A Wavelet Collocation Method for Optimal Control. Problems

Size: px
Start display at page:

Download "A Wavelet Collocation Method for Optimal Control. Problems"

Transcription

1 A Wavelet ollocation ethod or Optimal ontrol Problems Ran Dai * and John E. ochran Jr. Abstract A Haar wavelet technique is discussed as a method or discretizing the nonlinear sstem equations or optimal control problems. he technique is used to transorm the state and control variables into nonlinear programming NLP parameters at collocation points. A nonlinear programming solver can than be used to solve optimal control problems that are rather general in orm. Here general Bolza optimal control problems with state and control constraints are considered. Eamples o two inds o optimal control problems continuous and discrete are solved. he results are compared to those obtained b using other collocation methods. Kewords Haar Wavelet ollocation Discrete Optimal ontrol Nonlinear Programming * Ran Dai Department o Aerospace Engineering Auburn Universit Auburn AL aviator_dai@hotmail.com John E. ochran Jr. Department o Aerospace Engineering Auburn Universit Auburn AL jcochran@eng.auburn.edu.

2 Introduction Recentl wavelet theor has attracted considerable attention due to the advantages wavelets have over traditional Fourier transorms in accuratel approimating unctions that have discontinuities and sharp peas. Wavelets have been applied in signal processing multi-scale phenomena modeling and pattern recognition. he Haar wavelet unction was introduced b Alred Haar in 9 in the orm o a regular pulse pair []. Ater that man other wavelet unctions were generated and introduced. hose include the Shannon Daubechies and Legendre wavelets. Among those orms Haar wavelets have the simplest orthonormal series with compact support. hese characteristics maes Haar wavelets good candidates or application to optimal control problems. he wavelet applications in dealing with dnamic sstem problems especiall in solving partial dierential equations with two-point boundar value constraints have been discussed in man papers [-5]. B transorming dierential equations into algebraic equations the solution ma be ound b determining the corresponding coeicients that satis the algebraic equations. Some eorts have been made to solve linear optimal control problems b using wavelet collocation [6-9]. But when the sstem equations become comple and highl nonlinear it is necessar to see some useul tools to solve those inds o problems. he nonlinear programming solver NLPS SNOP [ ] which uses a Sequential Quadratic Programming algorithm to solve the nonlinear problems seems to be an eicient tool or this tas. At each major iteration o the NLPS algorithm the solver inds the search direction or the current nominall optimized points. his process is repeated until convergence occurs. hen the parameterized objective unction can be optimized with sstem equation constraints satisied.

3 he collocation methods developed to solve nonlinear optimal control problems generall all into two categories local collocation[3] and global orthogonal collocation [4-7]. In local collocation methods such as trapezoidal Hermite-Simpson and Runge-Kutta methods the time interval considered is divided into a series o subintervals within which the integration rule must be satisied. hese local collocation methods were introduced in direct collocation and nonlinear programming DNLP and have wide application [8-]. In recent ears more attention has been ocused on global orthogonal collocation methods such as Legendre hebshev Gauss method and some others. B epanding the state and control variables into piecewise-continuous polnomials the derivative o the state variables can be approimated b combinations o these interpolating polnomials and their derivatives. hen the objective unction and sstem constraints are all converted into algebraic equations with unnown coeicients. he orthogonal collocation methods are generall better than local collocation methods in achieving ast convergence rate and high accurac. here are three major classes o orthogonal unctions the orthogonal polnomials lie Legendre hebshev etc. the sine-cosine unctions in Fourier series and the constant basis unction lie Haar bloc-pulse etc.. he irst two classes o orthogonal unctions have been widel applied in collocation as mentioned above. But apparentl no attempts have been made to appl constant basis orthogonal unctions in collocation. hus it is o interest to see how this new collocation method wors. In this paper we irst introduce the Haar wavelets theor and properties including the Haar wavelets basis and its integral operational matri. hen we will assume that the control variables and derivatives o the state variables in the optimal control problems ma be epressed in the orm o Haar wavelets and unnown coeicients. he state 3

