ME 233, UC Berkeley, Spring Background Parseval s Theorem Frequency-shaped LQ cost function Transformation to a standard LQ
|
|
- Griffin Cox
- 5 years ago
- Views:
Transcription
1 ME 233, UC Berkeley, Spring 214 Xu Chen Lecture 1: LQ with Frequency Shaped Cost Function FSLQ Background Parseval s Theorem Frequency-shaped LQ cost function Transformation to a standard LQ Big picture why are we learning this: in standard LQ, Q and R are constant matrices in the cost function x T tqxt + ρu T trut dt 1 how can we introduce more design freedom for Q and R? Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
2 Connection between time and frequency domains Theorem Parseval s Theorem For a square integrable signal f t defined on [, f T tf tdt = 1 2π F T jωf jωdω 1D case: f t 2 dt = 1 F jω 2 dω 2π Intuition: energy in time-domain equals energy in frequency domain For the general case, f t can be acausal. We have f T tf tdt = 1 F T jωf jωdω 2π Discrete-time version: k= f T kf k = 1 2π F T e jω F e jω dω Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME History Marc-Antoine Parseval : French mathematician published just five but important mathematical publications in total source: Wikipedia.org Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
3 Frequency-domain LQ cost function From Parseval s Theorem, the LQ cost in frequency domain is = 1 2π x T tqxt + ρu T trut dt 2 X T jωqxjω + ρu T jωrujω dω 3 Frequency-shaped LQ expands Q and R to frequency-dependent functions: 1 X T jωq jωxjω + ρu T jωr jωujω dω 2π 4 Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME Frequency-domain LQ cost function Let Q jω = Q T f jωq f jω, X f jω = Q f jωx jω R jω = R T f jωr f jω, U f jω = R f jωu jω 4 becomes 1 2π Xf T jωx f jω + ρuf T jωu f jω dω which is equivalent to using Parseval s Theorem again xf T tx f t + ρuf T tu f t dt 5 Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
4 Frequency-domain LQ cost function Summarizing, we have: plant: { ẋ t y t = Ax t + Bu t = Cx t 6 new cost: xf T tx f t + ρuf T tu f t dt 7 filtered states and inputs: x t Q f s x f t, u t R f s u f t We just need to translate the problem to a standard one [which we know very well how to solve] Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME Frequency-domain weighting filters state filtering x t Q f s x f t a MIMO process in general: if x t R n and x f t R q, then Q f s is a q n transfer function matrix Q f s: state filter; designer s choice; can be selected to meet the desired control action and the performance requirements write Q f s = C 1 si A 1 1 B 1 + D 1 in the general state-space realization: { ż1 t = A 1 z 1 t + B 1 xt 8 x f t = C 1 z 1 t + D 1 xt Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
5 Frequency-domain weighting filters input filtering u t R f s u f t R f s: input filter; designer s choice; can be selected to meet the robustness requirements write R f s = C 2 si A 2 1 B 2 + D 2 in the general state-space realization: { ż 2 t = A 2 z 2 t + B 2 ut 9 u f t = C 2 z 2 t + D 2 ut Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME Back to time-domain design Combining 6, 8 and 9 gives the enlarged system xt A xt d z 1 t = B 1 A 1 z 1 t + dt z 2 t A 2 z 2 t }{{}}{{} x e t A e B B 2 }{{} B e ut and xt x f t = [D 1 C 1 ] z }{{} 1 t C e z 2 t u f t = [ C 2 ]x e t + D 2 ut Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
6 Summary of solution With the enlarged system, the cost xf T tx f t + ρuf T tu f t dt 1 translates to xe T tq e x e t + 2u T t [ ρd2 T C ] 2 x e t + u T tρd2 T D 2 }{{}}{{} N e R e Q e = D T 1 D 1 D T 1 C 1 C T 1 D 1 C T 1 C 1 ρc T 2 C 2 solution see appendix for more details: ut dt u t = Re 1 Be T P e + N e x e t = Kx t K 1 z 1 t K 2 z 2 t algebraic Riccati equation: A T e P e + P e A e B T e P e + N e T R 1 e B T e P e + N e + Q e = Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME Implementation structure of the FSLQ system: B si A 1 x u f D C z 2 2 si A 2 1 B 2 K 2 K 1 x f + C 1 si A z 1 B 1 D 1 K Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
