本文整理汇总了Python中sympy.physics.mechanics.inertia函数的典型用法代码示例。如果您正苦于以下问题:Python inertia函数的具体用法?Python inertia怎么用?Python inertia使用的例子?那么恭喜您, 这里精选的函数代码示例或许可以为您提供帮助。
在下文中一共展示了inertia函数的20个代码示例,这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞,您的评价将有助于我们的系统推荐出更棒的Python代码示例。
示例1: test_inertia
def test_inertia():
N = ReferenceFrame('N')
ixx, iyy, izz = symbols('ixx iyy izz')
ixy, iyz, izx = symbols('ixy iyz izx')
assert inertia(N, ixx, iyy, izz) == (ixx * (N.x | N.x) + iyy *
(N.y | N.y) + izz * (N.z | N.z))
assert inertia(N, 0, 0, 0) == 0 * (N.x | N.x)
assert inertia(N, ixx, iyy, izz, ixy, iyz, izx) == (ixx * (N.x | N.x) +
ixy * (N.x | N.y) + izx * (N.x | N.z) + ixy * (N.y | N.x) + iyy *
(N.y | N.y) + iyz * (N.y | N.z) + izx * (N.z | N.x) + iyz * (N.z |
N.y) + izz * (N.z | N.z))
开发者ID:AdrianPotter,项目名称:sympy,代码行数:11,代码来源:test_functions.py
示例2: _create_inertia_dyadics
def _create_inertia_dyadics(self):
leg_inertia_dyadic = me.inertia(self.frames['leg'], 0, 0,
self.parameters['leg_inertia'])
torso_inertia_dyadic = me.inertia(self.frames['torso'], 0, 0,
self.parameters['torso_inertia'])
self.central_inertias = OrderedDict()
self.central_inertias['leg'] = (leg_inertia_dyadic,
self.points['leg_mass_center'])
self.central_inertias['torso'] = (torso_inertia_dyadic,
self.points['torso_mass_center'])
开发者ID:csu-hmc,项目名称:opty,代码行数:13,代码来源:model.py
示例3: test_specifying_coordinate_issue_339
def test_specifying_coordinate_issue_339():
"""This test ensures that you can use derivatives as specified values."""
# beta will be a specified angle
beta = me.dynamicsymbols('beta')
q1, q2, q3, q4 = me.dynamicsymbols('q1, q2, q3, q4')
u1, u2, u3, u4 = me.dynamicsymbols('u1, u2, u3, u4')
N = me.ReferenceFrame('N')
A = N.orientnew('A', 'Axis', (q1, N.x))
B = A.orientnew('B', 'Axis', (beta, A.y))
No = me.Point('No')
Ao = No.locatenew('Ao', q2 * N.x + q3 * N.y + q4 * N.z)
Bo = Ao.locatenew('Bo', 10 * A.x + 10 * A.y + 10 * A.z)
A.set_ang_vel(N, u1 * N.x)
B.ang_vel_in(N) # compute it automatically
No.set_vel(N, 0)
Ao.set_vel(N, u2 * N.x + u3 * N.y + u4 * N.z)
Bo.v2pt_theory(Ao, N, B)
body_A = me.RigidBody('A', Ao, A, 1.0, (me.inertia(A, 1, 2, 3), Ao))
body_B = me.RigidBody('B', Bo, B, 1.0, (me.inertia(A, 3, 2, 1), Bo))
bodies = [body_A, body_B]
# TODO : This should be able to be simple an empty iterable.
loads = [(No, 0 * N.x)]
kdes = [u1 - q1.diff(),
u2 - q2.diff(),
u3 - q3.diff(),
u4 - q4.diff()]
kane = me.KanesMethod(N, q_ind=[q1, q2, q3, q4],
u_ind=[u1, u2, u3, u4], kd_eqs=kdes)
if sympy_newer_than('1.0'):
fr, frstar = kane.kanes_equations(bodies, loads)
else:
fr, frstar = kane.kanes_equations(loads, bodies)
sys = System(kane)
sys.specifieds = {(beta, beta.diff(), beta.diff().diff()):
lambda x, t: np.array([1.0, 1.0, 1.0])}
sys.times = np.linspace(0, 10, 20)
sys.integrate()
开发者ID:oliverlee,项目名称:pydy,代码行数:51,代码来源:test_system.py
示例4: __init__
def __init__(self):
#We define some quantities required for tests here..