4 variables can be calculated b using the Haar operational integration matri. hereore all variables in the nonlinear sstem equations are epressed as series o the Haar amil and its operational matri. Finall the tas o inding the unnown parameters that optimize the designate perormance while satising all constraints is perormed b the NLPS. o demonstrate the applicabilit o this new collocation method we consider two eample optimal control problems one with a smooth control and one with a non-smooth control. Haar Wavelets. Haar Functions he basic and simplest orm o Haar wavelet is the Haar scaling unction that appears in the orm o a square wave over the interval t [ as epressed in Eq. and illustrated in the irst subplot o Fig. : t < φ t elsewhere he above epression called Haar ather wavelet is the zeroth level wavelet which has no displacement and dilation o unit magnitude. orrespondingl there is a Haar mother wavelet to match the ather wavelet which is described as φ t t < t < elsewhere 4

5 he Haar mother wavelet is the irst level Haar wavelet and its graph is given in the second subplot o Fig.. his mother wavelet can also be written as the linear combination o the Haar scaling unction with translation and compression to hal o its original interval φ t φt φt 3 Similarl the other levels o wavelets can all be generated rom φ b the operations o translation and t compression. For eample the third subplot in Fig. is ormed b compression φ to let hal o its original t interval and the orth subplot is the same as the third one plus translating to the right side b /. In general we can write out the Haar wavelet amil as φi t +.5 t [ m m t [ m m elsewhere 4 here m is the level o the wavelet assume the maimum level resolution is integer J then m equals to j j K J ; the translation parameter K m. he series inde number i is deined b m and and i m +. For an ied level m there are m series o φ i to ill the interval [ corresponding to that level and or a provided J the inde number i can reach the maimum value J + when including 5

6 all levels o wavelets. Each Haar wavelet is composed o a couple o constant steps o opposite sign during its subinterval and is zero elsewhere. hereore the have the ollowing relationship j φi t φl t dt i l i l j + 5 his relationship shows that Haar wavelets are orthogonal to each other and thereore constitute an orthogonal basis. his allows us to transorm an unction square integrable on the interval time [ into Haar wavelets series.. Function Approimation b Haar Wavelets We just pointed out that a square integrable unction can be epressed in terms o Haar orthogonal basis on interval [. However beore the procession to this transer it is necessar to uni the time interval. B using a linear transormation the actual time t can be epressed as a unction o via t [ t t + t ] 6 where t is the initial time and t is the inal time in a square integrable unction t. he objective is to write this t in orm o wavelet epansion series with coeicients that is t a φ t i i i A Ψ t 7 6

7 where the coeicient vector A ] [ a a K a and Ψ t [ φ t φ t K φ t]. In vector A each coeicient ai is determined b j ai t φi t dt 8 and it is epected to approimate unction t with minimum mean integral square error ε deined as ε t A Ψ t dt 9 Obviousl ε should reduce when the level gets larger and it should go close to zero when approaches ininite. I we set all the collocation pic point t s at the middles o each wavelet then t s is deined as t s s.5 / where s K. With these chosen collocation points the unction is discretized into a series o nodes with equivalent distances. he vector Ψ t can also be determined at those collocation points. Let the Haar matri H be the combination o Ψ t at all the collocation points. hus we get H [ Ψ t Ψ t K Ψ t ] φ t φ t φ t φ t φ t φ t L L O K φ t φ t φ t 7

8 or eample [ Ψ t Ψ ] H t and [ Ψ t Ψ t Ψ t Ψ ] H t 3 3 hereore unction t is approimated as ts H..3 Haar Operational Integration atri In the solution o optimal control problems we alwas need to deal with equations involving dierentiation and integration. I the sstem unction is epressed in Haar wavelets the integration or dierentiation operation o Haar series cannot be avoided. he dierentiation o step waves will generate pulse signals which are diicult to handle while the integration o step waves will result in constant slope unctions which can be calculated b the ollowing equation ' ' Ψ t dt PΨ t 4 where P is the operational integration matri and is given b Gu and Jiang [] or how to calculate this matri 8