7 Appendix: general LQ solution Consider LQ problems with cost x T tc}{{ T C} x t + 2u T tnx t + u T tru t dt 11 Q and system dynamics ẋ t = Ax t + Bu t assume A, B is controllable/stabilizable and A, C is observable/detectable the solution of the problem is u t = R 1 B T P + Nx t A T P + PA B T P + N T R 1 B T P + N + Q = Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME Appendix: general LQ solution Intuition: under the assumptions, we know we can stabilize the system and drive x t to zero. Consider V t = x T tpx t V V = = Adding 11 on both sides yields V V + x T t Q + PA + A T P V tdt x T t PA + A T P x t + 2x T tpbu t dt x t + 2x T t PB + N T u t + u T tru t dt 12 to minimize the cost, we are going to re-organize the terms in 12 into some squared terms Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
8 Appendix: general LQ solution completing the squares : 2x T t PB + N T u t+u T tru t = R 1/2 u t + R 1/2 B T P + N x t x T t PB + N T R 1 B T P + N x t hence 12 is actually V V + J [ = x T t Q + PA + A T P PB + N T R 1 B T P + N x t + R 1/2 u t + R 1/2 B T P + N x t hence J min = V = x T Px is achieved when Q + PA + A T P PB + N T R 1 B T P + N = and u t = R 1 B T P + N x t 2 2 ] dt 2 2 Lecture 1: LQ with Frequency Shaped Cost Function FSLQ ME
Stability of Parameter Adaptation Algorithms. Big picture
ME5895, UConn, Fall 215 Prof. Xu Chen Big picture For ˆθ (k + 1) = ˆθ (k) + [correction term] we haven t talked about whether ˆθ(k) will converge to the true value θ if k. We haven t even talked about
More informationLecture 2: Discrete-time Linear Quadratic Optimal Control
ME 33, U Berkeley, Spring 04 Xu hen Lecture : Discrete-time Linear Quadratic Optimal ontrol Big picture Example onvergence of finite-time LQ solutions Big picture previously: dynamic programming and finite-horizon
More informationOptimal Control. Quadratic Functions. Single variable quadratic function: Multi-variable quadratic function:
Optimal Control Control design based on pole-placement has non unique solutions Best locations for eigenvalues are sometimes difficult to determine Linear Quadratic LQ) Optimal control minimizes a quadratic
More informationHankel Optimal Model Reduction 1
Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science 6.242, Fall 2004: MODEL REDUCTION Hankel Optimal Model Reduction 1 This lecture covers both the theory and
More informationExtensions and applications of LQ
Extensions and applications of LQ 1 Discrete time systems 2 Assigning closed loop pole location 3 Frequency shaping LQ Regulator for Discrete Time Systems Consider the discrete time system: x(k + 1) =
More informationRaktim Bhattacharya. . AERO 632: Design of Advance Flight Control System. Norms for Signals and Systems
. AERO 632: Design of Advance Flight Control System Norms for Signals and. Raktim Bhattacharya Laboratory For Uncertainty Quantification Aerospace Engineering, Texas A&M University. Norms for Signals ...
More informationOPTIMAL CONTROL. Sadegh Bolouki. Lecture slides for ECE 515. University of Illinois, Urbana-Champaign. Fall S. Bolouki (UIUC) 1 / 28
OPTIMAL CONTROL Sadegh Bolouki Lecture slides for ECE 515 University of Illinois, Urbana-Champaign Fall 2016 S. Bolouki (UIUC) 1 / 28 (Example from Optimal Control Theory, Kirk) Objective: To get from
More information5. Observer-based Controller Design
EE635 - Control System Theory 5. Observer-based Controller Design Jitkomut Songsiri state feedback pole-placement design regulation and tracking state observer feedback observer design LQR and LQG 5-1
More informationNonlinear Observers. Jaime A. Moreno. Eléctrica y Computación Instituto de Ingeniería Universidad Nacional Autónoma de México
Nonlinear Observers Jaime A. Moreno JMorenoP@ii.unam.mx Eléctrica y Computación Instituto de Ingeniería Universidad Nacional Autónoma de México XVI Congreso Latinoamericano de Control Automático October
More informationECEEN 5448 Fall 2011 Homework #4 Solutions
ECEEN 5448 Fall 2 Homework #4 Solutions Professor David G. Meyer Novemeber 29, 2. The state-space realization is A = [ [ ; b = ; c = [ which describes, of course, a free mass (in normalized units) with
