Python ReferenceFrame.orientnew方法代码示例

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_dcm():
    q1, q2, q3, q4 = dynamicsymbols('q1 q2 q3 q4')
    N = ReferenceFrame('N')
    A = N.orientnew('A', 'Axis', [q1, N.z])
    B = A.orientnew('B', 'Axis', [q2, A.x])
    C = B.orientnew('C', 'Axis', [q3, B.y])
    D = N.orientnew('D', 'Axis', [q4, N.y])
    E = N.orientnew('E', 'Space', [q1, q2, q3], '123')
    assert N.dcm(C) == Matrix([
        [- sin(q1) * sin(q2) * sin(q3) + cos(q1) * cos(q3), - sin(q1) *
        cos(q2), sin(q1) * sin(q2) * cos(q3) + sin(q3) * cos(q1)], [sin(q1) *
        cos(q3) + sin(q2) * sin(q3) * cos(q1), cos(q1) * cos(q2), sin(q1) *
            sin(q3) - sin(q2) * cos(q1) * cos(q3)], [- sin(q3) * cos(q2), sin(q2),
        cos(q2) * cos(q3)]])
    # This is a little touchy.  Is it ok to use simplify in assert?
    assert D.dcm(C) == Matrix(
        [[cos(q1) * cos(q3) * cos(q4) - sin(q3) * (- sin(q4) * cos(q2) +
        sin(q1) * sin(q2) * cos(q4)), - sin(q2) * sin(q4) - sin(q1) *
            cos(q2) * cos(q4), sin(q3) * cos(q1) * cos(q4) + cos(q3) * (- sin(q4) *
        cos(q2) + sin(q1) * sin(q2) * cos(q4))], [sin(q1) * cos(q3) +
        sin(q2) * sin(q3) * cos(q1), cos(q1) * cos(q2), sin(q1) * sin(q3) -
            sin(q2) * cos(q1) * cos(q3)], [sin(q4) * cos(q1) * cos(q3) -
        sin(q3) * (cos(q2) * cos(q4) + sin(q1) * sin(q2) * sin(q4)), sin(q2) *
                cos(q4) - sin(q1) * sin(q4) * cos(q2), sin(q3) * sin(q4) * cos(q1) +
                cos(q3) * (cos(q2) * cos(q4) + sin(q1) * sin(q2) * sin(q4))]])
    assert E.dcm(N) == Matrix(
        [[cos(q2)*cos(q3), sin(q3)*cos(q2), -sin(q2)],
        [sin(q1)*sin(q2)*cos(q3) - sin(q3)*cos(q1), sin(q1)*sin(q2)*sin(q3) +
        cos(q1)*cos(q3), sin(q1)*cos(q2)], [sin(q1)*sin(q3) +
        sin(q2)*cos(q1)*cos(q3), - sin(q1)*cos(q3) + sin(q2)*sin(q3)*cos(q1),
         cos(q1)*cos(q2)]])