self.p = dynamicsymbols('p:3')
self.q = dynamicsymbols('q:3')
self.dynamic = list(self.p) + list(self.q)
self.states = [radians(45) for x in self.p] + \
[radians(30) for x in self.q]
self.I = ReferenceFrame('I')
self.A = self.I.orientnew('A', 'space', self.p, 'XYZ')
self.B = self.A.orientnew('B', 'space', self.q, 'XYZ')
self.O = Point('O')
self.P1 = self.O.locatenew('P1', 10 * self.I.x + \
10 * self.I.y + 10 * self.I.z)
self.P2 = self.P1.locatenew('P2', 10 * self.I.x + \
10 * self.I.y + 10 * self.I.z)
self.point_list1 = [[2, 3, 1], [4, 6, 2], [5, 3, 1], [5, 3, 6]]
self.point_list2 = [[3, 1, 4], [3, 8, 2], [2, 1, 6], [2, 1, 1]]
self.shape1 = Cylinder()
self.shape2 = Cylinder()
self.Ixx, self.Iyy, self.Izz = symbols('Ixx Iyy Izz')
self.mass = symbols('mass')
self.parameters = [self.Ixx, self.Iyy, self.Izz, self.mass]
self.param_vals = [0, 0, 0, 0]
self.inertia = inertia(self.A, self.Ixx, self.Iyy, self.Izz)
self.rigid_body = RigidBody('rigid_body1', self.P1, self.A, \
self.mass, (self.inertia, self.P1))
self.global_frame1 = VisualizationFrame('global_frame1', \
self.A, self.P1, self.shape1)
self.global_frame2 = VisualizationFrame('global_frame2', \
self.B, self.P2, self.shape2)
self.scene1 = Scene(self.I, self.O, \
(self.global_frame1, self.global_frame2), \
name='scene')
self.particle = Particle('particle1', self.P1, self.mass)
#To make it more readable
p = self.p
q = self.q
#Here is the dragon ..
self.transformation_matrix = \
[[cos(p[1])*cos(p[2]), sin(p[2])*cos(p[1]), -sin(p[1]), 0], \
[sin(p[0])*sin(p[1])*cos(p[2]) - sin(p[2])*cos(p[0]), \
sin(p[0])*sin(p[1])*sin(p[2]) + cos(p[0])*cos(p[2]), \
sin(p[0])*cos(p[1]), 0], \
[sin(p[0])*sin(p[2]) + sin(p[1])*cos(p[0])*cos(p[2]), \
-sin(p[0])*cos(p[2]) + sin(p[1])*sin(p[2])*cos(p[0]), \
cos(p[0])*cos(p[1]), 0], \
[10, 10, 10, 1]]
开发者ID:jcrist,项目名称:pydy-viz,代码行数:60,代码来源:test_visualization_frame_scene.py
示例5: test_pendulum_angular_momentum
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
开发者ID:A-turing-machine,项目名称:sympy,代码行数:28,代码来源:test_rigidbody.py
示例6: test_body_add_force
def test_body_add_force():
# Body with RigidBody.
rigidbody_masscenter = Point('rigidbody_masscenter')
rigidbody_mass = Symbol('rigidbody_mass')
rigidbody_frame = ReferenceFrame('rigidbody_frame')
body_inertia = inertia(rigidbody_frame, 1, 0, 0)
rigid_body = Body('rigidbody_body', rigidbody_masscenter, rigidbody_mass,
rigidbody_frame, body_inertia)
l = Symbol('l')
Fa = Symbol('Fa')
point = rigid_body.masscenter.locatenew(
'rigidbody_body_point0',
l * rigid_body.frame.x)
point.set_vel(rigid_body.frame, 0)
force_vector = Fa * rigid_body.frame.z
# apply_force with point
rigid_body.apply_force(force_vector, point)
assert len(rigid_body.loads) == 1
force_point = rigid_body.loads[0][0]
frame = rigid_body.frame
assert force_point.vel(frame) == point.vel(frame)
assert force_point.pos_from(force_point) == point.pos_from(force_point)
assert rigid_body.loads[0][1] == force_vector
# apply_force without point
rigid_body.apply_force(force_vector)
assert len(rigid_body.loads) == 2
assert rigid_body.loads[1][1] == force_vector
# passing something else than point
raises(TypeError, lambda: rigid_body.apply_force(force_vector, 0))
raises(TypeError, lambda: rigid_body.apply_force(0))
开发者ID:KonstantinTogoi,项目名称:sympy,代码行数:31,代码来源:test_body.py
示例7: test_parallel_axis
def test_parallel_axis():
