Controller Coefficient Truncation Using Lyapunov Performance Certificate

Similar documents
Controller coefficient truncation using Lyapunov performance certificate

Linear Matrix Inequalities in Robust Control. Venkataramanan (Ragu) Balakrishnan School of ECE, Purdue University MTNS 2002

EE363 homework 7 solutions

June Engineering Department, Stanford University. System Analysis and Synthesis. Linear Matrix Inequalities. Stephen Boyd (E.

H 2 Suboptimal Estimation and Control for Nonnegative

Cherry-Picking Control Nodes and Sensors in Dynamic Networks

EE221A Linear System Theory Final Exam

Fast Algorithms for SDPs derived from the Kalman-Yakubovich-Popov Lemma

Denis ARZELIER arzelier

MATH4406 (Control Theory) Unit 1: Introduction Prepared by Yoni Nazarathy, July 21, 2012

Fall 線性系統 Linear Systems. Chapter 08 State Feedback & State Estimators (SISO) Feng-Li Lian. NTU-EE Sep07 Jan08

LMI Methods in Optimal and Robust Control

Modern Optimal Control

Linear Matrix Inequality (LMI)

LQR, Kalman Filter, and LQG. Postgraduate Course, M.Sc. Electrical Engineering Department College of Engineering University of Salahaddin

Modern Optimal Control

Decentralized and distributed control

Delay-independent stability via a reset loop

Balanced Truncation 1

EL2520 Control Theory and Practice

1. Find the solution of the following uncontrolled linear system. 2 α 1 1

14 - Gaussian Stochastic Processes

Subject: Optimal Control Assignment-1 (Related to Lecture notes 1-10)

ROBUST CONTROLLER DESIGN: POLYNOMIALLY PARAMETER DEPENDENT LYAPUNOV FUNCTION APPROACH

FEL3210 Multivariable Feedback Control

The norms can also be characterized in terms of Riccati inequalities.

Lecture 4 Continuous time linear quadratic regulator

MATH4406 (Control Theory) Unit 6: The Linear Quadratic Regulator (LQR) and Model Predictive Control (MPC) Prepared by Yoni Nazarathy, Artem

Convex Optimization Approach to Dynamic Output Feedback Control for Delay Differential Systems of Neutral Type 1,2

STATIC OUTPUT FEEDBACK CONTROLLER DESIGN

Stochastic resource allocation Boyd, Akuiyibo

EE363 homework 8 solutions

Lecture 10: Linear Matrix Inequalities Dr.-Ing. Sudchai Boonto

Multiobjective Optimization Applied to Robust H 2 /H State-feedback Control Synthesis

Quadratic Stability of Dynamical Systems. Raktim Bhattacharya Aerospace Engineering, Texas A&M University

LINEAR QUADRATIC OPTIMAL CONTROL BASED ON DYNAMIC COMPENSATION. Received October 2010; revised March 2011

Event-triggered control subject to actuator saturation

Semidefinite Programming Duality and Linear Time-invariant Systems

16.31 Fall 2005 Lecture Presentation Mon 31-Oct-05 ver 1.1

SYSTEMTEORI - KALMAN FILTER VS LQ CONTROL

Static Output Feedback Stabilisation with H Performance for a Class of Plants

Convex Optimization of Graph Laplacian Eigenvalues

Control with Random Communication Delays via a Discrete-Time Jump System Approach

Development of a Low-Cost Integrated

Event-Triggered Decentralized Dynamic Output Feedback Control for LTI Systems

Chapter 9 Observers, Model-based Controllers 9. Introduction In here we deal with the general case where only a subset of the states, or linear combin

CHAPTER 6 FAST OUTPUT SAMPLING CONTROL TECHNIQUE

LINEAR QUADRATIC GAUSSIAN

Robust Anti-Windup Controller Synthesis: A Mixed H 2 /H Setting

Analytic Center Cutting-Plane Method

Optimal discrete-time H /γ 0 filtering and control under unknown covariances

MS-E2133 Systems Analysis Laboratory II Assignment 2 Control of thermal power plant

EEE582 Homework Problems

MODEL REDUCTION BY A CROSS-GRAMIAN APPROACH FOR DATA-SPARSE SYSTEMS

State Feedback and State Estimators Linear System Theory and Design, Chapter 8.