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_dcm():
    q1, q2, q3, q4 = dynamicsymbols("q1 q2 q3 q4")
    N = ReferenceFrame("N")
    A = N.orientnew("A", "Axis", [q1, N.z])
    B = A.orientnew("B", "Axis", [q2, A.x])
    C = B.orientnew("C", "Axis", [q3, B.y])
    D = N.orientnew("D", "Axis", [q4, N.y])
    E = N.orientnew("E", "Space", [q1, q2, q3], "123")
    assert N.dcm(C) == Matrix(
        [
            [
                -sin(q1) * sin(q2) * sin(q3) + cos(q1) * cos(q3),
                -sin(q1) * cos(q2),
                sin(q1) * sin(q2) * cos(q3) + sin(q3) * cos(q1),
            ],
            [
                sin(q1) * cos(q3) + sin(q2) * sin(q3) * cos(q1),
                cos(q1) * cos(q2),
                sin(q1) * sin(q3) - sin(q2) * cos(q1) * cos(q3),
            ],
            [-sin(q3) * cos(q2), sin(q2), cos(q2) * cos(q3)],
        ]
    )
    # This is a little touchy.  Is it ok to use simplify in assert?
    test_mat = D.dcm(C) - Matrix(
        [
            [
                cos(q1) * cos(q3) * cos(q4) - sin(q3) * (-sin(q4) * cos(q2) + sin(q1) * sin(q2) * cos(q4)),
                -sin(q2) * sin(q4) - sin(q1) * cos(q2) * cos(q4),
                sin(q3) * cos(q1) * cos(q4) + cos(q3) * (-sin(q4) * cos(q2) + sin(q1) * sin(q2) * cos(q4)),
            ],
            [
                sin(q1) * cos(q3) + sin(q2) * sin(q3) * cos(q1),
                cos(q1) * cos(q2),
                sin(q1) * sin(q3) - sin(q2) * cos(q1) * cos(q3),
            ],
            [
                sin(q4) * cos(q1) * cos(q3) - sin(q3) * (cos(q2) * cos(q4) + sin(q1) * sin(q2) * sin(q4)),
                sin(q2) * cos(q4) - sin(q1) * sin(q4) * cos(q2),
                sin(q3) * sin(q4) * cos(q1) + cos(q3) * (cos(q2) * cos(q4) + sin(q1) * sin(q2) * sin(q4)),
            ],
        ]
    )
    assert test_mat.expand() == zeros(3, 3)
    assert E.dcm(N) == Matrix(
        [
            [cos(q2) * cos(q3), sin(q3) * cos(q2), -sin(q2)],
            [
                sin(q1) * sin(q2) * cos(q3) - sin(q3) * cos(q1),
                sin(q1) * sin(q2) * sin(q3) + cos(q1) * cos(q3),
                sin(q1) * cos(q2),
            ],
            [
                sin(q1) * sin(q3) + sin(q2) * cos(q1) * cos(q3),
                -sin(q1) * cos(q3) + sin(q2) * sin(q3) * cos(q1),
                cos(q1) * cos(q2),
            ],
        ]
    )

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_partial_velocity():
    q1, q2, q3, u1, u2, u3 = dynamicsymbols("q1 q2 q3 u1 u2 u3")
    u4, u5 = dynamicsymbols("u4, u5")
    r = symbols("r")

    N = ReferenceFrame("N")
    Y = N.orientnew("Y", "Axis", [q1, N.z])
    L = Y.orientnew("L", "Axis", [q2, Y.x])
    R = L.orientnew("R", "Axis", [q3, L.y])
    R.set_ang_vel(N, u1 * L.x + u2 * L.y + u3 * L.z)

    C = Point("C")
    C.set_vel(N, u4 * L.x + u5 * (Y.z ^ L.x))
    Dmc = C.locatenew("Dmc", r * L.z)
    Dmc.v2pt_theory(C, N, R)

    vel_list = [Dmc.vel(N), C.vel(N), R.ang_vel_in(N)]
    u_list = [u1, u2, u3, u4, u5]
    assert partial_velocity(vel_list, u_list) == [
        [-r * L.y, 0, L.x],
        [r * L.x, 0, L.y],
        [0, 0, L.z],
        [L.x, L.x, 0],
        [cos(q2) * L.y - sin(q2) * L.z, cos(q2) * L.y - sin(q2) * L.z, 0],
    ]

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_linearize_pendulum_lagrange_minimal():
    q1 = dynamicsymbols('q1')                     # angle of pendulum
    q1d = dynamicsymbols('q1', 1)                 # Angular velocity
    L, m, t = symbols('L, m, t')
    g = 9.8

    # Compose world frame
    N = ReferenceFrame('N')
    pN = Point('N*')
    pN.set_vel(N, 0)

    # A.x is along the pendulum
    A = N.orientnew('A', 'axis', [q1, N.z])
    A.set_ang_vel(N, q1d*N.z)

    # Locate point P relative to the origin N*
    P = pN.locatenew('P', L*A.x)
    P.v2pt_theory(pN, N, A)
    pP = Particle('pP', P, m)

