def test_lqr_discrete(self):
"""Test overloading of lqr operator for discrete time systems"""
csys = ct.rss(2, 1, 1)
dsys = ct.drss(2, 1, 1)
Q = np.eye(2)
R = np.eye(1)
# Calling with a system versus explicit A, B should be the sam
K_csys, S_csys, E_csys = ct.lqr(csys, Q, R)
K_expl, S_expl, E_expl = ct.lqr(csys.A, csys.B, Q, R)
np.testing.assert_almost_equal(K_csys, K_expl)
np.testing.assert_almost_equal(S_csys, S_expl)
np.testing.assert_almost_equal(E_csys, E_expl)
# Calling lqr() with a discrete time system should call dlqr()
K_lqr, S_lqr, E_lqr = ct.lqr(dsys, Q, R)
K_dlqr, S_dlqr, E_dlqr = ct.dlqr(dsys, Q, R)
np.testing.assert_almost_equal(K_lqr, K_dlqr)
np.testing.assert_almost_equal(S_lqr, S_dlqr)
np.testing.assert_almost_equal(E_lqr, E_dlqr)
# Calling lqr() with no timebase should call lqr()
asys = ct.ss(csys.A, csys.B, csys.C, csys.D, dt=None)
K_asys, S_asys, E_asys = ct.lqr(asys, Q, R)
K_expl, S_expl, E_expl = ct.lqr(csys.A, csys.B, Q, R)
np.testing.assert_almost_equal(K_asys, K_expl)
np.testing.assert_almost_equal(S_asys, S_expl)
np.testing.assert_almost_equal(E_asys, E_expl)
# Calling dlqr() with a continuous time system should raise an error
with pytest.raises(ControlArgument, match="dsys must be discrete"):
K, S, E = ct.dlqr(csys, Q, R)
def gainCallBack(self, req):
# start_time = time.time()
self.updateModel(req.l)
k1, _, _ = lqr(self.sys1, self.Q1, self.R1)
k2, _, _ = lqr(self.sys2, self.Q2, self.R2)
res = GainResponse(k1.flatten().tolist() + k2.flatten().tolist())
print(res)
# rospy.loginfo("--- %s seconds ---" % (time.time() - start_time))
return res
def control(self, dt, x, goal_x, est_params):
if hasattr(self, '_N'):
K, S, E = control.lqr(self._model.A, self._model.B, self._Q, self._R, self._N)
else:
K, S, E = control.lqr(self._model.A, self._model.B, self._Q, self._R)
self._K = K
output = - self._K @ x
return output
def getGainK(self):
#S = self.getRiccatiSolution()
#S1 = self.B.T.dot(S)
#if self.N is not None: S1 += self.N.T
#K = np.linalg.inv(self.R).dot(S1)
if self.N is None:
K, S, E = control.lqr(self.A, self.B, self.Q, self.R)
else:
K, S, E = control.lqr(self.A, self.B, self.Q, self.R, self.N)
return K
def test_lqr_integral_discrete(self):
# Generate a discrete time system for testing
sys = ct.drss(4, 4, 2, strictly_proper=True)
sys.C = np.eye(4) # reset output to be full state
C_int = np.eye(2, 4) # integrate outputs for first two states
nintegrators = C_int.shape[0]
# Generate a controller with integral action
K, _, _ = ct.lqr(sys,
np.eye(sys.nstates + nintegrators),
np.eye(sys.ninputs),
integral_action=C_int)
Kp, Ki = K[:, :sys.nstates], K[:, sys.nstates:]
# Create an I/O system for the controller
ctrl, clsys = ct.create_statefbk_iosystem(sys,
K,
integral_action=C_int)
# Construct the state space matrices by hand
A_ctrl = np.eye(nintegrators)
B_ctrl = np.block(
[[-C_int, np.zeros((nintegrators, sys.ninputs)), C_int]])
C_ctrl = -K[:, sys.nstates:]
D_ctrl = np.block([[Kp, np.eye(nintegrators), -Kp]])
# Check to make sure everything matches
assert ct.isdtime(clsys)
np.testing.assert_array_almost_equal(ctrl.A, A_ctrl)
np.testing.assert_array_almost_equal(ctrl.B, B_ctrl)
np.testing.assert_array_almost_equal(ctrl.C, C_ctrl)
np.testing.assert_array_almost_equal(ctrl.D, D_ctrl)
def lqr_control():
#ignore the platform mass and interia
m = 10 #blue bass mass
mw = 0.4 #wheel mass
h = 0.8 #center of mass height(roughly)
g = 9.8 #gravity coefficient
r = 0.1 #wheel radius
Iw = 0.15 #moment of inertia of wheel about y
Iz = 0.5 * mw * r**2 #moment of inertia of robotbase about z
# reference chapter 4 lqr model
t1 =
t2 =
t3 =
t4 =
t5 =
A = np.array([[0,1,0,0,0,0],
[t1,0,0,0,0,0],
[0,0,0,1,0,0],
[t2,0,0,0,0,0],
[0,0,0,0,0,1],
[0,0,0,0,0,0]])
B = np.array([[0,0],
[t3,0],
[0,0],
[t4,0],
[0,0],
[0,t5]])
Q = np.eye(6)
R = np.eye(2)
K,S,E = lqr(A,B,Q,R)
print(K)
return K
def lqr_control(self, traj, t):
"""
Get the control input for a given instant, given
a desired trajectory
Based on a Taylor linearization, so we're assuming the
actual location is pretty close to the desired one.