More informationLecture 15: H Control Synthesis
c A. Shiriaev/L. Freidovich. March 12, 2010. Optimal Control for Linear Systems: Lecture 15 p. 1/14 Lecture 15: H Control Synthesis Example c A. Shiriaev/L. Freidovich. March 12, 2010. Optimal Control
More informationChapter 3. LQ, LQG and Control System Design. Dutch Institute of Systems and Control
Chapter 3 LQ, LQG and Control System H 2 Design Overview LQ optimization state feedback LQG optimization output feedback H 2 optimization non-stochastic version of LQG Application to feedback system design
More informationRiccati Equations and Inequalities in Robust Control
Riccati Equations and Inequalities in Robust Control Lianhao Yin Gabriel Ingesson Martin Karlsson Optimal Control LP4 2014 June 10, 2014 Lianhao Yin Gabriel Ingesson Martin Karlsson (LTH) H control problem
More informationTopic # Feedback Control Systems
Topic #17 16.31 Feedback Control Systems Deterministic LQR Optimal control and the Riccati equation Weight Selection Fall 2007 16.31 17 1 Linear Quadratic Regulator (LQR) Have seen the solutions to the
More information1. Find the solution of the following uncontrolled linear system. 2 α 1 1
Appendix B Revision Problems 1. Find the solution of the following uncontrolled linear system 0 1 1 ẋ = x, x(0) =. 2 3 1 Class test, August 1998 2. Given the linear system described by 2 α 1 1 ẋ = x +
More information6.241 Dynamic Systems and Control
6.241 Dynamic Systems and Control Lecture 12: I/O Stability Readings: DDV, Chapters 15, 16 Emilio Frazzoli Aeronautics and Astronautics Massachusetts Institute of Technology March 14, 2011 E. Frazzoli
More informationProblem 1 Cost of an Infinite Horizon LQR
THE UNIVERSITY OF TEXAS AT SAN ANTONIO EE 5243 INTRODUCTION TO CYBER-PHYSICAL SYSTEMS H O M E W O R K # 5 Ahmad F. Taha October 12, 215 Homework Instructions: 1. Type your solutions in the LATEX homework
More informationEE C128 / ME C134 Final Exam Fall 2014
EE C128 / ME C134 Final Exam Fall 2014 December 19, 2014 Your PRINTED FULL NAME Your STUDENT ID NUMBER Number of additional sheets 1. No computers, no tablets, no connected device (phone etc.) 2. Pocket
More informationME 234, Lyapunov and Riccati Problems. 1. This problem is to recall some facts and formulae you already know. e Aτ BB e A τ dτ
ME 234, Lyapunov and Riccati Problems. This problem is to recall some facts and formulae you already know. (a) Let A and B be matrices of appropriate dimension. Show that (A, B) is controllable if and
More informationControl Systems. Frequency domain analysis. L. Lanari
Control Systems m i l e r p r a in r e v y n is o Frequency domain analysis L. Lanari outline introduce the Laplace unilateral transform define its properties show its advantages in turning ODEs to algebraic
More informationState Regulator. Advanced Control. design of controllers using pole placement and LQ design rules
Advanced Control State Regulator Scope design of controllers using pole placement and LQ design rules Keywords pole placement, optimal control, LQ regulator, weighting matrixes Prerequisites Contact state
More informationMin-Max Output Integral Sliding Mode Control for Multiplant Linear Uncertain Systems
Proceedings of the 27 American Control Conference Marriott Marquis Hotel at Times Square New York City, USA, July -3, 27 FrC.4 Min-Max Output Integral Sliding Mode Control for Multiplant Linear Uncertain
More informationLinearization problem. The simplest example
Linear Systems Lecture 3 1 problem Consider a non-linear time-invariant system of the form ( ẋ(t f x(t u(t y(t g ( x(t u(t (1 such that x R n u R m y R p and Slide 1 A: f(xu f(xu g(xu and g(xu exist and
More informationLecture 8. Applications
Lecture 8. Applications Ivan Papusha CDS270 2: Mathematical Methods in Control and System Engineering May 8, 205 / 3 Logistics hw7 due this Wed, May 20 do an easy problem or CYOA hw8 (design problem) will
More informationLinear System Theory
Linear System Theory Wonhee Kim Chapter 6: Controllability & Observability Chapter 7: Minimal Realizations May 2, 217 1 / 31 Recap State space equation Linear Algebra Solutions of LTI and LTV system Stability