# This is for a 2 dof inverted pendulum on a cart.
# This tests the parallel axis code in Kane. The inertia of the pendulum is
# defined about the hinge, not about the center of mass.
# Defining the constants and knowns of the system
gravity = symbols('g')
k, ls = symbols('k ls')
a, mA, mC = symbols('a mA mC')
F = dynamicsymbols('F')
Ix, Iy, Iz = symbols('Ix Iy Iz')
# Declaring the Generalized coordinates and speeds
q1, q2 = dynamicsymbols('q1 q2')
q1d, q2d = dynamicsymbols('q1 q2', 1)
u1, u2 = dynamicsymbols('u1 u2')
u1d, u2d = dynamicsymbols('u1 u2', 1)
# Creating reference frames
N = ReferenceFrame('N')
A = ReferenceFrame('A')
A.orient(N, 'Axis', [-q2, N.z])
A.set_ang_vel(N, -u2 * N.z)
# Origin of Newtonian reference frame
O = Point('O')
# Creating and Locating the positions of the cart, C, and the
# center of mass of the pendulum, A
C = O.locatenew('C', q1 * N.x)
Ao = C.locatenew('Ao', a * A.y)
# Defining velocities of the points
O.set_vel(N, 0)
C.set_vel(N, u1 * N.x)
Ao.v2pt_theory(C, N, A)
Cart = Particle('Cart', C, mC)
Pendulum = RigidBody('Pendulum', Ao, A, mA, (inertia(A, Ix, Iy, Iz), C))
# kinematical differential equations
kindiffs = [q1d - u1, q2d - u2]
bodyList = [Cart, Pendulum]
forceList = [(Ao, -N.y * gravity * mA),
(C, -N.y * gravity * mC),
(C, -N.x * k * (q1 - ls)),
(C, N.x * F)]
km=Kane(N)
km.coords([q1, q2])
km.speeds([u1, u2])
km.kindiffeq(kindiffs)
(fr,frstar) = km.kanes_equations(forceList, bodyList)
mm = km.mass_matrix_full
assert mm[3, 3] == -Iz
开发者ID:johanhake,项目名称:sympy,代码行数:58,代码来源:test_kane.py
示例8: test_aux
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()
开发者ID:101man,项目名称:sympy,代码行数:57,代码来源:test_kane.py
示例9: test_aux
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])
开发者ID:AStorus,项目名称:sympy,代码行数:54,代码来源:test_kane.py
示例10: parallel_axis
def parallel_axis(self, point):
"""Returns the inertia of the body about another point."""
# TODO : What if the new point is not fixed in the rigid body's frame?
a, b, c = self.masscenter.pos_from(point).to_matrix(self.frame)
return self.central_inertia + self.mass * inertia(self.frame,
b**2 + c**2,
c**2 + a**2,
a**2 + b**2,
-a * b,
-b * c,
-a * c)
开发者ID:moorepants,项目名称:BMD2016,代码行数:11,代码来源:falkor_inertia.py
示例11: test_parallel_axis
def test_parallel_axis():