    # Solve for eom with Lagranges method
    Lag = Lagrangian(N, pP)
    LM = LagrangesMethod(Lag, [q1], forcelist=[(P, m*g*N.x)], frame=N)
    LM.form_lagranges_equations()

    # Linearize
    A, B, inp_vec = LM.linearize([q1], [q1d], A_and_B=True)

    assert A == Matrix([[0, 1], [-9.8*cos(q1)/L, 0]])
    assert B == Matrix([])

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_linearize_pendulum_lagrange_nonminimal():
    q1, q2 = dynamicsymbols('q1:3')
    q1d, q2d = dynamicsymbols('q1:3', level=1)
    L, m, t = symbols('L, m, t')
    g = 9.8
    # Compose World Frame
    N = ReferenceFrame('N')
    pN = Point('N*')
    pN.set_vel(N, 0)
    # A.x is along the pendulum
    theta1 = atan(q2/q1)
    A = N.orientnew('A', 'axis', [theta1, N.z])
    # Create point P, the pendulum mass
    P = pN.locatenew('P1', q1*N.x + q2*N.y)
    P.set_vel(N, P.pos_from(pN).dt(N))
    pP = Particle('pP', P, m)
    # Constraint Equations
    f_c = Matrix([q1**2 + q2**2 - L**2])
    # Calculate the lagrangian, and form the equations of motion
    Lag = Lagrangian(N, pP)
    LM = LagrangesMethod(Lag, [q1, q2], hol_coneqs=f_c, forcelist=[(P, m*g*N.x)], frame=N)
    LM.form_lagranges_equations()
    # Compose operating point
    op_point = {q1: L, q2: 0, q1d: 0, q2d: 0, q1d.diff(t): 0, q2d.diff(t): 0}
    # Solve for multiplier operating point
    lam_op = LM.solve_multipliers(op_point=op_point)
    op_point.update(lam_op)
    # Perform the Linearization
    A, B, inp_vec = LM.linearize([q2], [q2d], [q1], [q1d],
            op_point=op_point, A_and_B=True)
    assert A == Matrix([[0, 1], [-9.8/L, 0]])
    assert B == Matrix([])

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_point_funcs():
    q, q2 = dynamicsymbols('q q2')
    qd, q2d = dynamicsymbols('q q2', 1)
    qdd, q2dd = dynamicsymbols('q q2', 2)
    N = ReferenceFrame('N')
    B = ReferenceFrame('B')
    B.set_ang_vel(N, 5 * B.y)
    O = Point('O')
    P = O.locatenew('P', q * B.x)
    assert P.pos_from(O) == q * B.x
    P.set_vel(B, qd * B.x + q2d * B.y)
    assert P.vel(B) == qd * B.x + q2d * B.y
    O.set_vel(N, 0)
    assert O.vel(N) == 0
    assert P.a1pt_theory(O, N, B) == ((-25 * q + qdd) * B.x + (q2dd) * B.y +
                               (-10 * qd) * B.z)

    B = N.orientnew('B', 'Axis', [q, N.z])
    O = Point('O')
    P = O.locatenew('P', 10 * B.x)
    O.set_vel(N, 5 * N.x)
    assert O.vel(N) == 5 * N.x
    assert P.a2pt_theory(O, N, B) == (-10 * qd**2) * B.x + (10 * qdd) * B.y

    B.set_ang_vel(N, 5 * B.y)
    O = Point('O')
    P = O.locatenew('P', q * B.x)
    P.set_vel(B, qd * B.x + q2d * B.y)
    O.set_vel(N, 0)
    assert P.v1pt_theory(O, N, B) == qd * B.x + q2d * B.y - 5 * q * B.z

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_pendulum_angular_momentum():
    """Consider a pendulum of length OA = 2a, of mass m as a rigid body of
    center of mass G (OG = a) which turn around (O,z). The angle between the
    reference frame R and the rod is q.  The inertia of the body is I =
    (G,0,ma^2/3,ma^2/3). """

    m, a = symbols('m, a')
    q = dynamicsymbols('q')