Design of hybrid control systems for continuous-time plants: from the Clegg integrator to the hybrid H controller

Research Article An Equivalent LMI Representation of Bounded Real Lemma for Continuous-Time Systems

9 The LQR Problem Revisited

Gramians based model reduction for hybrid switched systems

EE363 homework 2 solutions

CALIFORNIA INSTITUTE OF TECHNOLOGY Control and Dynamical Systems

José C. Geromel. Australian National University Canberra, December 7-8, 2017

IN many practical systems, there is such a kind of systems

Integral action in state feedback control

Robust Stability. Robust stability against time-invariant and time-varying uncertainties. Parameter dependent Lyapunov functions

Lecture 6. Foundations of LMIs in System and Control Theory

EECE Adaptive Control

Balancing of Lossless and Passive Systems

Analysis and Synthesis of State-Feedback Controllers With Timing Jitter

Filter Design for Feedback-loop Trade-off of L 1 Adaptive Controller: A Linear Matrix Inequality Approach

INVERSE MODEL APPROACH TO DISTURBANCE REJECTION AND DECOUPLING CONTROLLER DESIGN. Leonid Lyubchyk

Efficient Reinforcement Learning for High Dimensional Linear Quadratic Systems

Lecture 9. Introduction to Kalman Filtering. Linear Quadratic Gaussian Control (LQG) G. Hovland 2004

Analysis of undamped second order systems with dynamic feedback

LMIs for Observability and Observer Design

1 (30 pts) Dominant Pole

EE C128 / ME C134 Feedback Control Systems

Robust Multi-Objective Control for Linear Systems

6.241 Dynamic Systems and Control

Lecture 19 Observability and state estimation

Control Systems Design

Massachusetts Institute of Technology. Department of Electrical Engineering and Computer Science : MULTIVARIABLE CONTROL SYSTEMS by A.

Economic sensor/actuator selection and its application to flexible structure control

Here represents the impulse (or delta) function. is an diagonal matrix of intensities, and is an diagonal matrix of intensities.

On Input Design for System Identification

Appendix A Solving Linear Matrix Inequality (LMI) Problems

Chapter 3. LQ, LQG and Control System Design. Dutch Institute of Systems and Control

SYNTHESIS OF ROBUST DISCRETE-TIME SYSTEMS BASED ON COMPARISON WITH STOCHASTIC MODEL 1. P. V. Pakshin, S. G. Soloviev

Feedback control of transient energy growth in subcritical plane Poiseuille flow

Comparison of Feedback Controller for Link Stabilizing Units of the Laser Based Synchronization System used at the European XFEL

5. Observer-based Controller Design

Linear Matrix Inequalities in Control

STABILITY AND STABILIZATION OF A CLASS OF NONLINEAR SYSTEMS WITH SATURATING ACTUATORS. Eugênio B. Castelan,1 Sophie Tarbouriech Isabelle Queinnec

Consensus Control of Multi-agent Systems with Optimal Performance

WEIGHTING MATRICES DETERMINATION USING POLE PLACEMENT FOR TRACKING MANEUVERS

Control of Chatter using Active Magnetic Bearings

ECE504: Lecture 8. D. Richard Brown III. Worcester Polytechnic Institute. 28-Oct-2008

Lecture 20: Linear Dynamics and LQG

6.241 Dynamic Systems and Control

Control Systems Design

Transcription:

Controller Coefficient Truncation Using Lyapunov Performance Certificate Joëlle Skaf Stephen Boyd Information Systems Laboratory Electrical Engineering Department Stanford University European Control Conference, Kos, Greece, July 2007

Control system description Consider a discrete-time linear time-invariant control system, with plant x p (t + 1) = A p x p (t) + B 1 w(t) + B 2 u(t) z(t) = C 1 x p (t) + D 11 w(t) + D 12 u(t) y(t) = C 2 x p (t) + D 21 w(t) and controller x c (t + 1) = A c x c (t) + B c y(t) u(t) = C c x c (t) + D c y(t) European Control Conference, Kos, Greece, July 2007 1

