Dr. Broucke Talk

Page 1

Reach Control Problem Mireille E. Broucke Systems Control Group Department of Electrical and Computer Engineering University of Toronto

March 31, 2014


Acknowledgements • Past Students – Dr. Mohamed Helwa, PhD – Dr. Elham Semsar-Kazerooni, Postdoc – Krishnaa Mehta, MASc – Graeme Ashford, MASc – Marcus Ganness, MASc – Dr. Zhiyun Lin, Postdoc – Bartek Roszak, MASc • Current Students – Zachary Kroeze, PhD – Matthew Martino, MASc – Melkior Ornik, PhD – Mario Vukosavljev, MASc

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Logic Specifications in Control

Motivating Example

1


Linear Temporal Logic Boolean operators: ¬, ∧, ∨ Temporal operators: - always, ♦ - eventually, U - until • The power in the resistor never exceeds P. • The power through load 1 reaches P1 before the power through load 2 reaches P2. • Two loads must be turned on but not at the same time. • The pendulum swings through θ = 0 at least two times. • In a multi-agent system, if a vehicle visits a target, then no vehicle will visit the same target ever again. • For a walking robot, eventually always the right leg touches the ground and the left knee has an angle between θ1 and θ2 .

Motivating Example

2


Cart and Conveyor Belts

Control Specifications: 1. Safety: |x| ≤ 3, |x| ˙ ≤ 3, |x + x| ˙ ≤ 3. ˙ ≥ 1. 2. Liveness: |x| + |x| 3. Temporal behavior: Every box arriving on conveyor 1 is picked up and deposited on conveyor 2.

Motivating Example

3


Stabilization-based Approach

• Equilibrium stabilization gives no guarantee of safety or liveness. • Difficult to design for trade-off between safety and liveness. • Operationally inefficient - system must be run unnaturally slowly.

Motivating Example

4


Literature on LTL and Control • A. Bemporad and M. Morari. Control of systems integrating logic, dynamics, and constraints. Automatica, 1999. • P. Tabuada and G. Pappas. Model checking LTL over controllable linear systems is decidable. LNCS, 2003. • M. Kloetzer and C. Belta. A fully automated framework for control of linear systems from temporal logic specifications. IEEE TAC, 2008. • T. Wongpiromsarn, U. Topcu, and R.M. Murray. Receding horizon temporal logic planning for dynamical systems. CDC, 2009. • S. Karaman and E. Frazzoli. Sampling-based motion planning with deterministic mu-calculus specifications. CDC, 2009. • A. Girard. Synthesis using approximately bisimilar abstractions: state-feedback controllers for safety specifications. HSCC, 2010.

Motivating Example

5


Preferred Approach

• Safety is built in up front and is provably robust. • Liveness can be traded off with safety by adjusting the size of the hole. • Triangulation is used in algebraic topology, physics, numerical solution of PDE’s, computer graphics, etc. It has a role in control theory. Motivating Example

6


Reach Control Problem

Reach Control Problem

7


What is Given 1. An affine system x˙ = Ax + Bu + a ,

x ∈ Rn ,

u ∈ Rm .

(1)

2. An n-dimensional simplex S = conv{v0 , . . . , vn }. 3. A set of restricted facets {F1 , . . . , Fn }. 4. One exit facet F0 .

Reach Control Problem

8


Setup

v0 B = ImB cone(S) h1

h2 S

O = {x | Ax + a ∈ B} v1

Notation: Reach Control Problem

C(v1 )

F0

C(v2 )

v2

n C(vi ) := y ∈ R | hj · y ≤ 0 , j 6= i 9


Problem Statement Problem. (RCP) Given simplex S and system (1), find u(x) such that: for each x0 ∈ S there exist T ≥ 0 and γ > 0 such that • x(t) ∈ S for all t ∈ [0, T ], • x(T ) ∈ F0 , and • x(t) ∈ / S for all t ∈ (T, T + γ).

Notation: Reach Control Problem

S

S −→ F0

by feedback of class U. 10


Affine Feedback S

Theorem. S −→ F0 by affine feedback u(x) = Kx + g if and only if (a) The invariance conditions hold: Avi + a + Bu(vi ) ∈ C(vi ), i ∈ {0, . . . , n}. (b) The closed-loop system has no equilibrium in S.

[HvS06] L.C.G.J.M. Habets and J.H. van Schuppen. IEEE TAC 2006. [RosBro06] B. Roszak and M.E. Broucke. Automatica 2006. Reach Control Problem

11


Numerical Example 

x˙ = 

0 0

1 0

x + 

0 1

u + 

4

1

S determined by: v0 = (−1, −3), v1 = (4, −1), and v2 = (3, −6).

Invariance conditions give: • hT1 (Av0 + Bu0 + a) ≤ 0

u0 ≥ −1.75

• hT2 (Av0 + Bu0 + a) ≤ 0

u0 ≤ −0.6

• hT2 (Av1 + Bu1 + a) ≤ 0

u1 ≤ 0.2

• hT1 (Av2 + Bu2 + a) ≤ 0

u2 ≥ 0.5.

