├── .gitignore
├── LICENSE
├── MANIFEST.in
├── README.md
├── controlpy
├── __init__.py
├── analysis.py
└── synthesis.py
├── examples
├── example_controllability.py
├── example_lqr.py
└── example_systemGain.py
├── setup.cfg
├── setup.py
└── tests
├── test_analysis.py
└── test_synth.py
/.gitignore:
--------------------------------------------------------------------------------
1 | # Compiled python modules.
2 | *.pyc
3 |
4 | # Setuptools distribution folder.
5 | /dist/
6 |
7 | # Python egg metadata, regenerated from source files by setuptools.
8 | /*.egg-info
9 | /.eggs
10 |
11 | # vim temp files:
12 | *.py~
13 |
14 | #Eclipse/PyDev
15 | .project
16 | .pydevproject
17 |
18 | #Vim Temp files
19 | *~
20 |
--------------------------------------------------------------------------------
/LICENSE:
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--------------------------------------------------------------------------------
/MANIFEST.in:
--------------------------------------------------------------------------------
1 | include README.md
2 |
--------------------------------------------------------------------------------
/README.md:
--------------------------------------------------------------------------------
1 | Controlpy
2 | =========
3 |
4 | A library for commonly used controls algorithms (e.g. creating LQR controllers). An alternative to Richard Murray's "control" package -- however, here we do not require Slycot.
5 |
6 | Current capabilities:
7 |
8 | 1. System analysis:
9 | 1. Test whether a system is stable, controllable, stabilisable, observable, or stabilisable.
10 | 2. Get the uncontrollable/unobservable modes
11 | 3. Compute a system's controllability Gramian (finite horizon, and infinite horizon)
12 | 4. Compute a system's H2 and Hinfinity norm
13 | 2. Synthesis
14 | 1. Create continuous and discrete time LQR controllers
15 | 2. Full-information H2 optimal controller
16 | 3. H2 optimal observer
17 | 4. Full-information Hinf controller
18 |
19 |
20 | How to install
21 | --------------
22 | Install using pypi, or direct from the Github repository:
23 |
24 | 1. Clone this repository somewhere convenient: `git clone https://github.com/markwmuller/controlpy.git`
25 | 2. Install the package (we'll do a "develop" install, so any changes are immediately available): `pip install -e .` (you'll probably need to be administrator)
26 | 3. You're ready to go: try running the examples in the `example` folder.
27 |
28 |
29 | Testing
30 | -------
31 | If you want to run the unit tests, you'll need to install cvxpy.
32 |
33 |
34 | Licensing
35 | ---------
36 | `(c) Mark W. Mueller 2016`
37 |
38 | This program is free software: you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation, either version 3 of the License, or (at your option) any later version.
39 | This program is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details.
40 |
41 | You should have received a copy of the GNU General Public License along with this program. If not, see .
42 |
43 |
44 |
45 |
46 |
--------------------------------------------------------------------------------
/controlpy/__init__.py:
--------------------------------------------------------------------------------
1 | #(c) 2014 Mark W. Mueller
2 | __all__ = []
3 |
4 | from . import analysis
5 | from . import synthesis
6 |
7 | __all__.extend(['analysis', 'synthesis'])
8 |
--------------------------------------------------------------------------------
/controlpy/analysis.py:
--------------------------------------------------------------------------------
1 | """ Tools for analysing LTI systems.
2 |
3 | (c) 2014 Mark W. Mueller
4 | """
5 |
6 | import numpy as np
7 | import scipy.linalg
8 | import scipy.integrate
9 |
10 |
11 | def is_hurwitz(A, tolerance = 1e-9):
12 | '''Test whether the matrix A is Hurwitz (i.e. asymptotically stable).
13 |
14 | tolerance defines the minimum distance we should be from the imaginary axis
15 | to be considered stable.
16 |
17 | '''
18 | return max(np.real(np.linalg.eig(A)[0])) < -np.abs(tolerance)
19 |
20 |
21 | def uncontrollable_modes(A, B, returnEigenValues = False, tolerance=1e-9):
22 | '''Returns all the uncontrollable modes of the pair A,B.
23 |
24 | tolerance defines the minimum distance we should be from the imaginary axis
25 | to be considered stable.
26 |
27 | Does the PBH test for controllability for the system:
28 | dx = A*x + B*u
29 |
30 | Returns a list of the uncontrollable modes, and (optionally)
31 | the corresponding eigenvalues.
32 |
33 | See Callier & Desoer "Linear System Theory", P. 253
34 |
35 | NOTE!: This can't work if we have repeated eigen-values! TODO FIXME!
36 | '''
37 |
38 | assert A.shape[0]==A.shape[1], "Matrix A is not square"
39 | assert A.shape[0]==B.shape[0], "Matrices A and B do not align"
40 |
41 | nStates = A.shape[0]
42 | nInputs = B.shape[1]
43 |
44 | eVal, eVec = np.linalg.eig(np.matrix(A)) # todo, matrix cast is ugly.
45 |
46 | uncontrollableModes = []
47 | uncontrollableEigenValues = []
48 |
49 | for e,v in zip(eVal, eVec.T):
50 | M = np.matrix(np.zeros([nStates,(nStates+nInputs)]), dtype=complex)
51 | M[:,:nStates] = e*np.identity(nStates) - A
52 | M[:,nStates:] = B
53 |
54 | s = np.linalg.svd(M, compute_uv=False)
55 | if min(s) <= tolerance:
56 | uncontrollableModes.append(v.T[:,0])
57 | uncontrollableEigenValues.append(e)
58 |
59 | if returnEigenValues:
60 | return uncontrollableModes, uncontrollableEigenValues
61 | else:
62 | return uncontrollableModes
63 |
64 |
65 |
66 | def is_controllable(A, B, tolerance=1e-9):
67 | '''Compute whether the pair (A,B) is controllable.
68 | tolerance defines the minimum distance we should be from the imaginary axis
69 | to be considered stable.
70 |
71 | Returns True if controllable, False otherwise.
72 | '''
73 |
74 | if uncontrollable_modes(A, B, tolerance=tolerance):
75 | return False
76 | else:
77 | return True
78 |
79 |
80 |
81 | def is_stabilizable(A, B):
82 | '''Compute whether the pair (A,B) is stabilisable.
83 |
84 | Returns True if stabilisable, False otherwise.