"""
A = np.array([[
0, 0, -traj.vdes(t) * np.sin(traj.theta_des(t)),
np.cos(traj.theta_des(t)), 0
],
[
0, 0,
traj.vdes(t) * np.cos(traj.theta_des(t)),
np.sin(traj.theta_des(t)), 0
], [0, 0, 0, 0, 1], [0, 0, 0, 0, 0], [0, 0, 0, 0, 0]])
B = np.array([[0, 0], [0, 0], [0, 0], [1, 0], [0, 1]])
Q = np.array([[1, 0, 0, 0, 0], [0, 1, 0, 0, 0], [0, 0, 1, 0, 0],
[0, 0, 0, 1, 0], [0, 0, 0, 0, 1]])
R = np.array([[1, 0], [0, 1]])
K, S, E = control.lqr(A, B, Q, R)
x = self.current_extended_state(traj, t)
u = np.matmul(-K, x)
return u
def lqr_sys(A, B, C, D, in_q, r=1, num_q=6):
#parameter
sys = control.StateSpace(A, B, C, D)
Q = np.zeros((num_q, num_q))
R = [r]
for i in range(num_q):
Q[i, i] = in_q[i]
K, solu_R, Eig_sys = control.lqr(sys, Q, r)
kr = -1 / np.matmul(np.matmul(C, npl.inv((A - np.matmul(B, K)))), B)[0]
pole, eig_v = npl.eig(A - B * K)
pole_real = [a.real for a in pole]
minpol = -3 + min(pole_real)
repol = []
for i in range(num_q):
repol.append(minpol + i + 1)
repol = np.array(repol)
L = scis.place_poles(A.transpose(), C.transpose(), repol).gain_matrix
L = L.transpose()
upCA = np.column_stack(((A - np.matmul(B, K)), (np.matmul(B, K))))
downCA = np.column_stack((np.zeros((num_q, num_q)), (A - np.matmul(L, C))))
CA = np.row_stack((upCA, downCA))
CB = np.row_stack((B * kr, np.zeros((num_q, 1))))
CC = np.column_stack((C, np.zeros((1, num_q))))
CD = np.array([0])
return CA, CB, CC, CD
def test_lqr():
control_spec = {
'feedback': 'LQR',
'params': {
'feedback': {
'Q': np.array([[1, 0], [0, 1]]),
'R': 1
}
}
}
model = Model(np.array([[0, 1], [1, 0]]), [[0], [1]])
dt = 0.01
x = np.array([[1], [1]])
goal_x = np.array([[0], [0]])
est_params = []
test_controller = controller.Controller(control_spec, model)
output = test_controller.control(dt, x, goal_x, est_params)
# expected results
K, S, E = control.lqr(model.A, model.B,
control_spec['params']['feedback']['Q'],
control_spec['params']['feedback']['R'])
expec_output = -K @ x
assert output == expec_output
def policy_rollout(self):
A, B = self.get_system()
Q = np.eye(self.hidden_dim)
R = np.array([[0.01]])
K, _, _ = control.lqr(A, B, Q, R)
ref = torch.FloatTensor([[1.0, 0., 0.]])