Reach Control Problem

12


Numerical Example Choose u0 = −1.175, u1 = 0.2, u2 = 0.5.

h2 v1 = (4, −1)

v0 = (−1, −3)

F0 equilibrium

v2 = (3, −6) h1

Reach Control Problem

13


Numerical Example The affine feedback is: u = [0.325 − 0.125]x − 1.225 h2 v1 = (4, −1)

v0 = (−1, −3)

F0 equilibrium

v2 = (3, −6) h1

Reach Control Problem

14


Geometric Theory

Geometric Theory

15


Equilibrium Set and Triangulations Let B = ImB. The equilibrium set is O = {x | Ax + a ∈ B} . Define G := S ∩ O . Assumption. If G = 6 ∅, then G is a κ-dimensional face of S, where 0 ≤ κ < n. Reorder indices so that G = conv{v1 , . . . , vκ+1 } . Note: v0 6∈ G, otherwise there’s a trivial solution to RCP.

Can be achieved using the placing triangulation. Geometric Theory

16


Continuous State Feedback

Theorem. Suppose the triangulation assumption holds. TFAE: S

(a) S −→ F0 by affine feedback. S

(b) S −→ F0 by continuous state feedback.

Proof. Fixed point argument using Sperner’s lemma, M -matrices.

[B10] M.E. Broucke. SIAM J. Control and Opt. 2010.

Geometric Theory

17


Limits of Continuous State Feedback v0

y0 F1

F2

b2 S

v1 F0

v2

b1

Let u(x) be a continuous state feedback satisyfing the invariance conditions. If B = sp{b} and G = v1 v2 , then y(x) := c(x)b ,

x ∈ v1 v2

n

c:R

→ R continuous ,

where c(v1 ) ≥ 0 and c(v2 ) ≤ 0. By Intermediate Value Theorem there exists x s.t. c(x) = 0. Geometric Theory

18


Conditions for a Topological Obstruction 1. B ∩ cone(S) = 0

nontriviality condition

2. 6 ∃ lin. indep. set {b1 , . . . , bκ+1 | bi ∈ B ∩ C(vi )}

system is “underactuated”

B cone(S)

v0

h3 v3 v1 b1

G b2 v2

Geometric Theory

O 19


Reach Control Indices Theorem. There exist integers r1 , . . . , rp ≥ 2 and control directions bi ∈ B ∩ C(vi ) such that w.l.o.g. B ∩ C(vi ) ⊂ sp{bm1 , . . . , bm1 +r1 −1 } , i = m1 , . . . , m1 + r1 − 1 , .. .

.. .

B ∩ C(vi ) ⊂ sp{bmp , . . . , bmp +rp −1 } , i = mp , . . . , mp + rp − 1 ,

where mk := r1 + · · · + rk−1 + 1 , k = 1, . . . , p. Moreover, 0 ∈ conv bmk , . . . , bmk +rk −1 , k = 1, . . . , p . {r1 , . . . , rp } are called the reach control indices of system (1). [BG14] M.E. Broucke and M. Ganness. SIAM J. Control and Opt. 2014. Geometric Theory

20


Reach Control Indices For k = 1, . . . , p define Gk := conv vmk , . . . , vmk +rk −1 .

Theorem. Let u(x) be a continuous state feedback satisfying the invariance conditions. Then each Gk contains an equilibrium of the closed-loop system.

[B10] M.E. Broucke. SIAM J. Control and Opt. 2010.

Geometric Theory

21


Piecewise Affine Feedback

1.2 1 1 0.8 0.8 0.6 0.6 0.4

0.4

0.2

0.2

0

−0.2

O

−1

−0.8

−0.4

−0.2

0

0.2

0.4

(a) Affine feedback

Geometric Theory

0

F0 −0.6

F0’

0.6

0.8

1

−0.2 −1

F0 −0.8

−0.6

−0.4

−0.2

0

0.2

0.4

0.6

0.8

1

(b) PWA feedback

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Piecewise Affine Feedback Theorem. Suppose the triangulation assumption holds. For a somewhat stronger version of RCP, TFAE: S

1. S −→ F0 by piecewise affine feedback. S

2. S −→ F0 by open-loop controls.

[BG14] M.E. Broucke and M. Ganness. SIAM J. Control and Opt. 2014.

Geometric Theory

23


Time-varying Affine Feedback Equilibria are such a drag...

v0

v0

v1

v2 x

Geometric Theory

v1

v2 x

24


Time-varying Affine Feedback Theorem. Suppose the triangulation assumption holds and the invariance conditions are solvable. There exists c > 0 sufficiently small S such that S −→ F0 using the time-varying affine feedback u(x, t) = e−ct u0 (x) + (1 − e−ct )u∞ (x) where u0 (x) = K 0 x + g 0 places closed-loop equilibria at vm1 , . . . , vmp and u∞ (x) = K ∞ x + g ∞ places closed-loop equilibria at vm1 +r1 −1 , . . . , vmp +rp −1 .

[AB13] G. Ashford and M. Broucke. Automatica 2013.