    R = ReferenceFrame('R')
    R1 = R.orientnew('R1', 'Axis', [q, R.z])
    R1.set_ang_vel(R, q.diff() * R.z)

    I = inertia(R1, 0, m * a**2 / 3, m * a**2 / 3)

    O = Point('O')

    A = O.locatenew('A', 2*a * R1.x)
    G = O.locatenew('G', a * R1.x)

    S = RigidBody('S', G, R1, m, (I, G))

    O.set_vel(R, 0)
    A.v2pt_theory(O, R, R1)
    G.v2pt_theory(O, R, R1)

    assert (4 * m * a**2 / 3 * q.diff() * R.z -
            S.angular_momentum(O, R).express(R)) == 0

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_aux():
    # Same as above, except we have 2 auxiliary speeds for the ground contact
    # point, which is known to be zero. In one case, we go through then
    # substitute the aux. speeds in at the end (they are zero, as well as their
    # derivative), in the other case, we use the built-in auxiliary speed part
    # of Kane. The equations from each should be the same.
    q1, q2, q3, u1, u2, u3  = dynamicsymbols('q1 q2 q3 u1 u2 u3')
    q1d, q2d, q3d, u1d, u2d, u3d = dynamicsymbols('q1 q2 q3 u1 u2 u3', 1)
    u4, u5, f1, f2 = dynamicsymbols('u4, u5, f1, f2')
    u4d, u5d = dynamicsymbols('u4, u5', 1)
    r, m, g = symbols('r m g')

    N = ReferenceFrame('N')
    Y = N.orientnew('Y', 'Axis', [q1, N.z])
    L = Y.orientnew('L', 'Axis', [q2, Y.x])
    R = L.orientnew('R', 'Axis', [q3, L.y])
    R.set_ang_vel(N, u1 * L.x + u2 * L.y + u3 * L.z)
    R.set_ang_acc(N, R.ang_vel_in(N).dt(R) + (R.ang_vel_in(N) ^
        R.ang_vel_in(N)))

    C = Point('C')
    C.set_vel(N, u4 * L.x + u5 * (Y.z ^ L.x))
    Dmc = C.locatenew('Dmc', r * L.z)
    Dmc.v2pt_theory(C, N, R)
    Dmc.a2pt_theory(C, N, R)

    I = inertia(L, m / 4 * r**2, m / 2 * r**2, m / 4 * r**2)

    kd = [q1d - u3/cos(q3), q2d - u1, q3d - u2 + u3 * tan(q2)]

    ForceList = [(Dmc, - m * g * Y.z), (C, f1 * L.x + f2 * (Y.z ^ L.x))]
    BodyD = RigidBody()
    BodyD.mc = Dmc
    BodyD.inertia = (I, Dmc)
    BodyD.frame = R
    BodyD.mass = m
    BodyList = [BodyD]

    KM = Kane(N)
    KM.coords([q1, q2, q3])
    KM.speeds([u1, u2, u3, u4, u5])
    KM.kindiffeq(kd)
    kdd = KM.kindiffdict()
    (fr, frstar) = KM.kanes_equations(ForceList, BodyList)
    fr = fr.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5:0})
    frstar = frstar.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5:0})

    KM2 = Kane(N)
    KM2.coords([q1, q2, q3])
    KM2.speeds([u1, u2, u3], u_auxiliary=[u4, u5])
    KM2.kindiffeq(kd)
    (fr2, frstar2) = KM2.kanes_equations(ForceList, BodyList)
    fr2 = fr2.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5:0})
    frstar2 = frstar2.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5:0})

    assert fr.expand() == fr2.expand()
    assert frstar.expand() == frstar2.expand()

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_rolling_disc():
    # Rolling Disc Example
    # Here the rolling disc is formed from the contact point up, removing the
    # need to introduce generalized speeds. Only 3 configuration and 3
    # speed variables are need to describe this system, along with the
    # disc's mass and radius, and the local gravity.
    q1, q2, q3 = dynamicsymbols('q1 q2 q3')
    q1d, q2d, q3d = dynamicsymbols('q1 q2 q3', 1)
    r, m, g = symbols('r m g')