ref = model.encoder(ref).detach().numpy()
obs_old = self.transform_state(self.env.reset())
#obs_old[2] = obs_old[2] / 8.0
for _ in range(100):
if np.random.random() > 0.5:
state = torch.FloatTensor(obs_old.reshape((1, -1)))
y = model.encoder(state).detach().numpy()
action = -np.dot(K, (y-ref).T)
action = np.clip(np.array([action.item()]), self.env.action_space.low, self.env.action_space.high)
else:
action = self.env.action_space.sample() * 0.4
#self.env.render()
obs, reward, done, info = self.env.step(action)
#obs[2] = obs[2] / 8.0
obs = self.transform_state(obs)
self.replay_buffer.push((obs_old, action / 2.0, obs))
obs_old = obs
def LQR(plant, x):
A = np.matrix(
[[0, 1, 0, 0],
[0, 0, plant.params['g'] * plant.params['m'] / plant.params['M'], 0],
[0, 0, 0, 1],
[
0, 0, (plant.params['M'] + plant.params['m']) *
plant.params['g'] / (plant.params['l'] * plant.params['M']), 0
]])
B = np.matrix([[0], [1 / plant.params['M']], [0],
[1 / (plant.params['l'] * plant.params['M'])]])
# The Q and R matrices are emperically tuned. It is described further in the report
Q = np.matrix([[1, 0, 0, 0], [0, 0.01, 0, 0], [0, 0, 15, 0], [0, 0, 0,
11]])
R = np.matrix([5])
# The K matrix is calculated using the lqr function from the controls library
K, S, E = control.lqr(A, B, Q, R)
np.matrix(K)
x = np.matrix([[-np.squeeze(np.asarray(x[0]))],
[np.squeeze(np.asarray(x[1]))],
[np.squeeze(np.asarray(np.arcsin(x[3])))],
[-np.squeeze(np.asarray(x[2]))]])
desired = np.matrix([[0], [0], [0], [0]])
F = (K * (x - desired))
return np.array(F)
def clfqp_a(self, X, Xd, Ud):
#Xn = np.array([1,np.pi/3,1,np.pi/3])
#An = self.sdcA(Xn)
#Bn = self.dynamicsg(Xn)
e = X - Xd
B = self.dynamicsg(X)
Bd = self.dynamicsg(Xd)
f = self.dynamicsf(X) + B @ Ud
fd = self.dynamicsf(Xd) + Bd @ Ud
Q = np.identity(self.n_states) * 10
R = np.identity(self.m_inputs)
A = self.sdcA(X)
try:
K, P, _ = control.lqr(A, B, Q, R)
invR = np.linalg.inv(R)
phi0 = 2 * e @ P @ (f - fd) + e @ (P @ B @ invR @ B.T @ P + Q) @ e
phi1 = (2 * e @ P @ B).T
if phi0 > 0:
U = -(phi0 / (phi1.T @ phi1)) * phi1
U = Ud + U.ravel()
else:
U = Ud
except:
U = Ud
print("clfqp infeasible")
return U
def callback(self, data):
self.K, self.S, self.e = lqr(A, B, self.Q, self.R)
y = data.orientation.y * 180 / 3.1416
if y > self.yMax:
self.yMax = y
elif y < self.yMin:
self.yMin = y
vel = Twist()
diff_yaw = y - self.y_
np_x = np.array([[y], [diff_yaw]])
xvel = self.K.dot(np_x)[0, 0]
if xvel > self.xvelMax:
self.xvelMax = xvel
elif xvel < self.xvelMin:
self.xvelMin = xvel
vel.linear.x = xvel
vel.linear.y = 0
vel.linear.z = 0
vel.angular.x = 0
vel.angular.y = 0
vel.angular.z = 0
self.pub.publish(vel)
#print "Max vel " + str(self.xvelMax) + " & Min vel " + str(self.xvelMin) + " Max y " + str(self.yMax*180/3.1416) +" & Min y" + str(self.yMin*180/3.1416)
#print "Velocity "+ str(xvel)+ " & yaw " + str(y)
self.y_ = y
self.pub1.publish(data.orientation.y)
def compute_whipple_lqr_gain(velocity):