85 | '''
86 |
87 | return is_stabilisable(A, B)
88 |
89 |
90 | def is_stabilisable(A, B):
91 | '''Compute whether the pair (A,B) is stabilisable.
92 |
93 | Returns True if stabilisable, False otherwise.
94 | '''
95 |
96 | modes, eigVals = uncontrollable_modes(A, B, returnEigenValues=True)
97 | if not modes:
98 | return True #controllable => stabilisable
99 |
100 | if max(np.real(eigVals)) >= 0:
101 | return False
102 | else:
103 | return True
104 |
105 |
106 | def controllability_gramian(A, B, T = np.inf):
107 | '''Compute the causal controllability Gramian of the continuous time system.
108 |
109 | The system is described as
110 | dx = A*x + B*u
111 |
112 | T is the horizon over which to compute the Gramian. If not specified, the
113 | infinite horizon Gramian is computed. Note that the infinite horizon Gramian
114 | only exists for asymptotically stable systems.
115 |
116 | If T is specified, we compute the Gramian as
117 | Wc = integrate exp(A*t)*B*B.H*exp(A.H*t) dt
118 |
119 | Returns the matrix Wc.
120 | '''
121 |
122 | assert A.shape[0]==A.shape[1], "Matrix A is not square"
123 | assert A.shape[0]==B.shape[0], "Matrix A and B do not align"
124 |
125 | if not np.isfinite(T):
126 | #Infinite time Gramian:
127 | assert is_hurwitz(A), "Can only compute infinite horizon Gramian for a stable system."
128 |
129 | Wc = scipy.linalg.solve_lyapunov(A, -B.dot(B.T))
130 | return Wc
131 |
132 | # We need to solve the finite time Gramian
133 | # Boils down to solving an ODE:
134 | A = np.array(A,dtype=float)
135 | B = np.array(B,dtype=float)
136 | T = np.float(T)
137 |
138 | def gramian_ode(y, t0, A, B):
139 | temp = np.dot(scipy.linalg.expm(A*t0),B)
140 | dQ = np.dot(temp,np.conj(temp.T))
141 |
142 | return dQ.reshape((A.shape[0]**2,1))[:,0]
143 |
144 | y0 = np.zeros([A.shape[0]**2,1])[:,0]
145 | out = scipy.integrate.odeint(gramian_ode, y0, [0,T], args=(A,B))
146 | Q = out[1,:].reshape([A.shape[0], A.shape[0]])
147 | return Q
148 |
149 |
150 | def unobservable_modes(C, A, returnEigenValues = False):
151 | '''Returns all the unobservable modes of the pair A,C.
152 |
153 | Does the PBH test for observability for the system:
154 | dx = A*x
155 | y = C*x
156 |
157 | Returns a list of the unobservable modes, and (optionally)
158 | the corresponding eigenvalues.
159 |
160 | See Callier & Desoer "Linear System Theory", P. 253
161 | '''
162 |
163 | return uncontrollable_modes(A.conj().T, C.conj().T, returnEigenValues)
164 |
165 |
166 | def is_observable(C, A):
167 | '''Compute whether the pair (C,A) is observable.
168 |
169 | Returns True if observable, False otherwise.
170 | '''
171 |
172 | return is_controllable(A.conj().T, C.conj().T)
173 |
174 |
175 | def is_detectable(C, A):
176 | '''Compute whether the pair (C,A) is detectable.
177 |
178 | Returns True if detectable, False otherwise.
179 | '''
180 |
181 | return is_stabilisable(A.conj().T, C.conj().T)
182 |
183 |
184 | #TODO
185 | # def observability_gramian(A, B, T = np.inf):
186 | # '''Compute the observability Gramian of the continuous time system.
187 | #
188 | # The system is described as
189 | # dx = A*x + B*u
190 | #
191 | # T is the horizon over which to compute the Gramian. If not specified, the
192 | # infinite horizon Gramian is computed. Note that the infinite horizon Gramian
193 | # only exists for asymptotically stable systems.
194 | #
195 | # If T is specified, we compute the Gramian as
196 | # Wc = integrate exp(A*t)*B*B.H*exp(A.H*t) dt
197 | #
198 | # Returns the matrix Wc.
199 | # '''
200 | #
201 | # assert A.shape[0]==A.shape[1], "Matrix A is not square"
202 | # assert A.shape[0]==B.shape[0], "Matrix A and B do not align"
203 | #
204 | # if not np.isfinite(T):
205 | # #Infinite time Gramian:
206 | # eigVals, eigVecs = scipy.linalg.eig(A)
207 | # assert np.max(np.real(eigVals)) < 0, "Can only compute infinite horizon Gramian for a stable system."
208 | #
209 | # Wc = scipy.linalg.solve_lyapunov(A, -B*B.T)
210 | # return Wc
211 | #
212 | # # We need to solve the finite time Gramian
213 | # # Boils down to solving an ODE:
214 | # A = np.array(A,dtype=float)
215 | # B = np.array(B,dtype=float)
216 | # T = np.float(T)
217 | #
218 | # def gramian_ode(y, t0, A, B):
219 | # temp = np.dot(scipy.linalg.expm(A*t0),B)
220 | # dQ = np.dot(temp,np.conj(temp.T))
221 | #
222 | # return dQ.reshape((A.shape[0]**2,1))[:,0]
223 | #
224 | # y0 = np.zeros([A.shape[0]**2,1])[:,0]
225 | # out = scipy.integrate.odeint(gramian_ode, y0, [0,T], args=(A,B))
226 | # Q = out[1,:].reshape([A.shape[0], A.shape[0]])
227 | # return Q
228 |
229 |
230 | def system_norm_H2(Acl, Bdisturbance, C):
231 | '''Compute a system's H2 norm.
232 |
233 | Acl, Bdisturbance are system matrices, describing the systems dynamics:
234 | dx/dt = Acl*x + Bdisturbance*v
235 | where x is the system state and v is the disturbance.
236 |
237 | The system output is:
238 | z = C*x
239 |
240 | The matrix Acl must be Hurwitz for the H2 norm to be finite.
241 |
242 | Parameters
243 | ----------
244 | A : (n, n) Matrix,
245 | Input
246 | Bdisturbance : (n, m) Matrix
247 | Input
248 | C : (n, q) Matrix
249 | Input
250 |
251 | Returns
252 | -------
253 | J2 : Systems H2 norm.