    # The kinematics are formed by a series of simple rotations. Each simple
    # rotation creates a new frame, and the next rotation is defined by the new
    # frame's basis vectors. This example uses a 3-1-2 series of rotations, or
    # Z, X, Y series of rotations. Angular velocity for this is defined using
    # the second frame's basis (the lean frame).
    N = ReferenceFrame('N')
    Y = N.orientnew('Y', 'Axis', [q1, N.z])
    L = Y.orientnew('L', 'Axis', [q2, Y.x])
    R = L.orientnew('R', 'Axis', [q3, L.y])

    # This is the translational kinematics. We create a point with no velocity
    # in N; this is the contact point between the disc and ground. Next we form
    # the position vector from the contact point to the disc's center of mass.
    # Finally we form the velocity and acceleration of the disc.
    C = Point('C')
    C.set_vel(N, 0)
    Dmc = C.locatenew('Dmc', r * L.z)
    Dmc.v2pt_theory(C, N, R)

    # Forming the inertia dyadic.
    I = inertia(L, m / 4 * r**2, m / 2 * r**2, m / 4 * r**2)
    BodyD = RigidBody('BodyD', Dmc, R, m, (I, Dmc))

    # Finally we form the equations of motion, using the same steps we did
    # before. Supply the Lagrangian, the generalized speeds.
    BodyD.set_potential_energy(- m * g * r * cos(q2))
    Lag = Lagrangian(N, BodyD)
    q = [q1, q2, q3]
    q1 = Function('q1')
    q2 = Function('q2')
    q3 = Function('q3')
    l = LagrangesMethod(Lag, q)
    l.form_lagranges_equations()
    RHS = l.rhs()
    RHS.simplify()
    t = symbols('t')

    assert (l.mass_matrix[3:6] == [0, 5*m*r**2/4, 0])
    assert RHS[4].simplify() == (-8*g*sin(q2(t)) + 5*r*sin(2*q2(t)
        )*Derivative(q1(t), t)**2 + 12*r*cos(q2(t))*Derivative(q1(t), t
        )*Derivative(q3(t), t))/(10*r)
    assert RHS[5] == (-5*cos(q2(t))*Derivative(q1(t), t) + 6*tan(q2(t)
        )*Derivative(q3(t), t) + 4*Derivative(q1(t), t)/cos(q2(t))
        )*Derivative(q2(t), t)

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_point_pos():
    q = dynamicsymbols('q')
    N = ReferenceFrame('N')
    B = N.orientnew('B', 'Axis', [q, N.z])
    O = Point('O')
    P = O.locatenew('P', 10 * N.x + 5 * B.x)
    assert P.pos_from(O) == 10 * N.x + 5 * B.x
    Q = P.locatenew('Q', 10 * N.y + 5 * B.y)
    assert Q.pos_from(P) == 10 * N.y + 5 * B.y
    assert Q.pos_from(O) == 10 * N.x + 10 * N.y + 5 * B.x + 5 * B.y
    assert O.pos_from(Q) == -10 * N.x - 10 * N.y - 5 * B.x - 5 * B.y

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_aux():
    # Same as above, except we have 2 auxiliary speeds for the ground contact
    # point, which is known to be zero. In one case, we go through then
    # substitute the aux. speeds in at the end (they are zero, as well as their
    # derivative), in the other case, we use the built-in auxiliary speed part
    # of KanesMethod. The equations from each should be the same.
    q1, q2, q3, u1, u2, u3 = dynamicsymbols('q1 q2 q3 u1 u2 u3')
    q1d, q2d, q3d, u1d, u2d, u3d = dynamicsymbols('q1 q2 q3 u1 u2 u3', 1)
    u4, u5, f1, f2 = dynamicsymbols('u4, u5, f1, f2')
    u4d, u5d = dynamicsymbols('u4, u5', 1)
    r, m, g = symbols('r m g')