# This is for a 2 dof inverted pendulum on a cart.
# This tests the parallel axis code in KanesMethod. The inertia of the
# pendulum is defined about the hinge, not about the center of mass.
# Defining the constants and knowns of the system
gravity = symbols("g")
k, ls = symbols("k ls")
a, mA, mC = symbols("a mA mC")
F = dynamicsymbols("F")
Ix, Iy, Iz = symbols("Ix Iy Iz")
# Declaring the Generalized coordinates and speeds
q1, q2 = dynamicsymbols("q1 q2")
q1d, q2d = dynamicsymbols("q1 q2", 1)
u1, u2 = dynamicsymbols("u1 u2")
u1d, u2d = dynamicsymbols("u1 u2", 1)
# Creating reference frames
N = ReferenceFrame("N")
A = ReferenceFrame("A")
A.orient(N, "Axis", [-q2, N.z])
A.set_ang_vel(N, -u2 * N.z)
# Origin of Newtonian reference frame
O = Point("O")
# Creating and Locating the positions of the cart, C, and the
# center of mass of the pendulum, A
C = O.locatenew("C", q1 * N.x)
Ao = C.locatenew("Ao", a * A.y)
# Defining velocities of the points
O.set_vel(N, 0)
C.set_vel(N, u1 * N.x)
Ao.v2pt_theory(C, N, A)
Cart = Particle("Cart", C, mC)
Pendulum = RigidBody("Pendulum", Ao, A, mA, (inertia(A, Ix, Iy, Iz), C))
# kinematical differential equations
kindiffs = [q1d - u1, q2d - u2]
bodyList = [Cart, Pendulum]
forceList = [(Ao, -N.y * gravity * mA), (C, -N.y * gravity * mC), (C, -N.x * k * (q1 - ls)), (C, N.x * F)]
km = KanesMethod(N, [q1, q2], [u1, u2], kindiffs)
with warnings.catch_warnings():
warnings.filterwarnings("ignore", category=SymPyDeprecationWarning)
(fr, frstar) = km.kanes_equations(forceList, bodyList)
mm = km.mass_matrix_full
assert mm[3, 3] == Iz
开发者ID:ashutoshsaboo,项目名称:sympy,代码行数:54,代码来源:test_kane.py
示例12: test_rolling_disc
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)
开发者ID:Acebulf,项目名称:sympy,代码行数:54,代码来源:test_lagrange.py
示例13: test_default
def test_default():
body = Body('body')
assert body.name == 'body'
assert body.loads == []
point = Point('body_masscenter')
point.set_vel(body.frame, 0)
com = body.masscenter
frame = body.frame
assert com.vel(frame) == point.vel(frame)
assert body.mass == Symbol('body_mass')
ixx, iyy, izz = symbols('body_ixx body_iyy body_izz')
ixy, iyz, izx = symbols('body_ixy body_iyz body_izx')
assert body.inertia == (inertia(body.frame, ixx, iyy, izz, ixy, iyz, izx),
body.masscenter)
开发者ID:KonstantinTogoi,项目名称:sympy,代码行数:14,代码来源:test_body.py
示例14: test_custom_rigid_body
def test_custom_rigid_body():
# Body with RigidBody.
rigidbody_masscenter = Point('rigidbody_masscenter')
rigidbody_mass = Symbol('rigidbody_mass')
rigidbody_frame = ReferenceFrame('rigidbody_frame')
body_inertia = inertia(rigidbody_frame, 1, 0, 0)
rigid_body = Body('rigidbody_body', rigidbody_masscenter, rigidbody_mass,
rigidbody_frame, body_inertia)
com = rigid_body.masscenter
frame = rigid_body.frame
rigidbody_masscenter.set_vel(rigidbody_frame, 0)
assert com.vel(frame) == rigidbody_masscenter.vel(frame)
assert com.pos_from(com) == rigidbody_masscenter.pos_from(com)
assert rigid_body.mass == rigidbody_mass
assert rigid_body.inertia == (body_inertia, rigidbody_masscenter)
assert hasattr(rigid_body, 'masscenter')
assert hasattr(rigid_body, 'mass')
assert hasattr(rigid_body, 'frame')
assert hasattr(rigid_body, 'inertia')
开发者ID:KonstantinTogoi,项目名称:sympy,代码行数:21,代码来源:test_body.py
示例15: __init__
def __init__(self, name, masscenter=None, mass=None, frame=None,
central_inertia=None):
self.name = name
self.loads = []
if frame is None:
frame = ReferenceFrame(name + '_frame')
if masscenter is None:
masscenter = Point(name + '_masscenter')
if central_inertia is None and mass is None:
ixx = Symbol(name + '_ixx')
iyy = Symbol(name + '_iyy')
izz = Symbol(name + '_izz')
izx = Symbol(name + '_izx')
ixy = Symbol(name + '_ixy')
iyz = Symbol(name + '_iyz')
_inertia = (inertia(frame, ixx, iyy, izz, ixy, iyz, izx),
masscenter)
else:
_inertia = (central_inertia, masscenter)
if mass is None:
_mass = Symbol(name + '_mass')
else:
_mass = mass
masscenter.set_vel(frame, 0)