More informationSuppose that we have a specific single stage dynamic system governed by the following equation:
Dynamic Optimisation Discrete Dynamic Systems A single stage example Suppose that we have a specific single stage dynamic system governed by the following equation: x 1 = ax 0 + bu 0, x 0 = x i (1) where
More informationFEL3210 Multivariable Feedback Control
FEL3210 Multivariable Feedback Control Lecture 8: Youla parametrization, LMIs, Model Reduction and Summary [Ch. 11-12] Elling W. Jacobsen, Automatic Control Lab, KTH Lecture 8: Youla, LMIs, Model Reduction
More informationProblem Set 4 Solution 1
Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science 6.245: MULTIVARIABLE CONTROL SYSTEMS by A. Megretski Problem Set 4 Solution Problem 4. For the SISO feedback
More informationH 2 Optimal State Feedback Control Synthesis. Raktim Bhattacharya Aerospace Engineering, Texas A&M University
H 2 Optimal State Feedback Control Synthesis Raktim Bhattacharya Aerospace Engineering, Texas A&M University Motivation Motivation w(t) u(t) G K y(t) z(t) w(t) are exogenous signals reference, process
More informationRaktim Bhattacharya. . AERO 632: Design of Advance Flight Control System. Preliminaries
. AERO 632: of Advance Flight Control System. Preliminaries Raktim Bhattacharya Laboratory For Uncertainty Quantification Aerospace Engineering, Texas A&M University. Preliminaries Signals & Systems Laplace
More informationLecture 9. Introduction to Kalman Filtering. Linear Quadratic Gaussian Control (LQG) G. Hovland 2004
MER42 Advanced Control Lecture 9 Introduction to Kalman Filtering Linear Quadratic Gaussian Control (LQG) G. Hovland 24 Announcement No tutorials on hursday mornings 8-9am I will be present in all practical
More informationStatic and Dynamic Optimization (42111)
Static and Dynamic Optimization (421) Niels Kjølstad Poulsen Build. 0b, room 01 Section for Dynamical Systems Dept. of Applied Mathematics and Computer Science The Technical University of Denmark Email:
More informationSYSTEMTEORI - KALMAN FILTER VS LQ CONTROL
SYSTEMTEORI - KALMAN FILTER VS LQ CONTROL 1. Optimal regulator with noisy measurement Consider the following system: ẋ = Ax + Bu + w, x(0) = x 0 where w(t) is white noise with Ew(t) = 0, and x 0 is a stochastic
More informationInfinite Horizon LQ. Given continuous-time state equation. Find the control function u(t) to minimize
Infinite Horizon LQ Given continuous-time state equation x = Ax + Bu Find the control function ut) to minimize J = 1 " # [ x T t)qxt) + u T t)rut)] dt 2 0 Q $ 0, R > 0 and symmetric Solution is obtained
More informationA Tour of Reinforcement Learning The View from Continuous Control. Benjamin Recht University of California, Berkeley
A Tour of Reinforcement Learning The View from Continuous Control Benjamin Recht University of California, Berkeley trustable, scalable, predictable Control Theory! Reinforcement Learning is the study
More information16.31 Fall 2005 Lecture Presentation Mon 31-Oct-05 ver 1.1
16.31 Fall 2005 Lecture Presentation Mon 31-Oct-05 ver 1.1 Charles P. Coleman October 31, 2005 1 / 40 : Controllability Tests Observability Tests LEARNING OUTCOMES: Perform controllability tests Perform
More informationRobust Multivariable Control
Lecture 2 Anders Helmersson anders.helmersson@liu.se ISY/Reglerteknik Linköpings universitet Today s topics Today s topics Norms Today s topics Norms Representation of dynamic systems Today s topics Norms
More informationControl Systems. Laplace domain analysis
Control Systems Laplace domain analysis L. Lanari outline introduce the Laplace unilateral transform define its properties show its advantages in turning ODEs to algebraic equations define an Input/Output
More informationTime-Invariant Linear Quadratic Regulators!
Time-Invariant Linear Quadratic Regulators Robert Stengel Optimal Control and Estimation MAE 546 Princeton University, 17 Asymptotic approach from time-varying to constant gains Elimination of cross weighting
More informationECE 301 Division 1 Final Exam Solutions, 12/12/2011, 3:20-5:20pm in PHYS 114.