_, A, B = benchmark_state_space_vs_speed(*benchmark_matrices(), velocity)
Q = np.diag([1e5, 1e3, 1e3, 1e2])
R = np.eye(2)
gains = [control.lqr(Ai, Bi, Q, R)[0] for Ai, Bi in zip(A, B)]
return gains
def compute_whipple_lqr_gain(velocity):
_, A, B = benchmark_state_space_vs_speed(*benchmark_matrices(), velocity)
Q = np.diag([1e5, 1e3, 1e3, 1e2])
R = np.eye(2)
gains = [control.lqr(Ai, Bi, Q, R)[0] for Ai, Bi in zip(A, B)]
return gains
def update(self):
t = self.simulationHandler.currentTime
x, dx = self.controlInputStateSpaceHandler.getX_dx(t)
q, v, a = self.stateHandler.getPositionVelocityAcceleration()
A = self.linearizedModelHandler.getA()
B = self.linearizedModelHandler.getB()
F = self.constraintsHandler.getJacobian(DM(q))
dF = self.constraintsHandler.getJacobianDerivative(DM(q), DM(v))
G = horzcat(F, dF)
N = scipy.linalg.null_space(G)
An = N.T @ A @ N
Bn = N.T @ B.T
Qn = N.T @ self.Q @ N
Kn, S, CLP = lqr(An, Bn, Qn, self.R)
K = Kn @ N.T
e = (self.stateSpaceHandler.x - x)
u_FB = -K @ e
u_FF = self.inverseDynamicsHandler.u
self.u = u_FB + u_FF
def lqr_gain(rotor):
A = np.array([
[0, 1, 0, 0, 0, 0],
[0, 0, 0, 0, -rotor.g, 0],
[0, 0, 0, 1, 0, 0],
[0, 0, 0, 0, 0, 0],
[0, 0, 0, 0, 0, 1],
[0, 0, 0, 0, 0, 0],
],
dtype=float)
B = np.array([
[0, 0],
[0, 0],
[0, 0],
[1, 1],
[0, 0],
[-rotor.r / rotor.I, rotor.r / rotor.I],
],
dtype=float)
Q = np.eye(A.shape[1])
R = np.eye(B.shape[1])
K, _, _ = control.lqr(A, B, Q, R)
return K
def diffeomorphism_full_state_control(self):
d = 1
xi_bar = np.array([[0, 0, 1]]).T
zeta_bar = xi_bar + np.array([[0, 0, d]]).T
m = self.M
g = self.G
R = self.rot_mat
x = self.state
xi = x[0:3]
eta = x[3:6]
xi_dot = x[6:9]
eta_dot = x[9:12]
phi = eta[0]
theta = eta[1]
psi = eta[2]
phi_dot = eta_dot[0]
theta_dot = eta_dot[1]
psi_dot = eta_dot[2]
zeta = (self * rigid.Vector(*(0, 0, -d))).array
chi = np.vstack([zeta - zeta_bar, psi, xi_dot, psi_dot])
W = mechanics.att_vel_to_ang_vel_jacobian(phi, theta)
W_inv = np.linalg.inv(W)
W_dot = mechanics.time_derivative_att_vel_to_ang_vel_jacobian(
phi, theta, phi_dot, theta_dot)
A = np.hstack(
[np.zeros((8, 4)),
np.vstack([np.identity(4), np.zeros((4, 4))])])
b = np.array([[-1 / m * R[0, 2], d * R[0, 1], -d * R[0, 0]],
[-1 / m * R[1, 2], d * R[1, 1], -d * R[1, 0]],
[-1 / m * R[2, 2], d * R[2, 1], -d * R[2, 0]]])
B = np.vstack([
np.zeros((4, 4)),
np.hstack([b, np.zeros((3, 1))]),
np.array([[0, 0, 0, 1]])
])
G = np.array([[0, 0, 0, 0, 0, 0, -g, 0]]).T
QQ = np.diag([100, 100, 10, 1, 1, 1, 1, 1])
RR = np.diag(np.array([1, 1, 1, 1]))
K, _, _ = lqr(A, B, QQ, RR)
# mu_bar = np.array([[-g*m*R[2, 2], g/d*R[2, 1], -g/d*R[2, 0], 0]]).T
mu_bar = np.array([[g * m, 0, 0, 0]]).T
mu_delta = -np.dot(K, chi)
mu = mu_bar + mu_delta
F = mu[0, 0]
alpha = mu[1:4]
J = generialized_coordinate_inertia(self.I, phi, theta, psi)
C = quad_coriolis(self.I, phi, theta, phi_dot, theta_dot, psi_dot)
tau_eta = np.dot(J, np.dot(W_inv,
(alpha - np.dot(W_dot, eta_dot)))) + np.dot(
C, eta_dot)