Nominal and acceptable controllers design parameters or coefficients in controller θ R N (typically entries of A c, B c, C c and D c ) given: set of acceptable controller designs C R N (controllers that achieve given performance specifications) nominal controller design θ nom C European Control Conference, Kos, Greece, July 2007 2

Controller (coefficient) complexity Φ(θ) is complexity of controller described by θ Φ(θ) = N φ i (θ i ), i=1 where φ i (θ i ) gives the complexity of the ith coefficient of θ φ(z) is number of bits needed to express the fractional part of the binary expansion of z European Control Conference, Kos, Greece, July 2007 3

The controller coefficient truncation problem controller coefficient truncation problem (CCTP): find lowest complexity controller among acceptable designs minimize Φ(θ) subject to θ C very difficult to solve can be cast as combinatiorial optimization problem global optimization techniques (e.g., branch-and-bound) can only solve small CCTP need an efficient method that can handle large problems European Control Conference, Kos, Greece, July 2007 4

The algorithm initialize algorihm with nominal design at each step, choose an index i randomly and fix all parameters except θ i use subroutine interv to find an interval [l, u] of acceptable values for θ i use subroutine trunc to find a value of θ i in [l, u] with lower complexity repeat until there is no change in θ run the algorithm several times, with the best controller coefficient vector found taken as the final choice European Control Conference, Kos, Greece, July 2007 5

interv(θ,i) takes as input coefficient vector θ C, and coefficient index i it returns an interval [l, u] with θ i [l, u] and (θ 1,...,θ i 1,z,θ i+1,...,θ N ) C for z [l, u]. simplest choice, always valid: return l = u = θ i other extreme: return largest valid interval that contains θ i typical implementation of interv: return reasonably large interval in C, using linear matrix inequalities (LMIs) European Control Conference, Kos, Greece, July 2007 6

Interval computation via Lyapunov performance certificate given θ C, find a convex set Ĉ such that θ Ĉ C θ Ĉ C European Control Conference, Kos, Greece, July 2007 7

take l = inf{z (θ 1,...,θ i+1, z,θ i+1,...,θ N ) Ĉ}, u = sup{z (θ 1,...,θ i+1,z,θ i+1,...,θ N ) Ĉ}. since Ĉ is convex, (θ 1,...,θ i+1,z,θ i+1,...,θ N ) Ĉ C for z [l, u]. use a Lyapunov performance certificate to find Ĉ θ Ĉ ν L(θ,ν) 0 L is a bi-affine function in ν and θ L(θ,ν) = L 0 + N θ i L i i=1 European Control Conference, Kos, Greece, July 2007 8

given θ C, compute ν such that L(θ, ν) 0 (typically by maximizing minimum eigenvalue of L(θ,ν) or maximizing detl(θ, ν)) fix ν and take Ĉ = {θ L(θ,ν) 0} (C is convex because described by an LMI in θ) need to minimize or maximize scalar variable over an LMI to find l and u can be reduced to an eigenvalue computation, carried out efficiently l = θ i min{1/λ i λ i > 0} u = θ i max{1/λ i λ i < 0} where λ i are the eigenvalues of L(θ, ν) 1/2 L i L(θ,ν) 1/2 European Control Conference, Kos, Greece, July 2007 9

State feedback controller with LQR cost specification plant is given by: x(t + 1) = Ax(t) + Bu(t), x(0) = x 0 controlled by a state feedback gain controller: u(t) = Kx(t) design variables are entries of the matrix K performance measure is LQR cost [ ] J(K) = E x(t) T Qx(t) + u(t) T Ru(t) t=0 = Tr(ΣP) where P is unique solution to (A + BK) T P(A + BK) P + Q + K T RK = 0 European Control Conference, Kos, Greece, July 2007 10

nominal design K nom is the optimal state feedback controller set of acceptable controller designs is set of ǫ-suboptimal designs C = {K J(K) (1 + ǫ)j nom } Lyapunov performance certificate: P (A + BK) T P(A + BK) Q + K T RK Tr(ΣP) (1 + ǫ)j nom P 0 European Control Conference, Kos, Greece, July 2007 11

given K C, take P to be the solution of maximize λ min (L(K, P)) subject to L(K, P) 0. for a particular choice P, Ĉ = {K (A + BK) T P(A + BK) P + Q + K T RK 0} easy to show that Ĉ C European Control Conference, Kos, Greece, July 2007 12

