Alternative Derivation of Linear Quadratic Regulator

نویسنده

  • Jerry Ding
چکیده

The purpose of this short note is to provide an alternative derivation of the optimal controller for the linear quadratic optimization problem in Section 2. Consider the linear time-varying system dynamics ˙ x(t) = A(t)x(t) + B(t)u(t), x(t 0) = x 0 , (1) where x(t) ∈ R n , u(t) ∈ R n i , ∀t ∈ [t 0 ,t 1 ]. Define the quadratic cost function J(u) = 1 2 t 1 t 0 u(t) 2 2 + C(t)x(t) 2 2 dt + x(t 1) T Sx(t 1) , (2) where S is a symmetric, positive semi-definite matrix. We are interested in the linear quadratic optimization problem J * := min u∈PC J(u), subject to (1), (3) where we denote by PC the set of piecewise continuous functions on [t 0 ,t 1 ]. The more familiar form of this problem is the linear quadratic regulation (LQR) problem, with both penalties on the state and the control. Specifically, consider a modified cost function ˜ J(u) = 1 2 t 1 t 0 x(t) T Q(t)x(t) + u(t) T R(t)u(t)dt + x(t 1) T Sx(t 1) , (4) where Q(t), R(t) are symmetric matrices, with Q(t) positive semi-definite and R(t) positive definite. The LQR problem is then given by ˜ J * := min u∈PC˜J(u), subject to (1). With appropriate choices of weighting matrices, problems (3) and (5) are in fact equivalent. In particular, let R 1/2 , Q 1/2 be the square root of the matrices R, Q. Consider the pseudo-input˜u = R 1/2 u. Then the system dynamics (1) can be rewritten as ˙ x(t) = A(t)x(t) + B(t)R −1/2 (t) ˜ u(t), x(t 0) = x 0 ,

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Enhancement of Articulated Heavy Vehicle Stability by Optimal Linear Quadratic Regulator (LQR) Controller of Roll-yaw Dynamics

Non-linear characteristic of tire forces is the main cause of vehicle lateral dynamics instability, while direct yaw moment control is an effective method to recover the vehicle stability. In this paper, an optimal linear quadratic regulator (LQR) controller for roll-yaw dynamics to articulated heavy vehicles is developed. For this purpose, the equations of motion obtained by the MATLAB sof...

متن کامل

Mathematical Model and Vibration Analysis of Aircraft with Active Landing Gear System using Linear Quadratic Regulator Technique

This paper deals with the study and comparison of passive and active landing gear system of  the aircraft and dynamic responses due to runway irregularities while the aircraft is taxying. The dynamic load and vibration caused by the unevenness of runway will result in airframe fatigue, discomfort of passengers and the reduction of the pilot’s ability to control the aircraft. One of the objectiv...

متن کامل

Control System Design for a Surface Effect Ship by Linear-Quadratic Regulator Method

In this paper, the main goal is to reduce the heave motion between a surface effect ship (SES) and a wind turbine in order to safely transfer equipment and person to SES. For this purpose, an LQR control system is designed to damp the vertical motion of the surface effect ship in critical sea states including high-frequency and high amplitude regular waves as well as high frequency irregular wa...

متن کامل

Active vibration control of smart building frames by feedback controllers

In this paper the active vibration control of a four-story shear frame instrumented with piezoelectric actuators is presented. The piezoelectric actuators are hosted on the columns in two manners and the produced controlling forces by actuators are considered in the equation of motion. The smart structure modeling and control design is carried out using MATLAB software in state space form. Subs...

متن کامل

AN OPTIMAL FUZZY SLIDING MODE CONTROLLER DESIGN BASED ON PARTICLE SWARM OPTIMIZATION AND USING SCALAR SIGN FUNCTION

This paper addresses the problems caused by an inappropriate selection of sliding surface parameters in fuzzy sliding mode controllers via an optimization approach. In particular, the proposed method employs the parallel distributed compensator scheme to design the state feedback based control law. The controller gains are determined in offline mode via a linear quadratic regular. The particle ...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2012