return np.vstack([F, tau_eta])
def LQRControl(plant, Q, R):
plantStateSpace = control.tf2ss(plant)
A, B, C, D = control.ssdata(plantStateSpace)
print(A, B, C, D)
K, P, E = control.lqr(plantStateSpace, Q, R)
output = control.ss(A - B * K, B * K, C, D)
return control.step_response(output, T)
def lqr(self,x,A,B,Q,R):
K, S, E = control.lqr(A, B, Q, R)
u = -scipy.linalg.inv(R)*(B.T*(S*x))
#if B.size==2:
#print("S",S)
#print("x",x)
#print("B",self.B)
return u
def calculate_LQR_gains(A, B, C, D, Q, R):
# calculate LQR gains
(K, X, E) = ctl.lqr(A, B, Q, R)
# calculate Nu, Nx matrices for including reference input
Nu, Nx = getInputMatrices(A, B, C, D)
return K, Nu, Nx
def get_linear_quadratic_regulator(linear_model, q=numpy.identity(3),
r=numpy.identity(1)):
ctrb_matrix = control.ctrb(linear_model.A, linear_model.B)
if ctrb_matrix.shape[0] != linear_model.A.shape[0]:
raise ValueError("System is not controllable!")
k_matrix, s_matrix, e_matrix = control.lqr(linear_model.A, linear_model.B,
q, r)
return k_matrix, s_matrix, e_matrix
def diffeomorphism_full_state_control(self):
d = 1
xi_bar = np.array([[0, 0, 1]]).T
zeta_bar = xi_bar + np.array([[0, 0, d]]).T
m = self.M
g = self.G
R = self.rot_mat
x = self.state
xi = x[0:3]
eta = x[3:6]
xi_dot = x[6:9]
eta_dot = x[9:12]
phi = eta[0]
theta = eta[1]
psi = eta[2]
phi_dot = eta_dot[0]
theta_dot = eta_dot[1]
psi_dot = eta_dot[2]
zeta = (self * rigid.Vector(*(0, 0, -d))).array
chi = np.vstack([zeta-zeta_bar, psi, xi_dot, psi_dot])
W = mechanics.att_vel_to_ang_vel_jacobian(phi, theta)
W_inv = np.linalg.inv(W)
W_dot = mechanics.time_derivative_att_vel_to_ang_vel_jacobian(phi,
theta,
phi_dot,
theta_dot)
A = np.hstack([np.zeros((8, 4)),
np.vstack([np.identity(4), np.zeros((4, 4))])])
b = np.array([[-1/m*R[0, 2], d*R[0, 1], -d*R[0, 0]],
[-1/m*R[1, 2], d*R[1, 1], -d*R[1, 0]],
[-1/m*R[2, 2], d*R[2, 1], -d*R[2, 0]]])
B = np.vstack([np.zeros((4, 4)),
np.hstack([b, np.zeros((3, 1))]),
np.array([[0, 0, 0, 1]])])
G = np.array([[0, 0, 0, 0, 0, 0, -g, 0]]).T
QQ = np.diag([100, 100, 10, 1, 1, 1, 1, 1])
RR = np.diag(np.array([1, 1, 1, 1]))
K,_,_ = lqr(A, B, QQ, RR)
# mu_bar = np.array([[-g*m*R[2, 2], g/d*R[2, 1], -g/d*R[2, 0], 0]]).T
mu_bar = np.array([[g*m, 0, 0, 0]]).T
mu_delta = -np.dot(K, chi)
mu = mu_bar + mu_delta
F = mu[0, 0]
alpha = mu[1:4]
J = generialized_coordinate_inertia(self.I, phi, theta, psi)
C = quad_coriolis(self.I, phi, theta, phi_dot, theta_dot, psi_dot)
tau_eta = np.dot(J, np.dot(W_inv, (alpha - np.dot(W_dot, eta_dot)))) + np.dot(C, eta_dot)
return np.vstack([F, tau_eta])
def _test_lqr_random(rng, n):
# pylint: disable=import-outside-toplevel
import control
from jax.tree_util import tree_multimap
A, B, Q, R, N = random_env(rng, n)
actual = lqr_continuous_time_infinite_horizon(A, B, Q, R, N)
expected = control.lqr(A, B, Q, R, N)
assert tree_multimap(jp.allclose, actual, expected)
def one_step_sim(self,y):
runge_num = self.runge_num
A = self.Aekf(self.Z,self.t)