254 | '''
255 |
256 | if not is_hurwitz(Acl):
257 | return np.inf
258 |
259 | #first, compute the controllability Gramian of (Acl, Bdisturbance)
260 | P = controllability_gramian(Acl, Bdisturbance)
261 |
262 | #output the gain
263 | return np.sqrt(np.trace(C.dot(P).dot(C.T)))
264 |
265 |
266 | def system_norm_Hinf(Acl, Bdisturbance, C, D = None, lowerBound = 0.0, upperBound = np.inf, relTolerance = 1e-3):
267 | '''Compute a system's Hinfinity norm.
268 |
269 | Acl, Bdisturbance are system matrices, describing the systems dynamics:
270 | dx/dt = Acl*x + Bdisturbance*v
271 | where x is the system state and v is the disturbance.
272 |
273 | The system output is:
274 | z = C*x + D*v
275 |
276 | The matrix Acl must be Hurwitz for the Hinf norm to be finite.
277 |
278 | The norm is found by iterating over the Riccati equation. The search can
279 | be sped up by providing lower and upper bounds for the norm. If ommitted,
280 | these are determined automatically.
281 | The search proceeds via bisection, and terminates when a specified relative
282 | tolerance is achieved.
283 |
284 | Parameters
285 | ----------
286 | A : (n, n) Matrix
287 | Input
288 | Bdisturbance : (n, m) Matrix
289 | Input
290 | C : (q, n) Matrix
291 | Input
292 | D : (q,m) Matrix
293 | Input (optional)
294 | lowerBound: float
295 | Input (optional)
296 | upperBound: float
297 | Input (optional)
298 | relTolerance: float
299 | Input (optional)
300 |
301 | Returns
302 | -------
303 | Jinf : Systems Hinf norm.
304 |
305 | '''
306 |
307 | if not is_hurwitz(Acl):
308 | return np.inf
309 |
310 | eps = 1e-10
311 |
312 | if D is None:
313 | #construct a fake feed-through matrix
314 | D = np.matrix(np.zeros([C.shape[0], Bdisturbance.shape[1]]))
315 |
316 |
317 | def test_upper_bound(gamma, A, B, C, D):
318 | '''Is the given gamma an upper bound for the Hinf gain?
319 | '''
320 | #Construct the R matrix:
321 | Rric = -gamma**2*np.matrix(np.eye(D.shape[1],D.shape[1])) + D.T.dot(D)
322 | #test that Rric is negative definite
323 | eigsR = np.linalg.eig(Rric)[0]
324 | if max(np.real(eigsR)) > -eps:
325 | return False, None
326 |
327 | #matrices for the Ricatti equation:
328 | Aric = A - B.dot(np.linalg.inv(Rric)).dot(D.T).dot(C)
329 | Bric = B
330 | Qric = C.T.dot(C) - C.T.dot(D).dot(np.linalg.inv(Rric)).dot(D.T).dot(C)
331 |
332 | try:
333 | X = scipy.linalg.solve_continuous_are(Aric, Bric, Qric, Rric)
334 | except np.linalg.linalg.LinAlgError:
335 | #Couldn't solve
336 | return False, None
337 |
338 | eigsX = np.linalg.eigvals(X)
339 | if (np.min(np.real(eigsX)) < 0) or (np.sum(np.abs(np.imag(eigsX)))>eps):
340 | #The ARE has to return a pos. semidefinite solution, but X is not
341 | return False, None
342 | if np.max(np.linalg.svd(X-X.T, compute_uv=False)) > 1e-6:
343 | #The ARE solution is not symmetric! Fail
344 | return False, None
345 |
346 |
347 | CL = A + B.dot(np.linalg.inv(-Rric)).dot(B.T.dot(X) + D.T.dot(C))
348 | eigs = np.linalg.eigvals(CL)
349 |
350 | return (np.max(np.real(eigs)) < -eps), X
351 |
352 | #our output ricatti solution
353 | X = None
354 |
355 | #Are we supplied an upper bound?
356 | if not np.isfinite(upperBound):
357 | upperBound = max([1.0,lowerBound])
358 | counter = 1
359 | while True:
360 | isOK, X2 = test_upper_bound(upperBound, Acl, Bdisturbance, C, D)
361 |
362 | if isOK:
363 | X = X2.copy()
364 | break
365 |
366 | upperBound *= 2.0
367 | counter += 1
368 | assert counter<1024, 'Exceeded max. number of iterations searching for upper bound'
369 |
370 | #perform a bisection search to find the gain:
371 | while (upperBound-lowerBound)>relTolerance*upperBound:
372 | g = 0.5*(upperBound+lowerBound)
373 |
374 | stab, X2 = test_upper_bound(g, Acl, Bdisturbance, C, D)
375 | if stab:
376 | upperBound = g
377 | X = X2
378 | else:
379 | lowerBound = g
380 |
381 | assert X is not None, 'No solution found! Check supplied upper bound'
382 |
383 | return upperBound
384 |
385 |
386 |
387 | def discretise_time(A, B, dt):
388 | '''Compute the exact discretization of the continuous system A,B.
389 |
390 | Goes from a description
391 | d/dt x(t) = A*x(t) + B*u(t)
392 | u(t) = ud[k] for t in [k*dt, (k+1)*dt)
393 | to the description
394 | xd[k+1] = Ad*xd[k] + Bd*ud[k]
395 | where
396 | xd[k] := x(k*dt)
397 |
398 | Returns: Ad, Bd
399 | '''
400 |
401 | nstates = A.shape[0]
402 | ninputs = B.shape[1]
403 |
404 | M = np.matrix(np.zeros([nstates+ninputs,nstates+ninputs]))
405 | M[:nstates,:nstates] = A
406 | M[:nstates, nstates:] = B
407 |
408 | Md = scipy.linalg.expm(M*dt)
409 | Ad = Md[:nstates, :nstates]
410 | Bd = Md[:nstates, nstates:]
411 |
412 | return Ad, Bd
413 |
414 |
415 |
416 |
417 |
418 |
--------------------------------------------------------------------------------
/controlpy/synthesis.py:
--------------------------------------------------------------------------------
1 | """ Tools for synthesising controllers for LTI systems.