    N = ReferenceFrame('N')
    Y = N.orientnew('Y', 'Axis', [q1, N.z])
    L = Y.orientnew('L', 'Axis', [q2, Y.x])
    R = L.orientnew('R', 'Axis', [q3, L.y])
    w_R_N_qd = R.ang_vel_in(N)
    R.set_ang_vel(N, u1 * L.x + u2 * L.y + u3 * L.z)

    C = Point('C')
    C.set_vel(N, u4 * L.x + u5 * (Y.z ^ L.x))
    Dmc = C.locatenew('Dmc', r * L.z)
    Dmc.v2pt_theory(C, N, R)
    Dmc.a2pt_theory(C, N, R)

    I = inertia(L, m / 4 * r**2, m / 2 * r**2, m / 4 * r**2)

    kd = [dot(R.ang_vel_in(N) - w_R_N_qd, uv) for uv in L]

    ForceList = [(Dmc, - m * g * Y.z), (C, f1 * L.x + f2 * (Y.z ^ L.x))]
    BodyD = RigidBody('BodyD', Dmc, R, m, (I, Dmc))
    BodyList = [BodyD]

    KM = KanesMethod(N, q_ind=[q1, q2, q3], u_ind=[u1, u2, u3, u4, u5],
                     kd_eqs=kd)
    with warnings.catch_warnings():
        warnings.filterwarnings("ignore", category=SymPyDeprecationWarning)
        (fr, frstar) = KM.kanes_equations(ForceList, BodyList)
    fr = fr.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5: 0})
    frstar = frstar.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5: 0})

    KM2 = KanesMethod(N, q_ind=[q1, q2, q3], u_ind=[u1, u2, u3], kd_eqs=kd,
                      u_auxiliary=[u4, u5])
    with warnings.catch_warnings():
        warnings.filterwarnings("ignore", category=SymPyDeprecationWarning)
        (fr2, frstar2) = KM2.kanes_equations(ForceList, BodyList)
    fr2 = fr2.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5: 0})
    frstar2 = frstar2.subs({u4d: 0, u5d: 0}).subs({u4: 0, u5: 0})

    frstar.simplify()
    frstar2.simplify()

    assert (fr - fr2).expand() == Matrix([0, 0, 0, 0, 0])
    assert (frstar - frstar2).expand() == Matrix([0, 0, 0, 0, 0])

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_point_a2pt_theorys():
    q = dynamicsymbols('q')
    qd = dynamicsymbols('q', 1)
    qdd = dynamicsymbols('q', 2)
    N = ReferenceFrame('N')
    B = N.orientnew('B', 'Axis', [q, N.z])
    O = Point('O')
    P = O.locatenew('P', 0)
    O.set_vel(N, 0)
    assert P.a2pt_theory(O, N, B) == 0
    P.set_pos(O, B.x)
    assert P.a2pt_theory(O, N, B) == (-qd**2) * B.x + (qdd) * B.y

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_point_v2pt_theorys():
    q = dynamicsymbols('q')
    qd = dynamicsymbols('q', 1)
    N = ReferenceFrame('N')
    B = N.orientnew('B', 'Axis', [q, N.z])
    O = Point('O')
    P = O.locatenew('P', 0)
    O.set_vel(N, 0)
    assert P.v2pt_theory(O, N, B) == 0
    P = O.locatenew('P', B.x)
    assert P.v2pt_theory(O, N, B) == (qd * B.z ^ B.x)
    O.set_vel(N, N.x)
    assert P.v2pt_theory(O, N, B) == N.x + qd * B.y

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def get_equations(m_val, g_val, l_val):
    # This function body is copyied from:
    # http://www.pydy.org/examples/double_pendulum.html
    # Retrieved 2015-09-29
    from sympy import symbols
    from sympy.physics.mechanics import (
        dynamicsymbols, ReferenceFrame, Point, Particle, KanesMethod
    )

    q1, q2 = dynamicsymbols('q1 q2')
    q1d, q2d = dynamicsymbols('q1 q2', 1)
    u1, u2 = dynamicsymbols('u1 u2')
    u1d, u2d = dynamicsymbols('u1 u2', 1)
    l, m, g = symbols('l m g')