R = 1*np.eye(1)
Q = 100*np.eye(3)
K,P,E = control.lqr(A.T,C.T,Q,R)
L = K.T
for num in range(0, runge_num)
self.Z, self.t = self.rk4(L,y)
return self.Z, self.t
def test_discrete_lqr():
# oscillator model defined in 2D
# Source: https://www.mpt3.org/UI/RegulationProblem
A = [[0.5403, -0.8415], [0.8415, 0.5403]]
B = [[-0.4597], [0.8415]]
C = [[1, 0]]
D = [[0]]
# Linear discrete-time model with sample time 1
sys = ct.ss2io(ct.ss(A, B, C, D, 1))
# Include weights on states/inputs
Q = np.eye(2)
R = 1
K, S, E = ct.lqr(A, B, Q, R) # note: *continuous* time LQR
# Compute the integral and terminal cost
integral_cost = opt.quadratic_cost(sys, Q, R)
terminal_cost = opt.quadratic_cost(sys, S, None)
# Formulate finite horizon MPC problem
time = np.arange(0, 5, 1)
x0 = np.array([1, 1])
optctrl = opt.OptimalControlProblem(sys,
time,
integral_cost,
terminal_cost=terminal_cost)
res1 = optctrl.compute_trajectory(x0, return_states=True)
with pytest.xfail("discrete LQR not implemented"):
# Result should match LQR
K, S, E = ct.dlqr(A, B, Q, R)
lqr_sys = ct.ss2io(ct.ss(A - B @ K, B, C, D, 1))
_, _, lqr_x = ct.input_output_response(lqr_sys,
time,
0,
x0,
return_x=True)
np.testing.assert_almost_equal(res1.states, lqr_x)
# Add state and input constraints
trajectory_constraints = [
(sp.optimize.LinearConstraint, np.eye(3), [-10, -10, -1], [10, 10, 1]),
]
# Re-solve
res2 = opt.solve_ocp(sys,
time,
x0,
integral_cost,
constraints,
terminal_cost=terminal_cost)
# Make sure we got a different solution
assert np.any(np.abs(res1.inputs - res2.inputs) > 0.1)
def lqr_attitude_control(self):
Q_rot = np.diag([80, 80, 2, 1, 1, 1])
R_rot = np.diag(np.array([1000, 1000, 1000]))
K_rot,_,_ = lqr(self.A_rot, self.B_rot, Q_rot, R_rot)
X_rot = np.vstack([self.state[3:6], self.state[9:12]])
torque_attitude = -np.dot(K_rot, X_rot)
force = self.G*self.M
return np.vstack([force, torque_attitude])
def __init__(self, plant, state0, t0, Q=None, R=None):
A = plant.df(state0, t0)
B = plant.control_matrix(state0, t0)
Q = Q or np.identity(A.shape[1]) * 1.0
R = R or np.identity(B.shape[1]) * 0.00000001
K, S, E = control.lqr(A, B, Q, R)
self.state0 = state0.copy()
self.K = K
self.S = S
self.E = E
def __init__(self, plant, state0, t0, Q=None, R=None):
A = plant.df(state0, t0)
B = plant.control_matrix(state0, t0)
Q = Q or np.identity(A.shape[1]) * 1.0
R = R or np.identity(B.shape[1]) * 0.00000001
K, S, E = control.lqr(A, B, Q, R)
self.state0 = state0.copy()
self.K = K
self.S = S
self.E = E
def __init__(self, intopic, outtopic,
A, B, target=None, Q=None, R=None, realizable=True):
if Q is None:
Q = np.eye(A.shape[0])
if R is None:
R = np.eye(B.shape[1])
self.target_state = np.zeros(A.shape[0])
if target is not None:
self.target_state[:target.shape[0]] = target
K, S, E = lqr(A,B,Q,R)
StateFeedback.__init__(self, intopic, outtopic, K, realizable=realizable)
def LQR():
A = np.array([[0, 1], [g / lp, 0]])
B = np.array([[0], [1]])
Q = np.array([[3000., 0], [0, 1.]])