# If user passes masscenter and mass then a particle is created
# otherwise a rigidbody. As a result a body may or may not have inertia.
if central_inertia is None and mass is not None:
self.frame = frame
self.masscenter = masscenter
Particle.__init__(self, name, masscenter, _mass)
else:
RigidBody.__init__(self, name, masscenter, frame, _mass, _inertia)
开发者ID:arghdos,项目名称:sympy,代码行数:39,代码来源:body.py
示例16: test_linearize_rolling_disc_lagrange
def test_linearize_rolling_disc_lagrange():
q1, q2, q3 = q = dynamicsymbols("q1 q2 q3")
q1d, q2d, q3d = qd = dynamicsymbols("q1 q2 q3", 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])
C = Point("C")
C.set_vel(N, 0)
Dmc = C.locatenew("Dmc", r * L.z)
Dmc.v2pt_theory(C, N, R)
I = inertia(L, m / 4 * r ** 2, m / 2 * r ** 2, m / 4 * r ** 2)
BodyD = RigidBody("BodyD", Dmc, R, m, (I, Dmc))
BodyD.potential_energy = -m * g * r * cos(q2)
Lag = Lagrangian(N, BodyD)
l = LagrangesMethod(Lag, q)
l.form_lagranges_equations()
# Linearize about steady-state upright rolling
op_point = {q1: 0, q2: 0, q3: 0, q1d: 0, q2d: 0, q1d.diff(): 0, q2d.diff(): 0, q3d.diff(): 0}
A = l.linearize(q_ind=q, qd_ind=qd, op_point=op_point, A_and_B=True)[0]
sol = Matrix(
[
[0, 0, 0, 1, 0, 0],
[0, 0, 0, 0, 1, 0],
[0, 0, 0, 0, 0, 1],
[0, 0, 0, 0, -6 * q3d, 0],
[0, -4 * g / (5 * r), 0, 6 * q3d / 5, 0, 0],
[0, 0, 0, 0, 0, 0],
]
)
assert A == sol
开发者ID:guanlongtianzi,项目名称:sympy,代码行数:38,代码来源:test_linearize.py
示例17: symbols
body_mass_center.v2pt_theory(l_hip, inertial_frame, body_frame)
r_leg_mass_center.v2pt_theory(r_hip, inertial_frame, body_frame)
# Mass
# ====
l_leg_mass, body_mass, r_leg_mass = symbols("m_L, m_B, m_R")
# Inertia
# =======
l_leg_inertia, body_inertia, r_leg_inertia = symbols("I_Lz, I_Bz, I_Rz")
l_leg_inertia_dyadic = inertia(l_leg_frame, 0, 0, l_leg_inertia)
l_leg_central_inertia = (l_leg_inertia_dyadic, l_leg_mass_center)
body_inertia_dyadic = inertia(body_frame, 0, 0, body_inertia)
body_central_inertia = (body_inertia_dyadic, body_mass_center)
r_leg_inertia_dyadic = inertia(body_frame, 0, 0, r_leg_inertia)
r_leg_central_inertia = (r_leg_inertia_dyadic, r_leg_mass_center)
# Rigid Bodies
# ============
l_leg = RigidBody("Lower Leg", l_leg_mass_center, l_leg_frame, l_leg_mass, l_leg_central_inertia)
开发者ID:notokay,项目名称:robot_balancing,代码行数:30,代码来源:double_block_setup.py
示例18: test_aux_dep
#.........这里部分代码省略.........