2 |
3 | (c) 2014 Mark W. Mueller
4 | """
5 | from __future__ import division, print_function
6 |
7 | import numpy as np
8 | import scipy.linalg
9 |
10 | from controlpy import analysis
11 |
12 |
13 | def controller_lqr(A, B, Q, R):
14 | """Solve the continuous time LQR controller for a continuous time system.
15 |
16 | A and B are system matrices, describing the systems dynamics:
17 | dx/dt = A x + B u
18 |
19 | The controller minimizes the infinite horizon quadratic cost function:
20 | cost = integral (x.T*Q*x + u.T*R*u) dt
21 |
22 | where Q is a positive semidefinite matrix, and R is positive definite matrix.
23 |
24 | Returns K, X, eigVals:
25 | Returns gain the optimal gain K, the solution matrix X, and the closed loop system eigenvalues.
26 | The optimal input is then computed as:
27 | input: u = -K*x
28 | """
29 | #ref Bertsekas, p.151
30 |
31 | #first, try to solve the ricatti equation
32 | X = scipy.linalg.solve_continuous_are(A, B, Q, R)
33 |
34 | #compute the LQR gain
35 | K = np.dot(np.linalg.inv(R),(np.dot(B.T,X)))
36 |
37 | eigVals = np.linalg.eigvals(A-np.dot(B,K))
38 |
39 | return K, X, eigVals
40 |
41 |
42 |
43 | def controller_lqr_discrete_time(A, B, Q, R):
44 | """Solve the discrete time LQR controller for a discrete time system.
45 |
46 | A and B are system matrices, describing the systems dynamics:
47 | x[k+1] = A x[k] + B u[k]
48 |
49 | The controller minimizes the infinite horizon quadratic cost function:
50 | cost = sum x[k].T*Q*x[k] + u[k].T*R*u[k]
51 |
52 | where Q is a positive semidefinite matrix, and R is positive definite matrix.
53 |
54 | Returns K, X, eigVals:
55 | Returns gain the optimal gain K, the solution matrix X, and the closed loop system eigenvalues.
56 | The optimal input is then computed as:
57 | input: u = -K*x
58 | """
59 |
60 | #first, try to solve the ricatti equation
61 | X = scipy.linalg.solve_discrete_are(A, B, Q, R)
62 |
63 | #compute the LQR gain
64 | K = np.dot(np.linalg.inv(np.dot(np.dot(B.T,X),B)+R),(np.dot(np.dot(B.T,X),A)))
65 |
66 | eigVals = np.linalg.eigvals(A-np.dot(B,K))
67 |
68 | return K, X, eigVals
69 |
70 |
71 | def estimator_kalman_steady_state_discrete_time(A, H, Q, R):
72 | """Solve the discrete time, steady-state Kalman filter for a discrete time system.
73 |
74 | A and H are system matrices, describing the systems dynamics:
75 | x[k+1] = A x[k] + B u[k] + v[k]
76 | z[k] = C x[k] + w[k]
77 |
78 | with v, w zero-mean noise sequences, and
79 | Var[v[k]] = Q
80 | Var[w[k]] = R
81 |
82 | and u[k] a known input
83 |
84 | Returns K, X, eigVals:
85 | Returns gain the optimal filter gain K, the solution matrix X, and the closed loop system eigenvalues.
86 | The estimate is then given by:
87 | est[k] = (I-K*H)A est[k-1] + (I-K*H)B u[k] + K meas[k]
88 | """
89 |
90 | #first, try to solve the ricatti equation
91 | X = scipy.linalg.solve_discrete_are(A.T, H.T, Q, R)
92 |
93 | #compute the LQR gain
94 | K = X.dot(H.T).dot(np.linalg.inv(H.dot(X).dot(H.T)+R))
95 |
96 | eigVals = np.linalg.eigvals( (np.identity(X.shape[0]) - K.dot(H)).dot(A) )
97 |
98 | return K, X, eigVals
99 |
100 |
101 | def controller_lqr_discrete_from_continuous_time(A, B, Q, R, dt):
102 | """Solve the discrete time LQR controller for a continuous time system.
103 |
104 | A and B are system matrices, describing the systems dynamics:
105 | dx/dt = A x + B u
106 |
107 | The controller minimizes the infinite horizon quadratic cost function:
108 | cost = integral (x.T*Q*x + u.T*R*u) dt
109 | where Q is a positive semidefinite matrix, and R is positive definite matrix.
110 |
111 | The controller is implemented to run at discrete times, at a rate given by
112 | onboard_dt,
113 | i.e. u[k] = -K*x(k*t)
114 | Discretization is done by zero order hold.
115 |
116 | Returns K, X, eigVals:
117 | Returns gain the optimal gain K, the solution matrix X, and the closed loop system eigenvalues.
118 | The optimal input is then computed as:
119 | input: u = -K*x
120 | """
121 | #ref Bertsekas, p.151
122 |
123 | Ad, Bd = analysis.discretise_time(A, B, dt)
124 |
125 | return controller_lqr_discrete_time(Ad, Bd, Q, R)
126 |
127 |
128 |
129 | def controller_H2_state_feedback(A, Binput, Bdist, C1, D12):
130 | """Solve for the optimal H2 static state feedback controller.
131 |
132 | A, Bdist, and Binput are system matrices, describing the systems dynamics:
133 | dx/dt = A*x + Binput*u + Bdist*v
134 | where x is the system state, u is the input, and v is the disturbance
135 |
136 | The goal is to minimize the output Z, defined as
137 | z = C1*x + D12*u
138 |
139 | The optimal output is given by a static feedback gain:
140 | u = - K*x
141 |
142 | This is related to the LQR problem, where the state cost matrix is Q and
143 | the input cost matrix is R, then:
144 | C1 = [[sqrt(Q)], [0]] and D = [[0], [sqrt(D12)]]
145 | With sqrt(Q).T*sqrt(Q) = Q
146 |
147 | Parameters
148 | ----------
149 | A : (n, n) Matrix
150 | Input
151 | Bdist : (n, m) Matrix
152 | Input
153 | Binput : (n, p) Matrix
154 | Input
155 | C1 : (q, n) Matrix
156 | Input
157 | D12: (q, p) Matrix
158 | Input
159 |
160 | Returns
161 | -------
162 | K : (m, n) Matrix
163 | H2 optimal controller gain
164 | X : (n, n) Matrix
165 | Solution to the Ricatti equation
166 | J : Minimum H2 cost value
167 |
168 | """
169 |
170 | X = scipy.linalg.solve_continuous_are(A, Binput, C1.T.dot(C1), D12.T.dot(D12))
171 |
172 | K = np.linalg.inv(D12.T.dot(D12)).dot(Binput.T).dot(X)
173 |
174 | J = np.sqrt(np.trace(Bdist.T.dot(X.dot(Bdist))))
175 |
176 | return K, X, J
177 |
178 |
179 | def observer_H2(A, Bdist, C1, C2, D21):
180 | """Solve for the optimal H2 state observer.