9 P P H / / H / P [ ] 5 3 Formulation o Optimal ontrol Problems he objective o an optimal control problem is to ind the histor o the control variables that will maimize or minimize a given perormance inde while satising the sstem constraints. he sstem constraints include irstorder ordinar dierential equations subject to initial and inal boundar conditions and some additional constraints on the states and controls. he dierential equations are written here as & tu 6 where is an n vector o states is an n vector o continuous dierential unctions t is the time and u is an m vector o controls. he states are subject to prescribed initial conditions and inal boundar conditions ψ t where ψ is a p vector o unctions t is the initial time and the terminal time t mabe ied or ree. Some problems also include etra path constraints which are unctions o state and control variables ormulated as g tu 7 9

10 where g is a q vector. In this paper we consider problems o the Bolza [] tpe which are ocused and minimizing the scalar perormance inde o the orm J φ t t + t L t u dt 8 where φ is a scalar unction o the inal time t and inal state variables and L t u is a scalar unction o the time state and control u. 4 Direct ollocation and Nonlinear Programming 4. Haar Discretization ethod In the discussion o Haar wavelets we have alread addressed how to approimate a unction in Haar wavelets and its corresponding operational integration matri. We are epecting to appl this methodolog in optimal control problems so that Haar discretization is used in direct collocation. hus the continuous solution to a problem will be represented b state and control variables in terms o Haar series and its operational matri to satis the dierential equations. he standard interval considered here is denoted as [ with collocation points set as.5 / K 9 where is the number o nodes used in discretization and also is the maimum wavelet inde number. Note that the magnitude o is in the power o so that the number o collocation points is also increasing in that power.

11 All the collocation points are equall distributed over the entire time interval [ with as the time distance to adjacent nodes. We assume that the derivative o the state variables & and control variables u can be approimated b Haar wavelets with collocation points i.e. & Ψ u Ψ u where [ K ] u [ K u u u ] B using the operational integration matri P deined in Eq. 5 the state variables can be epressed as & ' d ' + Ψ ' d ' + PΨ + 3 As stated in Eq. the epansion o the matri Ψ at the collocation points will ield the Haar matri H h h K h ]. It ollows that [ & h u h Ph u K 4

12 From the above epression we can evaluate the variables at an collocation point b using the product o its coeicients vector and the corresponding column vector in the Haar matri. 4. NLP Solver: SNOP 6. he NLPS used to solve the NLP problem considered in this wor is based on a Sequential Quadrature Programming SQP algorithm and is called SNOP. SNOP can be used to solve problems lie the ollowing: inimize a perormance inde J subject to constraints on individual state and/or control variables L U 5 constraints deined b linear combinations o state and/or control variables: b A L b U 6 and/or constraints deined b nonlinear unctions o state and/or control variables: c c L c U 7 When the Haar collocation method is applied in the optimal control problems the NLP variables can be set as the unnown coeicients vector o the derivative o the state variables and control variables together with initial and inal times that is [ K u u K u t t ] 8

13 3 he objective unction in Eq. 8 is then restated as φ d P L t t t J u Ψ + Ψ + 9 Since the Haar wavelets are epected to be constant steps at each time interval the above equation can be simpliied as Ψ + Ψ + u P L t t t J φ 3 with path constraints ormulated as Ψ + Ψ u P g 3 Substituting & u and in Eq. 6 with the Haar wavelets epression o Eq. 4 separatel ields: u P t t Ψ + Ψ Ψ 3 he sstem equation constraints and path constraints are all treated as nonlinear constraints in NLP solver. he boundar constraints need to be paid more attention. Since the irst and last collocation points are not set as the initial and inal time the initial and inal state variables are calculated according to / / & & + 33