ECE 301 Division 1 Final Exam Solutions, 12/12/2011, 3:20-5:20pm in PHYS 114. The exam for both sections of ECE 301 is conducted in the same room, but the problems are completely different. Your ID will
More informationSignals and Systems Spring 2004 Lecture #9
Signals and Systems Spring 2004 Lecture #9 (3/4/04). The convolution Property of the CTFT 2. Frequency Response and LTI Systems Revisited 3. Multiplication Property and Parseval s Relation 4. The DT Fourier
More informationCALIFORNIA INSTITUTE OF TECHNOLOGY Control and Dynamical Systems. CDS 110b
CALIFORNIA INSTITUTE OF TECHNOLOGY Control and Dynamical Systems CDS 110b R. M. Murray Kalman Filters 14 January 2007 Reading: This set of lectures provides a brief introduction to Kalman filtering, following
More informationIntroduction to Nonlinear Control Lecture # 4 Passivity
p. 1/6 Introduction to Nonlinear Control Lecture # 4 Passivity È p. 2/6 Memoryless Functions ¹ y È Ý Ù È È È È u (b) µ power inflow = uy Resistor is passive if uy 0 p. 3/6 y y y u u u (a) (b) (c) Passive
More informationECE504: Lecture 9. D. Richard Brown III. Worcester Polytechnic Institute. 04-Nov-2008
ECE504: Lecture 9 D. Richard Brown III Worcester Polytechnic Institute 04-Nov-2008 Worcester Polytechnic Institute D. Richard Brown III 04-Nov-2008 1 / 38 Lecture 9 Major Topics ECE504: Lecture 9 We are
More informationTRACKING AND DISTURBANCE REJECTION
TRACKING AND DISTURBANCE REJECTION Sadegh Bolouki Lecture slides for ECE 515 University of Illinois, Urbana-Champaign Fall 2016 S. Bolouki (UIUC) 1 / 13 General objective: The output to track a reference
More informationReview: control, feedback, etc. Today s topic: state-space models of systems; linearization
Plan of the Lecture Review: control, feedback, etc Today s topic: state-space models of systems; linearization Goal: a general framework that encompasses all examples of interest Once we have mastered
More informationLinear Quadratic Optimal Control Topics
Linear Quadratic Optimal Control Topics Finite time LQR problem for time varying systems Open loop solution via Lagrange multiplier Closed loop solution Dynamic programming (DP) principle Cost-to-go function
More informationNonlinear Control. Nonlinear Control Lecture # 6 Passivity and Input-Output Stability
Nonlinear Control Lecture # 6 Passivity and Input-Output Stability Passivity: Memoryless Functions y y y u u u (a) (b) (c) Passive Passive Not passive y = h(t,u), h [0, ] Vector case: y = h(t,u), h T =
More informationRobotics. Control Theory. Marc Toussaint U Stuttgart
Robotics Control Theory Topics in control theory, optimal control, HJB equation, infinite horizon case, Linear-Quadratic optimal control, Riccati equations (differential, algebraic, discrete-time), controllability,
More informationEE221A Linear System Theory Final Exam
EE221A Linear System Theory Final Exam Professor C. Tomlin Department of Electrical Engineering and Computer Sciences, UC Berkeley Fall 2016 12/16/16, 8-11am Your answers must be supported by analysis,
More informationHomework Solution # 3
ECSE 644 Optimal Control Feb, 4 Due: Feb 17, 4 (Tuesday) Homework Solution # 3 1 (5%) Consider the discrete nonlinear control system in Homework # For the optimal control and trajectory that you have found
More informationAdvanced Mechatronics Engineering
Advanced Mechatronics Engineering German University in Cairo 21 December, 2013 Outline Necessary conditions for optimal input Example Linear regulator problem Example Necessary conditions for optimal input
More informationRaktim Bhattacharya. . AERO 422: Active Controls for Aerospace Vehicles. Dynamic Response
.. AERO 422: Active Controls for Aerospace Vehicles Dynamic Response Raktim Bhattacharya Laboratory For Uncertainty Quantification Aerospace Engineering, Texas A&M University. . Previous Class...........