181 |
182 | TODO: document this!
183 |
184 | """
185 |
186 | return controller_H2_state_feedback(A.T, C2.T, C1.T, Bdist.T, D21.T)
187 |
188 |
189 | # def controller_H2_output_feedback(A, Binput, Bdist, C1, D12, C2, D21):
190 | # """Solve for the optimal H2 output feedback controller.
191 | #
192 | # TODO: document this!
193 | #
194 | # u = K*xhat
195 | # d/dt xhat = A*xhat - Binput*u + L*(y - C2*xhat)
196 | #
197 | # """
198 | #
199 | # K, X, Jc = controller_H2_state_feedback(A, Binput, Bdist, C1, D12)
200 | # L, S, Jo = observer_H2(A, Bdist, C1, C2, D21)
201 | #
202 | # J = np.sqrt(Jc**2 + Jo**2)
203 | #
204 | # return K, L, X, S, (Jc, Jo, J)
205 |
206 |
207 | def controller_Hinf_state_feedback(A, Binput, Bdist, C1, D12, stabilityBoundaryEps=1e-16, gammaRelTol=1e-3, gammaLB = 0, gammaUB = np.Inf, subOptimality = 1.0):
208 | """Solve for the optimal H_infinity static state feedback controller.
209 |
210 | A, Bdist, and Binput are system matrices, describing the systems dynamics:
211 | dx/dt = A*x + Binput*u + Bdist*v
212 | where x is the system state, u is the input, and v is the disturbance
213 |
214 | The goal is to minimize the output Z, in the H_inf sense, defined as
215 | z = C1*x + D12*u
216 |
217 | The optimal output is given by a static feedback gain:
218 | u = - K*x
219 |
220 | The optimizing gain is found by a bisection search to within a relative
221 | tolerance gammaRelTol, which may be supplied by the user. The search may
222 | be initialised with lower and upper bounds gammaLB and gammaUB.
223 |
224 | The user may also specify a desired suboptimality, so that the returned
225 | controller does not achieve the minimum Hinf norm. This may be desirable
226 | because of numerical issues near the optimal solution.
227 |
228 | Parameters
229 | ----------
230 | A : (n, n) Matrix
231 | Input
232 | Bdist : (n, m) Matrix
233 | Input
234 | Binput : (n, p) Matrix
235 | Input
236 | C1 : (q, n) Matrix
237 | Input
238 | D12: (q, p) Matrix
239 | Input
240 | stabilityBoundaryEps: float
241 | Input (optional)
242 | gammaRelTol: float
243 | Input (optional)
244 | gammaLB: float
245 | Input (optional)
246 | gammaUB: float
247 | Input (optional)
248 |
249 | Returns
250 | -------
251 | K : (m, n) Matrix
252 | Hinf optimal controller gain
253 | X : (n, n) Matrix
254 | Solution to the Ricatti equation
255 | J : Minimum cost value (gamma)
256 | """
257 |
258 | assert analysis.is_stabilisable(A, Binput), '(A, Binput) must be stabilisable'
259 | assert np.linalg.det(D12.T.dot(D12)), 'D12.T*D12 must be invertible'
260 | assert np.max(np.abs(D12.T.dot(C1)))==0, 'D12.T*C1 must be zero'
261 | tmp = analysis.unobservable_modes(C1, A, returnEigenValues=True)[1]
262 | if tmp:
263 | assert np.max(np.abs(np.real(tmp)))>0, 'The pair (C1,A) must have no unobservable modes on imag. axis'
264 |
265 | #First, solve the ARE:
266 | # A.T*X+X*A - X*Binput*inv(D12.T*D12)*Binput.T*X + gamma**(-2)*X*Bdist*Bdist.T*X + C1.T*C1 = 0
267 | #Let:
268 | # R = [[-gamma**(-2)*eye, 0],[0, D12.T*D12]]
269 | # B = [Bdist, Binput]
270 | # Q = C1.T*C1
271 | #then we have to solve
272 | # A.T*X+X*A - X*B*inv(R)*B.T*X + Q = 0
273 |
274 | B = np.matrix(np.zeros([Bdist.shape[0],(Bdist.shape[1]+Binput.shape[1])]))
275 | B[:,:Bdist.shape[1]] = Bdist
276 | B[:,Bdist.shape[1]:] = Binput
277 |
278 | R = np.matrix(np.zeros([B.shape[1], B.shape[1]]))
279 | #we fill the upper left of R later.
280 | R[Bdist.shape[1]:,Bdist.shape[1]:] = D12.T.dot(D12)
281 | Q = C1.T.dot(C1)
282 |
283 | #Define a helper function:
284 | def has_stable_solution(g, A, B, Q, R, eps):
285 | R[0:Bdist.shape[1], 0:Bdist.shape[1]] = -g**(2)*np.eye(Bdist.shape[1], Bdist.shape[1])
286 |
287 | #Riccati equation prerequisites:
288 | if not analysis.is_stabilisable(A, B):
289 | return False, None
290 |
291 | if not analysis.is_detectable(Q, A):
292 | return False, None
293 |
294 | try:
295 | X = scipy.linalg.solve_continuous_are(A, B, Q, R)
296 | except np.linalg.linalg.LinAlgError:
297 | return False, None
298 |
299 | eigsX = np.linalg.eigvals(X)
300 |
301 | if (np.min(np.real(eigsX)) < 0) or (np.sum(np.abs(np.imag(eigsX)))>eps):
302 | #The ARE has to return a pos. semidefinite solution, but X is not
303 | return False, None
304 |
305 |
306 | CL = A - Binput.dot(np.linalg.inv(D12.T.dot(D12))).dot(Binput.T).dot(X) + g**(-2)*Bdist.dot(Bdist.T).dot(X)
307 | eigs = np.linalg.eigvals(CL)
308 |
309 | return (np.max(np.real(eigs)) < -eps), X
310 |
311 |
312 | X = None
313 | if np.isinf(gammaUB):
314 | #automatically choose an UB
315 | gammaUB = np.float(np.max([1, gammaLB]))
316 |
317 | #Find an upper bound:
318 | counter = 1
319 | while True:
320 |
321 | stab, X2 = has_stable_solution(gammaUB, A, B, Q, R, stabilityBoundaryEps)
322 | if stab:
323 | X = X2.copy()
324 | break
325 |
326 | gammaUB *= 2
327 | counter += 1
328 |
329 | assert counter < 1024, 'Exceeded max number of iterations searching for upper gamma bound!'