Geometric Theory

25


Lyapunov Theory

Lyapunov Theory

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Revisiting RCP on Simplices S

Theorem. S −→ F0 by the affine feedback u(x) = Kx + g, if and only if (a) The invariance conditions hold. (b) Linear Flow Condition: (∃ξ ∈ Rn ) ξ · (Ax + Bu(x) + a) < 0, ∀x ∈ S. Under affine feedback, the flow condition is necessary and sufficient for leaving S in finite time. [HvS06] Habets and van Schuppen. IEEE TAC 2006. [RosBro06] Roszak and Broucke. Automatica 2006. Lyapunov Theory

27


Lyapunov Theory for RCP • For a given feedback u(x) solving RCP on a polytope P, the invariance conditions can be easily verified, but a linear flow condition may not exist. • In these cases RCP is verified to be solved via exhaustive simulation. • Urgent need for a verification tool for RCP, analogous to Lyapunov theory for stability.

We propose a Lyapunov-like analysis tool.

Lyapunov Theory

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Flow Functions Let u(x) be a locally Lipschitz state feedback satisfying the invariance conditions of P. To verify trajectories leave a compact set P: • V (x) is C 1 , V˙ (x) 6= 0, x ∈ P • V (x) = h0 · x, • V (x) = ξ · x,

V˙ (x) = h0 · (Ax + Bu(x) + a) 6= 0, x ∈ P V˙ (x) = ξ · (Ax + Bu(x) + a) 6= 0, x ∈ P

[RHL77] [HvS04] [RB06,HB11]

Definition. Let P ⊂ D. A flow function is any scalar function V : D → R that is strictly decreasing along solutions.

Lyapunov Theory

29


Locally Lipschitz Flow Functions

Theorem. Consider system (1) on P ⊂ D. Let u(x) be a c.s.f. such that the closed-loop vector field f (x) is locally Lipschitz on D. If there exists a locally Lipschitz V : D → R such that Df+ V (x) ≤ −1 ,

x∈P

then all trajectories leave P in finite time.

[HB14] M. Helwa and M. Broucke. Automatica 2014.

Lyapunov Theory

30


LaSalle Principle for RCP Theorem. Consider system (1) on P ⊂ D. Let u(x) be a c.s.f. such that the closed-loop vector field f (x) is locally Lipschitz on D. Suppose there exists a locally Lipschitz V : D → R such that Df+ V (x) ≤ 0, x ∈ P. Let M := {x ∈ P | Df+ V (x) = 0} . If M does not contain an invariant set, then all trajectories starting in P leave it in finite time.

Lyapunov Theory

31


Flow Functions on Simplices v4

v3

S2 S1 v1

F0

v2

Theorem. Let T = {S1 , S2 } be a triangulation of P, and u(x) a P

PWA feedback defined on T. If P −→ F0 by u(x), then there exist affine functions V1 (x) and V2 (x) such that V (x) := max{V1 (x), V2 (x)} satisfies Df+ V (x) < 0 for all x ∈ P. Lyapunov Theory

32


Analogies with Stability Theory Stability

RCP

Lyapunov function: V (x) C 1 positive definite

Flow function: V (x) locally Lipschitz

Neg. def. condition: V˙ (x) < 0

Flow condition: Df+ V (x) < −1

LaSalle theorem: V˙ (x) ≤ 0, trajectories tend to inv. set in M

LaSalle theorem: Df+ V (x) ≤ 0, no inv. sets in M

Linear systems: V (x) = xT P x

Affine systems: V (x) = ξ · x

Piecewise linear systems: V (x) = max{Vi (x)}

PWA feedback: max{Vi (x)}

Lyapunov Theory

V (x)

=

33


Emerging Applications

Emerging Applications

34


Automated Anesthesia

Emerging Applications

35


Aggressive Maneuvers of Mechanical Systems State Space Polytope 1.5

S10 S11

Crane Angle (rad)

1

S12

S9

0.5

S8

S13

0

S7

S1

−0.5

S2

−1

S6 S4 S3

Vertical Position (m)

−1.5

Emerging Applications

S5

−1

−0.5

0 Trolley Position (m) Crane Problem Animation

0.5

1

−1

−0.5

0 Trolley Position (m)

0.5

1

0.1 0 −0.1 −0.2 −0.3

36


Bumpless Transfer of Robotic Manipulators

ξ2

ρemax

y2 θ2

P1

P2

m2

x2

l2

F0

ks , rs

µ2

F1

ρ0

O

ρ3

µsw

P3

F2

l1 θ1

ρemin

x1

y1

y0

µ1

ρ2 ξ1

ρ1 P5 F3 P4

x0

Emerging Applications

x1

x2

−µ1 ρˆe

37


Motivating Example S ∩ O = ∅ [B10]

B

B ∩ cone(S) 6= 0 [B10]

B ∩ cone(S) 6= 0 [AB13] or [BG14]

O

Emerging Applications

38


Final Design 4 3 2 1 0 −1 −2 −3 −4 −4

Emerging Applications

−3

−2

−1

0

1

2

3

4

39


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