R = .1
K, S, E = lqr(A, B, Q, R)
return np.array(K)
def lqr_attitude_control(self):
Q_rot = np.diag([80, 80, 2, 1, 1, 1])
R_rot = np.diag(np.array([1000, 1000, 1000]))
K_rot, _, _ = lqr(self.A_rot, self.B_rot, Q_rot, R_rot)
X_rot = np.vstack([self.state[3:6], self.state[9:12]])
torque_attitude = -np.dot(K_rot, X_rot)
force = self.G * self.M
return np.vstack([force, torque_attitude])
def calc_lqr_gain(self):
# Choose state and input weights for cost function
self.Q = np.eye(4)
self.R = 0.0001
# Derive the optimal controller
K, S, E = control.lqr(self.A, self.B, self.Q, self.R)
# Set gain matrix
self.gain[:] = K
def solve_lqr(self, A, B, Q, R):
'''
Returns:
K: 2-d array : State feedback gains
S: 2-d array : Solution to Riccati equation
E: 1-d array : Eigenvalues of the closed loop system
'''
return control.lqr(A, B, Q, R)
def generateLQRTable(A_table, B_table, Q_table, R_table):
count = A_table.shape[0]
n = A_table.shape[2]
m = B_table.shape[2]
K_table = np.zeros((count, m, n))
for i in range(count):
K, S, CLP = lqr(A_table[i], B_table[i], Q_table[i], R_table[i])
K_table[i] = K
return K_table
def construct(self):
d_stat = 9
d_ctrl = self.n_contacts*6
self.A = np.zeros((d_stat,d_stat))
self.A[:3,3:6] = 1./self.mass*np.eye(3)
self.A[6:,:3] = self.cross_mat(self.mass*np.array([0., 0., -9.81]))
self.B = np.zeros((d_stat,d_ctrl))
for c in range(self.n_contacts):
self.B[3:,6*c:6*c+6] = np.eye(6)
self.B[6:,6*c:6*c+3] = self.cross_mat(self.cog_to_cont[c])
self.K,self.p,self.e = lqr(self.A,self.B,self.Q,self.R)
# dh = Gain*err + h_des
self.Gain = np.array(np.matrix(self.B[3:,:])*np.matrix(self.K))
def control_eq(self):
self.equilibrium_point = hstack(( 0, pi / 2 * ones(len(self.q) - 1), zeros(len(self.u)) ))
equilibrium_dict = dict(zip(self.q + self.u, self.equilibrium_point))
parameter_dict = dict(zip(self.parameters, self.parameter_vals))
# symbolically linearize about arbitrary equilibrium
self.linear_state_matrix, self.linear_input_matrix, inputs = self.kane.linearize()
# sub in the equilibrium point and the parameters
self.f_A_lin = self.linear_state_matrix.subs(parameter_dict).subs(equilibrium_dict)
self.f_B_lin = self.linear_input_matrix.subs(parameter_dict).subs(equilibrium_dict)
m_mat = self.kane.mass_matrix_full.subs(parameter_dict).subs(equilibrium_dict)
# compute A and B
from numpy import matrix
A = matrix(m_mat.inv() * self.f_A_lin)
B = matrix(m_mat.inv() * self.f_B_lin)
assert matrix_rank(control.ctrb(A, B)) == A.shape[0]
self.K, self.X, self.E = control.lqr(A, B, ones(A.shape), 1);