330 |
331 | #Find the minimising gain
332 | while (gammaUB-gammaLB)>gammaRelTol*gammaUB:
333 | g = 0.5*(gammaUB+gammaLB)
334 |
335 | stab, X2 = has_stable_solution(g, A, B, Q, R, stabilityBoundaryEps)
336 | if stab:
337 | gammaUB = g
338 | X = X2
339 | else:
340 | gammaLB = g
341 |
342 | assert X is not None, 'No solution found! Check supplied upper bound'
343 |
344 | g = gammaUB
345 | if subOptimality > 1.0:
346 | #compute a sub optimal solution
347 | g *= subOptimality
348 | stab, X = has_stable_solution(g, A, B, Q, R, stabilityBoundaryEps)
349 | assert stab, 'Sub-optimal solution not found!'
350 |
351 | K = np.linalg.inv(D12.T.dot(D12)).dot(Binput.T).dot(X)
352 |
353 | J = g
354 | return K, X, J
355 |
356 |
357 |
--------------------------------------------------------------------------------
/examples/example_controllability.py:
--------------------------------------------------------------------------------
1 | '''Example showing how to test a system's controllability
2 | '''
3 |
4 | from __future__ import print_function, division
5 |
6 | import controlpy
7 |
8 | import numpy as np
9 |
10 | # A single input system, one uncontrollable mode.
11 | A = np.matrix([[0,1,0],[0,0,1],[0,0,5]])
12 | B = np.matrix([[0],[1],[0]])
13 |
14 | uncontrollableModes = controlpy.analysis.uncontrollable_modes(A,B)
15 |
16 | if not uncontrollableModes:
17 | print('System is controllable.')
18 | else:
19 | print('System is uncontrollable. Uncontrollable modes are:')
20 | print(uncontrollableModes)
21 |
22 |
23 |
24 |
25 |
26 |
27 |
28 |
--------------------------------------------------------------------------------
/examples/example_lqr.py:
--------------------------------------------------------------------------------
1 | '''A simple example script, which implements an LQR controller for a double integrator.
2 | '''
3 |
4 | from __future__ import print_function, division
5 |
6 | import controlpy
7 |
8 | import numpy as np
9 |
10 | # Example system is a double integrator:
11 | A = np.matrix([[0,1],[0,0]])
12 | B = np.matrix([[0],[1]])
13 |
14 | # Define our costs:
15 | Q = np.matrix([[1,0],[0,0]])
16 | R = np.matrix([[1]])
17 |
18 | # Compute the LQR controller
19 | gain, X, closedLoopEigVals = controlpy.synthesis.controller_lqr(A,B,Q,R)
20 |
21 | print('The computed gain is:')
22 | print(gain)
23 |
24 | print('The closed loop eigenvalues are:')
25 | print(closedLoopEigVals)
26 |
27 |
28 |
29 |
30 |
31 |
--------------------------------------------------------------------------------
/examples/example_systemGain.py:
--------------------------------------------------------------------------------
1 | '''A simple example script, compute the norm of an LTI system
2 | '''
3 |
4 | from __future__ import print_function, division
5 |
6 | import controlpy
7 |
8 | import numpy as np
9 |
10 | # The system is
11 | # dx = A*x + B*v
12 | # z = C*x
13 | # v is a disturbance.
14 |
15 | A = np.matrix([[-0.1, 10],[0,-0.7]])
16 | B = np.matrix([[0],[1]])
17 | C = np.matrix([[1,0]])
18 |
19 | print('H2 norm: ', controlpy.analysis.system_norm_H2(A, B, C))
20 | print('Hinf norm: ', controlpy.analysis.system_norm_Hinf(A, B, C))
21 |
--------------------------------------------------------------------------------
/setup.cfg:
--------------------------------------------------------------------------------
1 | [metadata]
2 | description-file = README.md
3 |
--------------------------------------------------------------------------------
/setup.py:
--------------------------------------------------------------------------------
1 | from setuptools import setup
2 |
3 | def readme():
4 | with open('README.rst') as f:
5 | return f.read()
6 |
7 | setup(name='controlpy',
8 | version='0.1.1',
9 | description='Python control library',
10 | long_description='Tools for analysing and synthesising controllers in python. Includes LQR solvers, methods for H2 and Hinf, and other potentially useful (state space) methods.',
11 | url='http://github.com/markwmuller/controlpy',
12 | download_url = 'https://github.com/markwmuller/controlpy/archive/0.1',
13 | author='Mark W. Mueller',
14 | author_email='mwm@mwm.im',
15 | license='GPL V3',
16 | packages=['controlpy'],
17 | zip_safe=False,
18 | classifiers=[],
19 | install_requires=['numpy','scipy'],
20 | keywords='control lqr robust H2 Hinf Hinfinity',
21 | tests_require=['cvxpy'],
22 | )
23 |
--------------------------------------------------------------------------------
/tests/test_analysis.py:
--------------------------------------------------------------------------------
1 | from __future__ import print_function, division
2 |
3 | import os
4 | import sys
5 | sys.path.insert(0, os.path.abspath('..'))
6 |
7 | import numpy as np
8 |
9 | np.random.seed(1234)
10 |
11 | import controlpy
12 |
13 | import unittest
14 |
15 | import cvxpy
16 | def sys_norm_h2_LMI(Acl, Bdisturbance, C):
17 | #doesn't work very well, if problem poorly scaled Riccati works better.