14 In this wa the optimal control problems are transormed into NLP problems in a structured orm. 5 Eamples In this section we consider two optimal control problems that have nown solution and see how well the results o the NLP with direct collocation can approimate eact solution. 5. Brachistochrone Problem he Brachistochrone Problem is that o inding the shape o the curve down which a weight classicall a bead acted upon b the orce o gravit will descend rom rest and accelerate to a desired point in the least time assuming there is no riction and the ground orce is uniorm. athematicall this problem is described as inding the minimum time t or a bead rom the starting point [ ] to the inal point [ ] while satising the sstem equation constraints & & g g cosu sin u 34 where angle u is the slope o the curve and is treated as control variable o this problem. Using the Haar wavelets collocation method with collocation points the objective is to minimize J t with sstem equation constraints h h t t g g Ph Ph + cos h + sin h u u K 35 4

15 and boundar constraints Ph + Ph + h / h / Ph + Ph + h / h / 36 where u and t are all NLP variables solved at the collocation points. he analtical solution or this problem is epressed as a ccloid generated b a circle o diameter R that rolls through angle θ rom the vertical and described mathematicall b θ R θ sinθ θ R cosθ 37 he analtical optimal control epressed in terms o time is t π u t g / R 38 For the numerical solution we assume the starting point is [ ] and the ending point is [ 5] use 6 and 3 collocation points separatel or the Haar wavelets discretization method. he initial guess o the solution is the straight line connecting the starting and ending points. hereore the initial control and NLP variables are estimated according to this coarse initial guess. he trajector and control histor results using this new method is shown in Fig. and 3 separatel and compared to the analtical results. Also there are results o using the hebshev Pseudospectral P collocation method to solve the same problem with the same number o collocation points. 5

16 From Fig and 3 it can be seen that the results generated b the Haar wavelets collocation method made good approimation to the analtical solution. When the number o collocation points increases the accurac is improved and urther increase will mae the inal trajector converge to the eact solution. he absolute error o the objective unction between wavelet solution J and analtical solution * J with respect to the number o nodes is shown in Fig Discrete Optimal ontrol Problem he discrete optimal control problem considered here is to use Bang-Bang ontrol with maimum and minimum bounds to minimize the cost unction J t 39 subject to simple sstem equation constraints & & u 4 and initial state variable constraints t t 3 4 where u is the control and is constrained so that u t. he analtical solution or this problem is [6] 6

17 t / + t + t t / t t + t / t + t < t t t t t > t t < t u t t > t t < t t > t 4 where the switching time is calculated at t and the optimized inal time t. t For the DNLP solutions we assume that the trajector starts rom [ 3] and ends at ] [ again use 6 and 3 nodes in Haar wavelets collocation and the initial guess o the state variables are straight line connecting the starting and inal points. hen the results to analtical and P methods are compared in Fig. 4 or state variables and Fig. 5 or controls. It s obvious to see that Haar wavelet collocation has an advantage in Bang-Bang optimal control problems when the switching time is unnown. Instead o the slope solution with long and unstead time interval beore and ater the switching point in P method the wavelet solution provides Bang-Bang control wave which switch values ver close to the eact analtical switching time. he convergence rate or the wavelet solution is shown in Fig. 7. When the number o nodes increases it is epected the wavelet solution will generate the optimal control solution with error close to zero. Besides the state variables o the wavelet converge to the analtical solution. 7