    N = ReferenceFrame('N')
    A = N.orientnew('A', 'Axis', [q1, N.z])
    B = N.orientnew('B', 'Axis', [q2, N.z])

    A.set_ang_vel(N, u1 * N.z)
    B.set_ang_vel(N, u2 * N.z)

    O = Point('O')
    P = O.locatenew('P', l * A.x)
    R = P.locatenew('R', l * B.x)

    O.set_vel(N, 0)
    P.v2pt_theory(O, N, A)
    R.v2pt_theory(P, N, B)

    ParP = Particle('ParP', P, m)
    ParR = Particle('ParR', R, m)

    kd = [q1d - u1, q2d - u2]
    FL = [(P, m * g * N.x), (R, m * g * N.x)]
    BL = [ParP, ParR]

    KM = KanesMethod(N, q_ind=[q1, q2], u_ind=[u1, u2], kd_eqs=kd)

    (fr, frstar) = KM.kanes_equations(FL, BL)
    kdd = KM.kindiffdict()
    mm = KM.mass_matrix_full
    fo = KM.forcing_full
    qudots = mm.inv() * fo
    qudots = qudots.subs(kdd)
    qudots.simplify()
    # Edit:
    depv = [q1, q2, u1, u2]
    subs = list(zip([m, g, l], [m_val, g_val, l_val]))
    return zip(depv, [expr.subs(subs) for expr in qudots])

# 需要导入模块: from sympy.physics.mechanics import ReferenceFrame [as 别名]
# 或者: from sympy.physics.mechanics.ReferenceFrame import orientnew [as 别名]
def test_disc_on_an_incline_plane():
    # Disc rolling on an inclined plane
    # First the generalized coordinates are created. The mass center of the
    # disc is located from top vertex of the inclined plane by the generalized
    # coordinate 'y'. The orientation of the disc is defined by the angle
    # 'theta'. The mass of the disc is 'm' and its radius is 'R'. The length of
    # the inclined path is 'l', the angle of inclination is 'alpha'. 'g' is the
    # gravitational constant.
    y, theta = dynamicsymbols('y theta')
    yd, thetad = dynamicsymbols('y theta', 1)
    m, g, R, l, alpha = symbols('m g R l alpha')

    # Next, we create the inertial reference frame 'N'. A reference frame 'A'
    # is attached to the inclined plane. Finally a frame is created which is attached to the disk.
    N = ReferenceFrame('N')
    A = N.orientnew('A', 'Axis', [pi/2 - alpha, N.z])
    B = A.orientnew('B', 'Axis', [-theta, A.z])

    # Creating the disc 'D'; we create the point that represents the mass
    # center of the disc and set its velocity. The inertia dyadic of the disc
    # is created. Finally, we create the disc.
    Do = Point('Do')
    Do.set_vel(N, yd * A.x)
    I = m * R**2 / 2 * B.z | B.z
    D = RigidBody('D', Do, B, m, (I, Do))

    # To construct the Lagrangian, 'L', of the disc, we determine its kinetic
    # and potential energies, T and U, respectively. L is defined as the
    # difference between T and U.
    D.set_potential_energy(m * g * (l - y) * sin(alpha))
    L = Lagrangian(N, D)

    # We then create the list of generalized coordinates and constraint
    # equations. The constraint arises due to the disc rolling without slip on
    # on the inclined path. Also, the constraint is holonomic but we supply the
    # differentiated holonomic equation as the 'LagrangesMethod' class requires
    # that. We then invoke the 'LagrangesMethod' class and supply it the
    # necessary arguments and generate the equations of motion. The'rhs' method
    # solves for the q_double_dots (i.e. the second derivative with respect to
    # time  of the generalized coordinates and the lagrange multiplers.
    q = [y, theta]
    coneq = [yd - R * thetad]
    m = LagrangesMethod(L, q, coneq)
    m.form_lagranges_equations()
    rhs = m.rhs()
    rhs.simplify()
    assert rhs[2] == 2*g*sin(alpha)/3