# is q[3].
# Velocity constraints: f_v, for u3, u4 and u5.
# Acceleration constraints: f_a.
f_c = Matrix([dot(-r*B.z, A.z) - q[3]])
f_v = Matrix([dot(O.vel(N) - (P.vel(N) + cross(C.ang_vel_in(N),
O.pos_from(P))), ai).expand() for ai in A])
v_o_n = cross(C.ang_vel_in(N), O.pos_from(P))
a_o_n = v_o_n.diff(t, A) + cross(A.ang_vel_in(N), v_o_n)
f_a = Matrix([dot(O.acc(N) - a_o_n, ai) for ai in A])
# Solve for constraint equations in the form of
# u_dependent = A_rs * [u_i; u_aux].
# First, obtain constraint coefficient matrix: M_v * [u; ua] = 0;
# Second, taking u[0], u[1], u[2] as independent,
# taking u[3], u[4], u[5] as dependent,
# rearranging the matrix of M_v to be A_rs for u_dependent.
# Third, u_aux ==0 for u_dep, and resulting dictionary of u_dep_dict.
M_v = zeros(3, 9)
for i in range(3):
for j, ui in enumerate(u + ua):
M_v[i, j] = f_v[i].diff(ui)
M_v_i = M_v[:, :3]
M_v_d = M_v[:, 3:6]
M_v_aux = M_v[:, 6:]
M_v_i_aux = M_v_i.row_join(M_v_aux)
A_rs = - M_v_d.inv() * M_v_i_aux
u_dep = A_rs[:, :3] * Matrix(u[:3])
u_dep_dict = dict(zip(u[3:], u_dep))
#u_dep_dict = {udi : u_depi[0] for udi, u_depi in zip(u[3:], u_dep.tolist())}
# Active forces: F_O acting on point O; F_P acting on point P.
# Generalized active forces (unconstrained): Fr_u = F_point * pv_point.
F_O = m*g*A.z
F_P = Fx * A.x + Fy * A.y + Fz * A.z
Fr_u = Matrix([dot(F_O, pv_o) + dot(F_P, pv_p) for pv_o, pv_p in
zip(partial_v_O, partial_v_P)])
# Inertia force: R_star_O.
# Inertia of disc: I_C_O, where J is a inertia component about principal axis.
# Inertia torque: T_star_C.
# Generalized inertia forces (unconstrained): Fr_star_u.
R_star_O = -m*O.acc(N)
I_C_O = inertia(B, I, J, I)
T_star_C = -(dot(I_C_O, C.ang_acc_in(N)) \
+ cross(C.ang_vel_in(N), dot(I_C_O, C.ang_vel_in(N))))
Fr_star_u = Matrix([dot(R_star_O, pv) + dot(T_star_C, pav) for pv, pav in
zip(partial_v_O, partial_w_C)])
# Form nonholonomic Fr: Fr_c, and nonholonomic Fr_star: Fr_star_c.
# Also, nonholonomic Fr_star in steady turning condition: Fr_star_steady.
Fr_c = Fr_u[:3, :].col_join(Fr_u[6:, :]) + A_rs.T * Fr_u[3:6, :]
Fr_star_c = Fr_star_u[:3, :].col_join(Fr_star_u[6:, :])\
+ A_rs.T * Fr_star_u[3:6, :]
Fr_star_steady = Fr_star_c.subs(ud_zero).subs(u_dep_dict)\
.subs(steady_conditions).subs({q[3]: -r*cos(q[1])}).expand()
# Second, using KaneMethod in mechanics for fr, frstar and frstar_steady.
# Rigid Bodies: disc, with inertia I_C_O.
iner_tuple = (I_C_O, O)
disc = RigidBody('disc', O, C, m, iner_tuple)
bodyList = [disc]
# Generalized forces: Gravity: F_o; Auxiliary forces: F_p.
F_o = (O, F_O)
F_p = (P, F_P)
forceList = [F_o, F_p]
# KanesMethod.
kane = KanesMethod(
N, q_ind= q[:3], u_ind= u[:3], kd_eqs=kindiffs,
q_dependent=q[3:], configuration_constraints = f_c,
u_dependent=u[3:], velocity_constraints= f_v,
u_auxiliary=ua
)
# fr, frstar, frstar_steady and kdd(kinematic differential equations).
(fr, frstar)= kane.kanes_equations(forceList, bodyList)
frstar_steady = frstar.subs(ud_zero).subs(u_dep_dict).subs(steady_conditions)\
.subs({q[3]: -r*cos(q[1])}).expand()
kdd = kane.kindiffdict()