18 6 onclusion A new collocation method is applied to solve two well nown optimal control problems using a nonlinear programming solver. he sstem equations are all epressed in Haar wavelets with unnown coeicients and solving those unnown coeicients while optimizing the perormance inde becomes the tas o this ind o parameterized problems. his new method produces results similar to other collocation methods or the continuous optimal control problem and shows advantages in discrete optimal control problems when switching time is unnown. Reerences. Boggess A. and Narcowich F. J. A First ourse in Wavelets with Fourier Analsis Prentice-Hall Inc... Bertoluzza S. and Naldi G. A Wavelet ollocation ethod or the Numerical Solution o Partial Dierential Equations Applied and omputational Harmonic Analsis 3 No pp Lepi U. Numerical Solution o Dierential Equations Using Haar Wavelets athematics and omputers in Simulation No. 68 pp Belin G. On Wavelet-Based Algorithms or Solving Dierential Equations in Wavelets: athematics and Applications R Press 994 pp Xu J.. and Shann W.. Galerin-Wavelet ethods or wo-point Boundar Value Problems Numerical athematic Vol. 63 pp hen. F. and Hsiao. H. Wavelet Approach to Optimizing Dnamic Sstems IEE Proc.-ontrol heor Appl. Vol. 46 No. pp. 3-9 arch

19 7. Karimi H. R. aralani P. J. oshiri B. and Lohmann B. Haar Wavelet-Based ontrol o ime-varing State-Delaed Sstems: A omputational ethod International Journal o omputer athematics Razzaghi. and Yousei S. Legendre Wavelets ethod or onstrained Optimal ontrol Problems athematical ethod in he Applied Sciences 5 pp Hsiao. H. and Wang J. W. Optimal ontrol o Linear ime-varing Sstems via Haar Wavelets Journal o Optimization heor and Application Vol. 3 No. 3 pp Holmstrom K. Goran A.O. and Edvall. User s Guide or OLAB /SNOP omlab Optimization Inc. 5 Gano S. E. Perez V.. and Renaud J. E. Development and Veriication o A ALAB Driver For he SNOP Optimization Sotware AIAA Paper -6.. Hargraves. R. and Paris S. W. Direct rajector Optimization Using Nonlinear Programming and ollocation J. o Guidance ontrol and Dnamics Vol. No. 4 pp Jul- August Betts J.. and Human W. P. Path-onstrained rajector Optimization Using Sparse Sequential Quadratic Programming Journal o Guidance ontrol and Dnamics Vol. 6 No. pp Fahroo. and Ross I.. Direct rajector Optimization b a hebshev Pseudospectral ethod Journal o Guidance ontrol and Dnamics Vol. 5 No. pp Pietz J. A. Pseudospectral ollocation ethods or the Direct ranscription o Optimal ontrol Problems.A. hesis Dept. o omputational and Applied athematics Rice Universit Houston X Benson D. A Gauss Pseudospectral ranscription or Optimal ontrol Ph.D. hesis Department o Aeronautics and Astronautics I Nov. 4. 9

20 7. Huntington G.. Benson D. A. and Rao A. V. A comparison o Accurac and omputational Eicienc o hree Pseudospectral ethods in Proc. o the AIAA Guidance Navigation and ontrol onerence Hilton Head S August Horie K. and onwa B. A. Optimal Aeroassisted Orbital Interception Journal o Guidance ontrol and Dnamics Vol. No. 5 pp Geiger B. R. Horn J. F. DeLullo A.. AND Long L. N. Optimal Path Planning o UAVs Using Direct ollocation with Nonlinear Programming AIAA Guidance Navigation and ontrol onerence and Ehibit Kestone olorado AIAA Herman A. L. and Spencer D. B. Optimal Low-hrust Earth-Orbit ransers Using Higher-Order ollocation ethods Journal o Guidance ontrol and Dnamics Vol. 5 No. pp Gu J. S and Jiang W. S he Haar wavelets operational matri o integration international Journal o Sstems Science vol.7 no. 7 pp Brson. A.E. and Ho Y.. Applied Optimal ontrol Optimization Estimation and ontrol Hemisphere publishing corporation 975. List o Figures Fig. Graph o Haar Function. Fig. rajector or Brachistochrone Problem Fig. 3 ime Histor o ontrol or Brachistochrone Problem Fig. 4 Objective Function Error or Brachistochrone Problem

21 Fig. 5 ime Histor o States or Bang-Bang Problem Fig. 6 ime Histor o ontrol or Bang-Bang Problem Fig. 7 Objective Function Error or Bang-Bang Problem Fig. Graph o Haar Function.

