.apply_load(M, 0, -2)
    b.bc_deflection = [(0, 0)]
    b.bc_slope = [(0, 0)]
    b.solve_for_reaction_loads(R, M)
    assert b.slope().expand() == ((-80*(-log(-E) + log(-E + x))*SingularityFunction(x, 0, 0)
        + 80*(-log(-E + 4) + log(-E + x))*SingularityFunction(x, 4, 0) + 20*(-E*log(-E)
        + E*log(-E + x) + x)*SingularityFunction(x, 0, 0) - 20*(-E*log(-E + 4) + E*log(-E + x)
        + x - 4)*SingularityFunction(x, 4, 0))/I).expand()


def test_composite_beam():
    E = Symbol('E')
    I = Symbol('I')
    b1 = Beam(2, E, 1.5*I)
    b2 = Beam(2, E, I)
    b = b1.join(b2, "fixed")
    b.apply_load(-20, 0, -1)
    b.apply_load(80, 0, -2)
    b.apply_load(20, 4, -1)
    b.bc_slope = [(0, 0)]
    b.bc_deflection = [(0, 0)]
    assert b.length == 4
    assert b.second_moment == Piecewise((1.5*I, x <= 2), (I, x <= 4))
    assert b.slope().subs(x, 4) == 120.0/(E*I)
    assert b.slope().subs(x, 2) == 80.0/(E*I)
    assert int(b.deflection().subs(x, 4).args[0]) == 302  # Coefficient of 1/(E*I)

    l = symbols('l', positive=True)
    R1, M1, R2, R3, P = symbols('R1 M1 R2 R3 P')
    b1 = Beam(2*l, E, I)
    b2 = Beam(2*l, E, I)
    b = b1.join(b2,"hinge")
    b.apply_load(M1, 0, -2)
    b.apply_load(R1, 0, -1)
    b.apply_load(R2, l, -1)
    b.apply_load(R3, 4*l, -1)
    b.apply_load(P, 3*l, -1)
    b.bc_slope = [(0, 0)]
    b.bc_deflection = [(0, 0), (l, 0), (4*l, 0)]
    b.solve_for_reaction_loads(M1, R1, R2, R3)
    assert b.reaction_loads == {R3: -P/2, R2: -5*P/4, M1: -P*l/4, R1: 3*P/4}
    assert b.slope().subs(x, 3*l) == -7*P*l**2/(48*E*I)
    assert b.deflection().subs(x, 2*l) == 7*P*l**3/(24*E*I)
    assert b.deflection().subs(x, 3*l) == 5*P*l**3/(16*E*I)


def test_point_cflexure():
    E = Symbol('E')
    I = Symbol('I')
    b = Beam(10, E, I)
    b.apply_load(-4, 0, -1)
    b.apply_load(-46, 6, -1)
    b.apply_load(10, 2, -1)
    b.apply_load(20, 4, -1)
    b.apply_load(3, 6, 0)
    assert b.point_cflexure() == [S(10)/3]


def test_remove_load():
    E = Symbol('E')
    I = Symbol('I')
    b = Beam(4, E, I)

    try:
        b.remove_load(2, 1, -1)
    # As no load is applied on beam, ValueError should be returned.
    except ValueError:
        assert True
    else:
        assert False

    b.apply_load(-3, 0, -2)
    b.apply_load(4, 2, -1)
    b.apply_load(-2, 2, 2, end = 3)
    b.remove_load(-2, 2, 2, end = 3)
    assert b.load == -3*SingularityFunction(x, 0, -2) + 4*SingularityFunction(x, 2, -1)
    assert b.applied_loads == [(-3, 0, -2, None), (4, 2, -1, None)]

    try:
        b.remove_load(1, 2, -1)
    # As load of this magnitude was never applied at
    # this position, method should return a ValueError.
    except ValueError:
        assert True
    else:
        assert False

    b.remove_load(-3, 0, -2)
    b.remove_load(4, 2, -1)
    assert b.load == 0
    assert b.applied_loads == []


def test_apply_support():
    E = Symbol('E')
    I = Symbol('I')

    b = Beam(4, E, I)
    b.apply_support(0, "cantilever")
    b.apply_load(20, 4, -1)
    M_0, R_0 = symbols('M_0, R_0')
    b.solve_for_reaction_loads(R_0, M_0)
    assert b.slope() == (80*SingularityFunction(x, 0, 1) - 10*SingularityFunction(x, 0, 2)
                + 10*SingularityFunction(x, 4, 2))/(E*I)
    assert b.deflection() == (40*SingularityFunction(x, 0, 2) - 10*SingularityFunction(x, 0, 3)/3
                + 10*SingularityFunction(x, 4, 3)/3)/(E*I)

    b = Beam(30, E, I)
    b.apply_support(10, "pin")
    b.apply_support(30, "roller")
    b.apply_load(-8, 0, -1)
    b.apply_load(120, 30, -2)
    R_10, R_30 = symbols('R_10, R_30')
    b.solve_for_reaction_loads(R_10, R_30)
    assert b.slope() == (-4*SingularityFunction(x, 0, 2) + 3*SingularityFunction(x, 10, 2)
            + 120*SingularityFunction(x, 30, 1) + SingularityFunction(x, 30, 2) + 4000/3)/(E*I)
    assert b.deflection() == (4000*x/3 - 4*SingularityFunction(x, 0, 3)/3 + SingularityFunction(x, 10, 3)
            + 60*SingularityFunction(x, 30, 2) + SingularityFunction(x, 30, 3)/3 - 12000)/(E*I)