More informationQuadratic Stability of Dynamical Systems. Raktim Bhattacharya Aerospace Engineering, Texas A&M University
.. Quadratic Stability of Dynamical Systems Raktim Bhattacharya Aerospace Engineering, Texas A&M University Quadratic Lyapunov Functions Quadratic Stability Dynamical system is quadratically stable if
More informationMATH4406 (Control Theory) Unit 6: The Linear Quadratic Regulator (LQR) and Model Predictive Control (MPC) Prepared by Yoni Nazarathy, Artem
MATH4406 (Control Theory) Unit 6: The Linear Quadratic Regulator (LQR) and Model Predictive Control (MPC) Prepared by Yoni Nazarathy, Artem Pulemotov, September 12, 2012 Unit Outline Goal 1: Outline linear
More informationCONTROL DESIGN FOR SET POINT TRACKING
Chapter 5 CONTROL DESIGN FOR SET POINT TRACKING In this chapter, we extend the pole placement, observer-based output feedback design to solve tracking problems. By tracking we mean that the output is commanded
More informationLecture 13: Internal Model Principle and Repetitive Control
ME 233, UC Berkeley, Spring 2014 Xu Chen Lecture 13: Internal Model Principle and Repetitive Control Big picture review of integral control in PID design example: 0 Es) C s) Ds) + + P s) Y s) where P s)
More informationLinear Quadratic Zero-Sum Two-Person Differential Games Pierre Bernhard June 15, 2013
Linear Quadratic Zero-Sum Two-Person Differential Games Pierre Bernhard June 15, 2013 Abstract As in optimal control theory, linear quadratic (LQ) differential games (DG) can be solved, even in high dimension,
More informationEE363 Review Session 1: LQR, Controllability and Observability
EE363 Review Session : LQR, Controllability and Observability In this review session we ll work through a variation on LQR in which we add an input smoothness cost, in addition to the usual penalties on
More informationPower Systems Control Prof. Wonhee Kim. Modeling in the Frequency and Time Domains
Power Systems Control Prof. Wonhee Kim Modeling in the Frequency and Time Domains Laplace Transform Review - Laplace transform - Inverse Laplace transform 2 Laplace Transform Review 3 Laplace Transform
More informationME 132, Fall 2017, UC Berkeley, A. Packard 317. G 1 (s) = 3 s + 6, G 2(s) = s + 2
ME 132, Fall 2017, UC Berkeley, A. Packard 317 Be sure to check that all of your matrix manipulations have the correct dimensions, and that the concatenations have compatible dimensions (horizontal concatenations
More informationLecture 9: Discrete-Time Linear Quadratic Regulator Finite-Horizon Case
Lecture 9: Discrete-Time Linear Quadratic Regulator Finite-Horizon Case Dr. Burak Demirel Faculty of Electrical Engineering and Information Technology, University of Paderborn December 15, 2015 2 Previous
More informationLQR, Kalman Filter, and LQG. Postgraduate Course, M.Sc. Electrical Engineering Department College of Engineering University of Salahaddin
LQR, Kalman Filter, and LQG Postgraduate Course, M.Sc. Electrical Engineering Department College of Engineering University of Salahaddin May 2015 Linear Quadratic Regulator (LQR) Consider a linear system
More informationRandom signals II. ÚPGM FIT VUT Brno,
Random signals II. Jan Černocký ÚPGM FIT VUT Brno, cernocky@fit.vutbr.cz 1 Temporal estimate of autocorrelation coefficients for ergodic discrete-time random process. ˆR[k] = 1 N N 1 n=0 x[n]x[n + k],
More informationIn the presence of viscous damping, a more generalized form of the Lagrange s equation of motion can be written as
2 MODELING Once the control target is identified, which includes the state variable to be controlled (ex. speed, position, temperature, flow rate, etc), and once the system drives are identified (ex. force,
More informationECEN 420 LINEAR CONTROL SYSTEMS. Lecture 6 Mathematical Representation of Physical Systems II 1/67
1/67 ECEN 420 LINEAR CONTROL SYSTEMS Lecture 6 Mathematical Representation of Physical Systems II State Variable Models for Dynamic Systems u 1 u 2 u ṙ. Internal Variables x 1, x 2 x n y 1 y 2. y m Figure
More informationLinear Quadratic Regulator (LQR) Design II
Lecture 8 Linear Quadratic Regulator LQR) Design II Dr. Radhakant Padhi Asst. Professor Dept. of Aerospace Engineering Indian Institute of Science - Bangalore Outline Stability and Robustness properties
More informationDenis ARZELIER arzelier
COURSE ON LMI OPTIMIZATION WITH APPLICATIONS IN CONTROL PART II.2 LMIs IN SYSTEMS CONTROL STATE-SPACE METHODS PERFORMANCE ANALYSIS and SYNTHESIS Denis ARZELIER www.laas.fr/ arzelier arzelier@laas.fr 15
More informationHamilton-Jacobi-Bellman Equation Feb 25, 2008
Hamilton-Jacobi-Bellman Equation Feb 25, 2008 What is it? The Hamilton-Jacobi-Bellman (HJB) equation is the continuous-time analog to the discrete deterministic dynamic programming algorithm Discrete VS
More informationFirst-Order Low-Pass Filter!