18 | #Dullerud p 210
19 | n = Acl.shape[0]
20 | X = cvxpy.Semidef(n)
21 | Y = cvxpy.Semidef(n)
22 |
23 | constraints = [ Acl*X + X*Acl.T + Bdisturbance*Bdisturbance.T == -Y,
24 | ]
25 |
26 | obj = cvxpy.Minimize(cvxpy.trace(Y))
27 |
28 | prob = cvxpy.Problem(obj, constraints)
29 |
30 | prob.solve()
31 | eps = 1e-16
32 | if np.max(np.linalg.eigvals((-Acl*X - X*Acl.T - Bdisturbance*Bdisturbance.T).value)) > -eps:
33 | print('Acl*X + X*Acl.T +Bdisturbance*Bdisturbance.T is not neg def.')
34 | return np.Inf
35 |
36 | if np.min(np.linalg.eigvals(X.value)) < eps:
37 | print('X is not pos def.')
38 | return np.Inf
39 |
40 | return np.sqrt(np.trace(C*X.value*C.T))
41 |
42 |
43 | def sys_norm_hinf_LMI(A, Bdisturbance, C, D = None):
44 | '''Compute a system's Hinfinity norm, using an LMI approach.
45 |
46 | Acl, Bdisturbance are system matrices, describing the systems dynamics:
47 | dx/dt = Acl*x + Bdisturbance*v
48 | where x is the system state and v is the disturbance.
49 |
50 | The system output is:
51 | z = C*x + D*v
52 |
53 | The matrix Acl must be Hurwitz for the Hinf norm to be finite.
54 |
55 | Parameters
56 | ----------
57 | A : (n, n) Matrix
58 | Input
59 | Bdisturbance : (n, m) Matrix
60 | Input
61 | C : (q, n) Matrix
62 | Input
63 | D : (q,m) Matrix
64 | Input (optional)
65 |
66 | Returns
67 | -------
68 | Jinf : Systems Hinf norm.
69 |
70 | See: Robust Controller Design By Convex Optimization, Alireza Karimi Laboratoire d'Automatique, EPFL
71 | '''
72 |
73 | if not controlpy.analysis.is_hurwitz(A):
74 | return np.Inf
75 |
76 | n = A.shape[0]
77 | ndist = Bdisturbance.shape[1]
78 | nout = C.shape[0]
79 |
80 | X = cvxpy.Semidef(n)
81 | g = cvxpy.Variable()
82 |
83 | if D is None:
84 | D = np.matrix(np.zeros([nout, ndist]))
85 |
86 | r1 = cvxpy.hstack(cvxpy.hstack(A.T*X+X*A, X*Bdisturbance), C.T)
87 | r2 = cvxpy.hstack(cvxpy.hstack(Bdisturbance.T*X, -g*np.matrix(np.identity(ndist))), D.T)
88 | r3 = cvxpy.hstack(cvxpy.hstack(C, D), -g*np.matrix(np.identity(nout)))
89 | tmp = cvxpy.vstack(cvxpy.vstack(r1,r2),r3)
90 |
91 | constraints = [tmp == -cvxpy.Semidef(n + ndist + nout)]
92 |
93 | obj = cvxpy.Minimize(g)
94 |
95 | prob = cvxpy.Problem(obj, constraints)
96 |
97 | try:
98 | prob.solve()#solver='CVXOPT', kktsolver='robust')
99 | except cvxpy.error.SolverError:
100 | print('Solution not found!')
101 | return None
102 |
103 | if not prob.status == cvxpy.OPTIMAL:
104 | return None
105 |
106 | return g.value
107 |
108 |
109 |
110 | class TestAnalysis(unittest.TestCase):
111 |
112 | def test_scalar_hurwitz(self):
113 | self.assertTrue(controlpy.analysis.is_hurwitz(np.matrix([[-1]])))
114 | self.assertTrue(controlpy.analysis.is_hurwitz(np.array([[-1]])))
115 | self.assertFalse(controlpy.analysis.is_hurwitz(np.matrix([[1]])))
116 | self.assertFalse(controlpy.analysis.is_hurwitz(np.array([[1]])))
117 |
118 |
119 | def test_multidim_hurwitz(self):
120 | for matType in [np.matrix, np.array]:
121 | Astable = matType([[-1,2,1000], [0,-2,3], [0,0,-9]])
122 | Aunstable = matType([[1,2,1000], [0,-2,3], [0,0,-9]])
123 | Acritical = matType([[0,2,10], [0,-2,3], [0,0,-9]])
124 |
125 | tolerance = -1e-6 # for critically stable case
126 |
127 | for i in range(1000):
128 | T = matType(np.random.normal(size=[3,3]))
129 | Tinv = np.linalg.inv(T)
130 |
131 | Bs = np.dot(np.dot(T,Astable),Tinv)
132 | Bu = np.dot(np.dot(T,Aunstable),Tinv)
133 | Bc = np.dot(np.dot(T,Acritical),Tinv)
134 |
135 | self.assertTrue(controlpy.analysis.is_hurwitz(Bs), str(i))
136 | self.assertFalse(controlpy.analysis.is_hurwitz(Bu), str(i))
137 |
138 | self.assertFalse(controlpy.analysis.is_hurwitz(Bc, tolerance=tolerance), 'XXX'+str(i)+'_'+str(np.max(np.real(np.linalg.eigvals(Bc)))))
139 |
140 |
141 | # def test_uncontrollable_modes(self):
142 | # #TODO: FIXME: THIS FAILS!
143 | # for matType in [np.matrix, np.array]:
144 | #
145 | # es = [-1,0,1]
146 | # for e in es:
147 | # A = matType([[e,2,0],[0,e,0],[0,0,e]])
148 | # B = matType([[0,1,0]]).T
149 | #
150 | # tolerance = 1e-9
151 | # for i in range(1000):
152 | # T = matType(np.random.normal(size=[3,3]))
153 | # Tinv = np.linalg.inv(T)
154 | #
155 | # AA = np.dot(np.dot(T,A),Tinv)
156 | # BB = np.dot(T,B)
157 | #
158 | # isControllable = controlpy.analysis.is_controllable(AA, BB, tolerance=tolerance)
159 | # self.assertFalse(isControllable)
160 | #
161 | # isStabilisable = controlpy.analysis.is_stabilisable(A, B)
162 | # self.assertEqual(isStabilisable, e<0)
163 | #
164 | # if 0:
165 | # #These shouldn't fail!