# Test
# First try Fr_c == fr;
# Second try Fr_star_c == frstar;
# Third try Fr_star_steady == frstar_steady.
# Both signs are checked in case the equations were found with an inverse
# sign.
assert ((Matrix(Fr_c).expand() == fr.expand()) or
(Matrix(Fr_c).expand() == (-fr).expand()))
assert ((Matrix(Fr_star_c).expand() == frstar.expand()) or
(Matrix(Fr_star_c).expand() == (-frstar).expand()))
assert ((Matrix(Fr_star_steady).expand() == frstar_steady.expand()) or
(Matrix(Fr_star_steady).expand() == (-frstar_steady).expand()))
开发者ID:Acebulf,项目名称:sympy,代码行数:101,代码来源:test_kane2.py
示例19: test_rolling_disc
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 three
# speed variables are need to describe this system, along with the disc's
# mass and radius, and the local graivty (note that mass will drop out).
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)
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])
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)))
# 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 mass center.
# 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)
Dmc.a2pt_theory(C, N, R)
# This is a simple way to form the inertia dyadic.
I = inertia(L, m / 4 * r**2, m / 2 * r**2, m / 4 * r**2)
# Kinematic differential equations; how the generalized coordinate time
# derivatives relate to generalized speeds.
kd = [q1d - u3/cos(q3), q2d - u1, q3d - u2 + u3 * tan(q2)]
# Creation of the force list; it is the gravitational force at the mass
# center of the disc. Then we create the disc by assigning a Point to the
# mass center attribute, a ReferenceFrame to the frame attribute, and mass
# and inertia. Then we form the body list.
ForceList = [(Dmc, - m * g * Y.z)]
BodyD = RigidBody()
BodyD.mc = Dmc
BodyD.inertia = (I, Dmc)
BodyD.frame = R
BodyD.mass = m
BodyList = [BodyD]
# Finally we form the equations of motion, using the same steps we did
# before. Specify inertial frame, supply generalized speeds, supply
# kinematic differential equation dictionary, compute Fr from the force
# list and Fr* fromt the body list, compute the mass matrix and forcing
# terms, then solve for the u dots (time derivatives of the generalized
# speeds).
KM = Kane(N)
KM.coords([q1, q2, q3])
KM.speeds([u1, u2, u3])
KM.kindiffeq(kd)
KM.kanes_equations(ForceList, BodyList)
MM = KM.mass_matrix
forcing = KM.forcing
rhs = MM.inv() * forcing
kdd = KM.kindiffdict()
rhs = rhs.subs(kdd)
assert rhs.expand() == Matrix([(10*u2*u3*r - 5*u3**2*r*tan(q2) +
4*g*sin(q2))/(5*r), -2*u1*u3/3, u1*(-2*u2 + u3*tan(q2))]).expand()
开发者ID:101man,项目名称:sympy,代码行数:69,代码来源:test_kane.py
示例20: ReferenceFrame
l: 2,
w: 1,
f: 2,
v0: 20}
N = ReferenceFrame('N')
B = N.orientnew('B', 'axis', [q3, N.z])
O = Point('O')
S = O.locatenew('S', q1*N.x + q2*N.y)
S.set_vel(N, S.pos_from(O).dt(N))
#Is = m/12*(l**2 + w**2)
Is = symbols('Is')
I = inertia(B, 0, 0, Is, 0, 0, 0)
rb = RigidBody('rb', S, B, m, (I, S))
rb.set_potential_energy(0)
L = Lagrangian(N, rb)
lm = LagrangesMethod(
L, q, nonhol_coneqs = [q1d*sin(q3) - q2d*cos(q3) + l/2*q3d])
lm.form_lagranges_equations()
rhs = lm.rhs()
print('{} = {}'.format(msprint(q1d.diff(t)),
msprint(rhs[3].simplify())))
print('{} = {}'.format(msprint(q2d.diff(t)),
msprint(rhs[4].simplify())))
print('{} = {}'.format(msprint(q3d.diff(t)),
msprint(rhs[5].simplify())))
开发者ID:oliverlee,项目名称:advanced_dynamics,代码行数:31,代码来源:hw8.4.py
注:本文中的sympy.physics.mechanics.inertia函数示例由纯净天空整理自Github/MSDocs等源码及文档管理平台,相关代码片段筛选自各路编程大神贡献的开源项目,源码版权归原作者所有,传播和使用请参考对应项目的License;未经允许,请勿转载。 |
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