22 Fig. rajector or Brachistochrone Problem - - analtical solution wavelet with 3 nodes wavelet with 6 nodes cp with 6 nodes

23 Fig. 3 ime Histor o ontrol or Brachistochrone Problem control u rad analtical solution wavelet with 3 nodes wavelet with 6 nodes cp with 6 nodes time sec 3

24 Fig. 4 Objective Function Error or Brachistochrone Problem..8 J-J * Number o Nodes 4

25 Fig. 5 ime Histor o States or Bang-Bang Problem and analtical solution wavelet with 3 nodes wavelet with 6 nodes cp with 6 nodes time sec 5

26 Fig. 6 ime Histor o ontrol or Bang-Bang Problem.5 analtical solution wavelet with 6 nodes wavelet with 3 nodes P with 6 nodes control u time sec 6

27 Fig. 7 Objective Function Error or Bang-Bang Problem J-J * Number o Nodes 7

Three-Dimensional Trajectory Optimization in Constrained Airspace

Three-Dimensional Trajectory Optimization in Constrained Airspace Three-Dimensional Traectory Optimization in Constrained Airspace Ran Dai * and John E. Cochran, Jr. Auburn University, Auburn, Alabama 36849 The operational airspace o aerospace vehicles, including airplanes

More information

A NOVEL METHOD OF INTERPOLATION AND EXTRAPOLATION OF FUNCTIONS BY A LINEAR INITIAL VALUE PROBLEM

A NOVEL METHOD OF INTERPOLATION AND EXTRAPOLATION OF FUNCTIONS BY A LINEAR INITIAL VALUE PROBLEM A OVEL METHOD OF ITERPOLATIO AD EXTRAPOLATIO OF FUCTIOS BY A LIEAR IITIAL VALUE PROBLEM Michael Shatalov Sensor Science and Technolog o CSIR Manuacturing and Materials, P.O.Bo 395, Pretoria, CSIR and Department

More information

Feedback Optimal Control for Inverted Pendulum Problem by Using the Generating Function Technique

Feedback Optimal Control for Inverted Pendulum Problem by Using the Generating Function Technique (IJACSA) International Journal o Advanced Computer Science Applications Vol. 5 No. 11 14 Feedback Optimal Control or Inverted Pendulum Problem b Using the Generating Function echnique Han R. Dwidar Astronom

More information

. This is the Basic Chain Rule. x dt y dt z dt Chain Rule in this context.

. This is the Basic Chain Rule. x dt y dt z dt Chain Rule in this context. Math 18.0A Gradients, Chain Rule, Implicit Dierentiation, igher Order Derivatives These notes ocus on our things: (a) the application o gradients to ind normal vectors to curves suraces; (b) the generaliation

More information

Increasing and Decreasing Functions and the First Derivative Test. Increasing and Decreasing Functions. Video

Increasing and Decreasing Functions and the First Derivative Test. Increasing and Decreasing Functions. Video SECTION and Decreasing Functions and the First Derivative Test 79 Section and Decreasing Functions and the First Derivative Test Determine intervals on which a unction is increasing or decreasing Appl

More information

9.1 The Square Root Function

9.1 The Square Root Function Section 9.1 The Square Root Function 869 9.1 The Square Root Function In this section we turn our attention to the square root unction, the unction deined b the equation () =. (1) We begin the section

More information

Implicit Second Derivative Hybrid Linear Multistep Method with Nested Predictors for Ordinary Differential Equations

Implicit Second Derivative Hybrid Linear Multistep Method with Nested Predictors for Ordinary Differential Equations American Scientiic Research Journal or Engineering, Technolog, and Sciences (ASRJETS) ISSN (Print) -44, ISSN (Online) -44 Global Societ o Scientiic Research and Researchers http://asretsournal.org/ Implicit