def max_shear_force(self):
    E = Symbol('E')
    I = Symbol('I')

    b = Beam(3, E, I)
    R, M = symbols('R, M')
    b.apply_load(R, 0, -1)
    b.apply_load(M, 0, -2)
    b.apply_load(2, 3, -1)
    b.apply_load(4, 2, -1)
    b.apply_load(2, 2, 0, end=3)
    b.solve_for_reaction_loads(R, M)
    assert b.max_shear_force() == (Interval(0, 2), 8)

    l = symbols('l', positive=True)
    P = Symbol('P')
    b = Beam(l, E, I)
    R1, R2 = symbols('R1, R2')
    b.apply_load(R1, 0, -1)
    b.apply_load(R2, l, -1)
    b.apply_load(P, 0, 0, end=l)
    b.solve_for_reaction_loads(R1, R2)
    assert b.max_shear_force() == (0, l*Abs(P)/2)


def test_max_bmoment():
    E = Symbol('E')
    I = Symbol('I')
    l, P = symbols('l, P', positive=True)

    b = Beam(l, E, I)
    R1, R2 = symbols('R1, R2')
    b.apply_load(R1, 0, -1)
    b.apply_load(R2, l, -1)
    b.apply_load(P, l/2, -1)
    b.solve_for_reaction_loads(R1, R2)
    b.reaction_loads
    assert b.max_bmoment() == (l/2, P*l/4)

    b = Beam(l, E, I)
    R1, R2 = symbols('R1, R2')
    b.apply_load(R1, 0, -1)
    b.apply_load(R2, l, -1)
    b.apply_load(P, 0, 0, end=l)
    b.solve_for_reaction_loads(R1, R2)
    assert b.max_bmoment() == (l/2, P*l**2/8)


def test_max_deflection():
    E, I, l, F = symbols('E, I, l, F', positive=True)
    b = Beam(l, E, I)
    b.bc_deflection = [(0, 0),(l, 0)]
    b.bc_slope = [(0, 0),(l, 0)]
    b.apply_load(F/2, 0, -1)
    b.apply_load(-F*l/8, 0, -2)
    b.apply_load(F/2, l, -1)
    b.apply_load(F*l/8, l, -2)
    b.apply_load(-F, l/2, -1)
    assert b.max_deflection() == (l/2, F*l**3/(192*E*I))

def test_Beam3D():
    l, E, G, I, A = symbols('l, E, G, I, A')
    R1, R2, R3, R4 = symbols('R1, R2, R3, R4')

    b = Beam3D(l, E, G, I, A)
    m, q = symbols('m, q')
    b.apply_load(q, 0, 0, dir="y")
    b.apply_moment_load(m, 0, 0, dir="z")
    b.bc_slope = [(0, [0, 0, 0]), (l, [0, 0, 0])]
    b.bc_deflection = [(0, [0, 0, 0]), (l, [0, 0, 0])]
    b.solve_slope_deflection()

    assert b.shear_force() == [0, -q*x, 0]
    assert b.bending_moment() == [0, 0, -m*x + q*x**2/2]
    assert b.deflection() == [0, -l**2*q*x**2/(12*E*I) + l**2*x**2*(A*G*l**2*q - 2*A*G*l*m
            + 12*E*I*q)/(8*E*I*(A*G*l**2 + 12*E*I)) + l*m*x**2/(4*E*I) - l*x**3*(A*G*l**2*q
            - 2*A*G*l*m + 12*E*I*q)/(12*E*I*(A*G*l**2 + 12*E*I)) - m*x**3/(6*E*I) + q*x**4/(24*E*I)
            + l*x*(A*G*l**2*q - 2*A*G*l*m + 12*E*I*q)/(2*A*G*(A*G*l**2 + 12*E*I))
            - q*x**2/(2*A*G), 0]


    b2 = Beam3D(30, E, G, I, A, x)
    b2.apply_load(50, start=0, order=0, dir="y")
    b2.bc_deflection = [(0, [0, 0, 0]), (30, [0, 0, 0])]
    b2.apply_load(R1, start=0, order=-1, dir="y")
    b2.apply_load(R2, start=30, order=-1, dir="y")
    b2.solve_for_reaction_loads(R1, R2)
    assert b2.reaction_loads == {R1: -750, R2: -750}

    b2.solve_slope_deflection()
    assert b2.slope() == [0, 0, 25*x**3/(3*E*I) - 375*x**2/(E*I) + 3750*x/(E*I)]
    assert b2.deflection() == [0, 25*x**4/(12*E*I) - 125*x**3/(E*I) + 1875*x**2/(E*I)
                        - 25*x**2/(A*G) + 750*x/(A*G), 0]

    # Test for solve_for_reaction_loads
    b3 = Beam3D(30, E, G, I, A, x)
    b3.apply_load(8, start=0, order=0, dir="y")
    b3.apply_load(9*x, start=0, order=0, dir="z")
    b3.apply_load(R1, start=0, order=-1, dir="y")
    b3.apply_load(R2, start=30, order=-1, dir="y")
    b3.apply_load(R3, start=0, order=-1, dir="z")
    b3.apply_load(R4, start=30, order=-1, dir="z")
    b3.solve_for_reaction_loads(R1, R2, R3, R4)
    assert b3.reaction_loads == {R1: -120, R2: -120, R3: -1350, R4: -2700}