def calcK(self, Plant): #Calculates the K matrix using python control systems and lqr pole placement #Define A matrix A = [ [0, 1], [-Plant.g / Plant.l, -Plant.b / (Plant.m * (Plant.l ** 2))] ] #Define B matrix B = [ [0], [1 / (Plant.m * (Plant.l ** 2))] ] #define C matrix. It's just the identity C = np.identity(2) #The D matrix is just 0 D = [ [0], [0] ] #Create the statespace representation sys = control.ss(A, B, C, D) #Create the state weight matrix, weight position 20000, and speed 100 Q = [ [20000, 0], [0, 100] ] #Create input weight matrix R = [ [1] ] #Compute LQR LQR_vals = control.lqr(sys, Q, R) return LQR_vals[0] #return K values of LQR return
def lqr_position_attitude_control(self):
m = self.M
g = self.G
q = self.state
xi = q[0:3]
xi_dot = q[6:9]
phi = q[3,0]
theta = q[4,0]
psi = mmath.wrap_to_2pi(q[5,0])
eta = np.array([[phi, theta, psi]]).T
chi = np.vstack([xi, xi_dot])
xi_bar = self.state_desired[0:3]
psi_bar = mmath.wrap_to_2pi(self.state_desired[5,0])
xi_dot_bar = self.state_desired[6:9]
chi_bar = np.vstack([xi_bar, xi_dot_bar])
chi_delta = (chi - chi_bar)
A_pos = np.vstack([np.hstack([np.zeros((3,3)), np.identity(3)]),
np.zeros((3, 6))])
B_pos = np.vstack([np.zeros((3, 3)), np.identity(3)])
Q_pos = np.diag([2, 2, 2, 20, 20, 20])
R_pos = np.diag(np.array([5, 5, 5]))
K_pos,_,_ = lqr(A_pos, B_pos, Q_pos, R_pos)
acc_vec = -np.dot(K_pos, chi_delta) + np.array([[0, 0, g]]).T
Z = -acc_vec / np.linalg.norm(acc_vec)
a = Z[0, 0]*sin(psi_bar) + Z[1, 0]*cos(psi_bar)
b = -Z[2, 0]
c = -a
if np.allclose(a, 0):
X3 = 0
elif abs((-b+sqrt(b**2 - 4*a*c))/(2*a)) <= 1:
X3 = (-b+sqrt(b**2 - 4*a*c))/(2*a)
else:
X3 = (-b-sqrt(b**2 - 4*a*c))/(2*a)
d = sqrt(1 - X3**2)
if psi_bar >= 0 and psi_bar < PI:
X1 = sqrt(d**2 * (sin(psi_bar))**2)
else:
X1 = -sqrt(d**2 * (sin(psi_bar))**2)
if (psi_bar >= 0 and psi_bar < PI/2) or psi_bar >= 3*PI/2:
X2 = sqrt(d**2 * (cos(psi_bar))**2)
else:
X2 = -sqrt(d**2 * (cos(psi_bar))**2)
X = np.array([[X1, X2, X3]]).T
X = X / np.linalg.norm(X)
Y = np.atleast_2d(np.cross(np.squeeze(Z), np.squeeze(X))).T
Y = Y / np.linalg.norm(Y)
R = np.hstack([X, Y, Z])
(phi_bar, theta_bar, _) = mmath.rot2euler(np.dot(self.nominal_frame.rot_mat, R))
eta_bar = np.array([[phi_bar, theta_bar, psi_bar]]).T
eta_delta = eta - eta_bar
eta_delta = np.array([[mmath.wrap_to_pi(ang) for ang in eta_delta]]).T
Q_rot = np.diag([1, 1, 1, 1, 1, 1])
R_rot = np.diag(np.array([5, 5, 5]))
K_rot,_,_ = lqr(self.A_rot, self.B_rot, Q_rot, R_rot)
X_rot = np.vstack([eta_delta, self.state[9:12]])
torque_attitude = -np.dot(K_rot, X_rot)
force = np.linalg.norm(acc_vec)*m
u = np.vstack([force, torque_attitude])
return u
[0, -(I+m*l**2)*b/p, (m**2*g*l**2)/p, 0],
[0, 0, 0, 1],
[0, -(m*l*b)/p, m*g*l*(M+m)/p, 0]])
B = array([[0],
[(I+m*l**2)/p],
[0],
[m*l/p]])
C = array([[1, 0, 0, 0],
[0, 0, 1, 0]])
D = array([[0],
[0]])
poles,vect = eig(A)
# Print vectors to verify that the system is unstable
print poles
K = control.place(A,B, [-1,-1,-1,-1])
print 'K(place)=',K
Q = C.transpose().dot(C)
Q[1,1]=5000
Q[3,3] = 100
R = 1
K,S,E = control.lqr(A,B,Q,R)
print 'K(lqr)=',K
# New control matrix
Ac = A-B.dot(K)
poles,vect = eig(Ac)
print "Ac poles=", poles