Numerical instance A R 10 10 and B R 10 5 randomly generated Σ = I, Q = I, R = I fractional part of each entry of K nom expressed with 40 bits; Φ(K) = 2000 bits. ǫ = 15% i.e., acceptable feedback controllers are up to 15%-suboptimal European Control Conference, Kos, Greece, July 2007 13

total number of bits required to express K versus iteration number in a sample run of the algorihm 2000 1800 1600 1400 Φ(θ) 1200 1000 800 600 400 200 0 0 10 20 30 40 50 60 70 80 90 100 iteration number algorithm converges to a complexity of 85 bits in 50 iterations European Control Conference, Kos, Greece, July 2007 14

best design afer 100 random runs of the algorithm achieves Φ(K) = 75 bits (1.5 bits per coefficient) 10 frequency frequency 8 6 4 2 0 1 0.75 0.5 0.25 0 0.25 0.5 0.75 1 25 20 15 10 5 θ nom i 0 1 0.75 0.5 0.25 0 0.25 0.5 0.75 1 very aggressive coefficient truncation! θ i European Control Conference, Kos, Greece, July 2007 15

Dynamic controller with decay rate specification plant is given by x p (t + 1) = A p x p (t) + B p u(t), y(t) = C p x p (t) controlled by a dynamic controller x c (t + 1) = A c x c (t) + B c y(t), u(t) = C c x c (t) closed-loop system given by x(t + 1) = Ax(t) where x(t) = [ xp (t) x c (t) ], A = [ ] Ap B p C c B c C p A c European Control Conference, Kos, Greece, July 2007 16

design variables are entries of the controller matrices A c, B c and C c performance measure is the decay rate of the closed-loop system: J(A c, B c, C c ) = ρ(a) given a nominal design (A nom c, B nom set of acceptable controller designs where α = (1 + ǫ)j(a nom c c,cc nom ) C = {(A c, B c,c c ) J(A c, B c, C c ) α},, B nom, C nom c c ) Lyapunov performance certificate [ α 2 P A T PA 0 0 P ] 0 European Control Conference, Kos, Greece, July 2007 17

for (A c, B c, C c ) C, take P to be the solution of maximize λ min (L(A c,b c,c c,p)) subject to L(A c, B c, C c, P) 0 Tr(P) = 1. for a fixed choice of P, Ĉ = {(A c, B c, C c ) A T PA α 2 P } easy to show that Ĉ C European Control Conference, Kos, Greece, July 2007 18

Numerical instance plant is given by x p (t + 1) = A p x p (t) + B p u(t) + w(t), y(t) = C p x p (t) + v(t), where w(t) N(0, I) is input noise and v(t) N(0, I) is measurement noise A pr 5 5, B p R 5 2, C p R 2 5 generated randomly plant controlled by an LQG controller with Q = I, R = I. fractional part of each entry of A nom c, Bc nom 40 bits; Φ(θ nom ) = 1800 bits ǫ = 5% and C nom c is expressed with European Control Conference, Kos, Greece, July 2007 19

progress of the complexity Φ(θ) and percentage deterioration in performance 100(J J nom )/J nom during 3 sample runs of the algorithm 2000 1500 Φ(θ) 1000 500 0 0 50 100 150 200 250 300 350 400 100(J J nom )/J nom 5 4 3 2 1 0 0 50 100 150 200 250 300 350 400 iteration number European Control Conference, Kos, Greece, July 2007 20

best design complexity versus number of sample runs of the algorithm 205 200 195 190 Φ(θ) 185 180 175 170 165 160 0 10 20 30 40 50 60 70 80 90 100 number of sample runs best design after 100 random runs of the algorithm achieves a complexity of Φ(θ) = 164 bits and J(θ) = 1.0362J(θ nom ) European Control Conference, Kos, Greece, July 2007 21