Filters, Cost Functions, and Controller Structures! Robert Stengel! Optimal Control and Estimation MAE 546! Princeton University, 217!! Dynamic systems as low-pass filters!! Frequency response of dynamic
More informationGame Theory Extra Lecture 1 (BoB)
Game Theory 2014 Extra Lecture 1 (BoB) Differential games Tools from optimal control Dynamic programming Hamilton-Jacobi-Bellman-Isaacs equation Zerosum linear quadratic games and H control Baser/Olsder,
More informationObservability. Dynamic Systems. Lecture 2 Observability. Observability, continuous time: Observability, discrete time: = h (2) (x, u, u)
Observability Dynamic Systems Lecture 2 Observability Continuous time model: Discrete time model: ẋ(t) = f (x(t), u(t)), y(t) = h(x(t), u(t)) x(t + 1) = f (x(t), u(t)), y(t) = h(x(t)) Reglerteknik, ISY,
More informationControl Systems. Dynamic response in the time domain. L. Lanari
Control Systems Dynamic response in the time domain L. Lanari outline A diagonalizable - real eigenvalues (aperiodic natural modes) - complex conjugate eigenvalues (pseudoperiodic natural modes) - phase
More informationEE363 homework 2 solutions
EE363 Prof. S. Boyd EE363 homework 2 solutions. Derivative of matrix inverse. Suppose that X : R R n n, and that X(t is invertible. Show that ( d d dt X(t = X(t dt X(t X(t. Hint: differentiate X(tX(t =
More informationMassachusetts Institute of Technology. Department of Electrical Engineering and Computer Science : MULTIVARIABLE CONTROL SYSTEMS by A.
Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science 6.245: MULTIVARIABLE CONTROL SYSTEMS by A. Megretski Q-Parameterization 1 This lecture introduces the so-called
More informationLecture 4: Least Squares (LS) Estimation
ME 233, UC Berkeley, Spring 2014 Xu Chen Lecture 4: Least Squares (LS) Estimation Background and general solution Solution in the Gaussian case Properties Example Big picture general least squares estimation:
More informationLecture 8. Chapter 5: Input-Output Stability Chapter 6: Passivity Chapter 14: Passivity-Based Control. Eugenio Schuster.
Lecture 8 Chapter 5: Input-Output Stability Chapter 6: Passivity Chapter 14: Passivity-Based Control Eugenio Schuster schuster@lehigh.edu Mechanical Engineering and Mechanics Lehigh University Lecture
More informationEE C128 / ME C134 Fall 2014 HW 9 Solutions. HW 9 Solutions. 10(s + 3) s(s + 2)(s + 5) G(s) =
1. Pole Placement Given the following open-loop plant, HW 9 Solutions G(s) = 1(s + 3) s(s + 2)(s + 5) design the state-variable feedback controller u = Kx + r, where K = [k 1 k 2 k 3 ] is the feedback
More information9 Controller Discretization
9 Controller Discretization In most applications, a control system is implemented in a digital fashion on a computer. This implies that the measurements that are supplied to the control system must be
More information6.241 Dynamic Systems and Control
6.241 Dynamic Systems and Control Lecture 24: H2 Synthesis Emilio Frazzoli Aeronautics and Astronautics Massachusetts Institute of Technology May 4, 2011 E. Frazzoli (MIT) Lecture 24: H 2 Synthesis May
More informationEL 625 Lecture 10. Pole Placement and Observer Design. ẋ = Ax (1)
EL 625 Lecture 0 EL 625 Lecture 0 Pole Placement and Observer Design Pole Placement Consider the system ẋ Ax () The solution to this system is x(t) e At x(0) (2) If the eigenvalues of A all lie in the
More informationFormula Sheet for Optimal Control
Formula Sheet for Optimal Control Division of Optimization and Systems Theory Royal Institute of Technology 144 Stockholm, Sweden 23 December 1, 29 1 Dynamic Programming 11 Discrete Dynamic Programming
More informationIntro. Computer Control Systems: F8
Intro. Computer Control Systems: F8 Properties of state-space descriptions and feedback Dave Zachariah Dept. Information Technology, Div. Systems and Control 1 / 22 dave.zachariah@it.uu.se F7: Quiz! 2
More informationFull State Feedback for State Space Approach
Full State Feedback for State Space Approach State Space Equations Using Cramer s rule it can be shown that the characteristic equation of the system is : det[ si A] 0 Roots (for s) of the resulting polynomial
More informationRealization theory for systems biology
Realization theory for systems biology Mihály Petreczky CNRS Ecole Central Lille, France February 3, 2016 Outline Control theory and its role in biology. Realization problem: an abstract formulation. Realization