166 | # uncontrollableModes, uncontrollableEigenValues = controlpy.analysis.uncontrollable_modes(AA, BB, returnEigenValues=True, tolerance=tolerance)
167 | # self.assertEqual(len(uncontrollableModes), 1)
168 | #
169 | # self.assertAlmostEqual(uncontrollableEigenValues[0], 1, delta=tolerance)
170 | # self.assertAlmostEqual(np.linalg.norm(uncontrollableModes[0] - np.matrix([[0,0,1]]).T), 0, delta=tolerance)
171 |
172 |
173 |
174 | def test_time_discretisation(self):
175 | for matType in [np.matrix, np.array]:
176 | Ac = matType([[0,1],[0,0]])
177 | Bc = matType([[0],[1]])
178 |
179 | dt = 0.1
180 |
181 | Ad = matType([[1,dt],[0,1]])
182 | Bd = matType([[dt**2/2],[dt]])
183 | for i in range(1000):
184 | T = matType(np.random.normal(size=[2,2]))
185 | Tinv = np.linalg.inv(T)
186 |
187 | AAc = np.dot(np.dot(T,Ac),Tinv)
188 | BBc = np.dot(T,Bc)
189 |
190 | AAd = np.dot(np.dot(T,Ad),Tinv)
191 | BBd = np.dot(T,Bd)
192 |
193 | AAd2, BBd2 = controlpy.analysis.discretise_time(AAc, BBc, dt)
194 |
195 | self.assertLess(np.linalg.norm(AAd-AAd2), 1e-6)
196 | self.assertLess(np.linalg.norm(BBd-BBd2), 1e-6)
197 |
198 |
199 | #test some random systems against Euler discretisation
200 | nx = 20
201 | nu = 20
202 | dt = 1e-6
203 | tol = 1e-3
204 | for i in range(1000):
205 | Ac = matType(np.random.normal(size=[nx,nx]))
206 | Bc = matType(np.random.normal(size=[nx,nu]))
207 |
208 | Ad1 = np.identity(nx)+Ac*dt
209 | Bd1 = Bc*dt
210 |
211 | Ad2, Bd2 = controlpy.analysis.discretise_time(Ac, Bc, dt)
212 |
213 | self.assertLess(np.linalg.norm(Ad1-Ad2), tol)
214 | self.assertLess(np.linalg.norm(Bd1-Bd2), tol)
215 |
216 |
217 |
218 | def test_system_norm_H2(self):
219 | for matType in [np.matrix, np.array]:
220 | A = matType([[-1,2],[0,-3]])
221 | B = matType([[0,1]]).T
222 | C = matType([[1,0]])
223 |
224 | h2norm = controlpy.analysis.system_norm_H2(A, B, C)
225 |
226 | h2norm_lmi = sys_norm_h2_LMI(A, B, C)
227 |
228 | tol = 1e-3
229 | self.assertLess(np.linalg.norm(h2norm-h2norm_lmi), tol)
230 |
231 |
232 | def test_system_norm_Hinf(self):
233 | for matType in [np.matrix, np.array]:
234 | A = matType([[-1,2],[0,-3]])
235 | B = matType([[0,1]]).T
236 | C = matType([[1,0]])
237 |
238 | hinfnorm = controlpy.analysis.system_norm_Hinf(A, B, C)
239 |
240 | hinfnorm_lmi = sys_norm_hinf_LMI(A, B, C)
241 |
242 | tol = 1e-3
243 | self.assertLess(np.linalg.norm(hinfnorm-hinfnorm_lmi), tol)
244 |
245 | #TODO:
246 | # - observability tests, similar to controllability
247 |
248 |
249 |
250 |
251 | if __name__ == '__main__':
252 | np.random.seed(1)
253 | unittest.main()
254 |
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/tests/test_synth.py:
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1 | from __future__ import print_function, division
2 |
3 | import os
4 | import sys
5 | sys.path.insert(0, os.path.abspath('..'))
6 |
7 | import numpy as np
8 |
9 | np.random.seed(1234)
10 |
11 | import controlpy
12 |
13 | import unittest
14 |
15 | import cvxpy
16 | def synth_h2_state_feedback_LMI(A, Binput, Bdist, C1, D12):
17 | #Dullerud p 217 (?)
18 |
19 | n = A.shape[0] #num states
20 | m = Binput.shape[1] #num control inputs
21 | q = C1.shape[0] #num outputs to "be kept small"
22 |
23 | X = cvxpy.Variable(n,n)
24 | Y = cvxpy.Variable(m,n)
25 | Z = cvxpy.Variable(q,q)
26 |
27 | tmp1 = cvxpy.hstack(X, (C1*X+D12*Y).T)
28 | tmp2 = cvxpy.hstack((C1*X+D12*Y), Z)
29 | tmp = cvxpy.vstack(tmp1, tmp2)
30 |
31 | constraints = [A*X + Binput*Y + X*A.T + Y.T*Binput.T + Bdist*Bdist.T == -cvxpy.Semidef(n),
32 | tmp == cvxpy.Semidef(n+q),
33 | ]
34 |
35 | obj = cvxpy.Minimize(cvxpy.trace(Z))
36 |
37 | prob = cvxpy.Problem(obj, constraints)
38 |
39 | prob.solve(solver='CVXOPT', kktsolver='robust')
40 |
41 | K = -Y.value*np.linalg.inv(X.value)
42 | return K
43 |
44 |
45 | class TestSynthesis(unittest.TestCase):
46 |
47 | def test_h2(self):
48 | for matType in [np.matrix, np.array]:
49 | A = matType([[1,2],[0,3]])
50 | B = matType([[0,1]]).T
51 | Bdist = matType([[0,1]]).T
52 | C1 = matType([[1,0],[0,1],[0,0]])
53 | D12= matType([[0,0,1]]).T
54 |
55 | KLMI = synth_h2_state_feedback_LMI(A, B, Bdist, C1, D12)
56 | K2, X2, J2 = controlpy.synthesis.controller_H2_state_feedback(A, B, Bdist, C1, D12)
57 |
58 | self.assertLess(np.linalg.norm(K2-KLMI), 1e-3*np.linalg.norm(K2)) #note sign difference
59 |
60 |
61 |
62 |
63 | if __name__ == '__main__':
64 | np.random.seed(1)
65 | unittest.main()
66 |
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