More informationLecture 4 Continuous time linear quadratic regulator
EE363 Winter 2008-09 Lecture 4 Continuous time linear quadratic regulator continuous-time LQR problem dynamic programming solution Hamiltonian system and two point boundary value problem infinite horizon
More informationTopic # Feedback Control
Topic #5 6.3 Feedback Control State-Space Systems Full-state Feedback Control How do we change the poles of the state-space system? Or,evenifwecanchangethepolelocations. Where do we put the poles? Linear
More informationRobust Control 2 Controllability, Observability & Transfer Functions
Robust Control 2 Controllability, Observability & Transfer Functions Harry G. Kwatny Department of Mechanical Engineering & Mechanics Drexel University /26/24 Outline Reachable Controllability Distinguishable
More information1 st Tutorial on EG4321/EG7040 Nonlinear Control
1 st Tutorial on EG4321/EG7040 Nonlinear Control Introduction to State-Space Concepts Dr Angeliki Lekka 1 1 Control Systems Research Group Department of Engineering, University of Leicester February 9,
More informationModeling and Analysis of Dynamic Systems
Modeling and Analysis of Dynamic Systems Dr. Guillaume Ducard Fall 2017 Institute for Dynamic Systems and Control ETH Zurich, Switzerland G. Ducard c 1 / 57 Outline 1 Lecture 13: Linear System - Stability
More informationLinear-Quadratic-Gaussian (LQG) Controllers and Kalman Filters
Linear-Quadratic-Gaussian (LQG) Controllers and Kalman Filters Emo Todorov Applied Mathematics and Computer Science & Engineering University of Washington Winter 204 Emo Todorov (UW) AMATH/CSE 579, Winter
More information1 / 21 Perturbation of system dynamics and the covariance completion problem Armin Zare Joint work with: Mihailo R. Jovanović Tryphon T. Georgiou 55th
1 / 21 Perturbation of system dynamics and the covariance completion problem Armin Zare Joint work with: Mihailo R. Jovanović Tryphon T. Georgiou 55th IEEE Conference on Decision and Control, Las Vegas,
More information21 Linear State-Space Representations
ME 132, Spring 25, UC Berkeley, A Packard 187 21 Linear State-Space Representations First, let s describe the most general type of dynamic system that we will consider/encounter in this class Systems may
More informationCDS 101/110a: Lecture 2.1 Dynamic Behavior
CDS 11/11a: Lecture.1 Dynamic Behavior Richard M. Murray 6 October 8 Goals: Learn to use phase portraits to visualize behavior of dynamical systems Understand different types of stability for an equilibrium
More informationLinear Matrix Inequality (LMI)
Linear Matrix Inequality (LMI) A linear matrix inequality is an expression of the form where F (x) F 0 + x 1 F 1 + + x m F m > 0 (1) x = (x 1,, x m ) R m, F 0,, F m are real symmetric matrices, and the
More informationComputer Problem 1: SIE Guidance, Navigation, and Control
Computer Problem 1: SIE 39 - Guidance, Navigation, and Control Roger Skjetne March 12, 23 1 Problem 1 (DSRV) We have the model: m Zẇ Z q ẇ Mẇ I y M q q + ẋ U cos θ + w sin θ ż U sin θ + w cos θ θ q Zw
More informationContents lecture 6 2(17) Automatic Control III. Summary of lecture 5 (I/III) 3(17) Summary of lecture 5 (II/III) 4(17) H 2, H synthesis pros and cons:
Contents lecture 6 (7) Automatic Control III Lecture 6 Linearization and phase portraits. Summary of lecture 5 Thomas Schön Division of Systems and Control Department of Information Technology Uppsala
More informationSDS 321: Introduction to Probability and Statistics
SDS 321: Introduction to Probability and Statistics Lecture 14: Continuous random variables Purnamrita Sarkar Department of Statistics and Data Science The University of Texas at Austin www.cs.cmu.edu/
More informationTopic # Feedback Control Systems
Topic #20 16.31 Feedback Control Systems Closed-loop system analysis Bounded Gain Theorem Robust Stability Fall 2007 16.31 20 1 SISO Performance Objectives Basic setup: d i d o r u y G c (s) G(s) n control
More informationLet x(t) be a finite energy signal with Fourier transform X(jω). Let E denote the energy of the signal. Thus E <. We have.
Notes on the Uncertainty principle Let x(t) be a finite energy signal with Fourier transform X(jω). Let E denote the energy of the signal. Thus E
More information