More information

Solutions for Homework #8. Landing gear

Solutions for Homework #8. Landing gear Solutions or Homewor #8 PROBEM. (P. 9 on page 78 in the note) An airplane is modeled as a beam with masses as shown below: m m m m π [rad/sec] anding gear m m.5 Find the stiness and mass matrices. Find

More information

AP Calculus AB Summer Assignment

AP Calculus AB Summer Assignment AP Calculus AB Summer Assignment As Advanced placement students, our irst assignment or the 07-08 school ear is to come to class the ver irst da in top mathematical orm. Calculus is a world o change. While

More information

New Functions from Old Functions

New Functions from Old Functions .3 New Functions rom Old Functions In this section we start with the basic unctions we discussed in Section. and obtain new unctions b shiting, stretching, and relecting their graphs. We also show how

More information

3. Several Random Variables

3. Several Random Variables . Several Random Variables. Two Random Variables. Conditional Probabilit--Revisited. Statistical Independence.4 Correlation between Random Variables. Densit unction o the Sum o Two Random Variables. Probabilit

More information

CISE-301: Numerical Methods Topic 1:

CISE-301: Numerical Methods Topic 1: CISE-3: Numerical Methods Topic : Introduction to Numerical Methods and Taylor Series Lectures -4: KFUPM Term 9 Section 8 CISE3_Topic KFUPM - T9 - Section 8 Lecture Introduction to Numerical Methods What

More information

TFY4102 Exam Fall 2015

TFY4102 Exam Fall 2015 FY40 Eam Fall 05 Short answer (4 points each) ) Bernoulli's equation relating luid low and pressure is based on a) conservation o momentum b) conservation o energy c) conservation o mass along the low

More information

The Ascent Trajectory Optimization of Two-Stage-To-Orbit Aerospace Plane Based on Pseudospectral Method

The Ascent Trajectory Optimization of Two-Stage-To-Orbit Aerospace Plane Based on Pseudospectral Method Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 00 (014) 000 000 www.elsevier.com/locate/procedia APISAT014, 014 Asia-Paciic International Symposium on Aerospace Technology,

More information

Syllabus Objective: 2.9 The student will sketch the graph of a polynomial, radical, or rational function.

Syllabus Objective: 2.9 The student will sketch the graph of a polynomial, radical, or rational function. Precalculus Notes: Unit Polynomial Functions Syllabus Objective:.9 The student will sketch the graph o a polynomial, radical, or rational unction. Polynomial Function: a unction that can be written in

More information

SIO 211B, Rudnick. We start with a definition of the Fourier transform! ĝ f of a time series! ( )

SIO 211B, Rudnick. We start with a definition of the Fourier transform! ĝ f of a time series! ( ) SIO B, Rudnick! XVIII.Wavelets The goal o a wavelet transorm is a description o a time series that is both requency and time selective. The wavelet transorm can be contrasted with the well-known and very

More information

Nonlinear Integro-differential Equations by Differential Transform Method with Adomian Polynomials

Nonlinear Integro-differential Equations by Differential Transform Method with Adomian Polynomials Math Sci Lett No - Mathematical Science Letters An International Journal http://ddoior//msl/ Nonlinear Intero-dierential Equations b Dierential Transorm Method with Adomian Polnomials S H Behir General

More information

Numerical Methods - Lecture 2. Numerical Methods. Lecture 2. Analysis of errors in numerical methods

Numerical Methods - Lecture 2. Numerical Methods. Lecture 2. Analysis of errors in numerical methods Numerical Methods - Lecture 1 Numerical Methods Lecture. Analysis o errors in numerical methods Numerical Methods - Lecture Why represent numbers in loating point ormat? Eample 1. How a number 56.78 can

More information

Initial Value Problems for. Ordinary Differential Equations

Initial Value Problems for. Ordinary Differential Equations Initial Value Problems for Ordinar Differential Equations INTRODUCTION Equations which are composed of an unnown function and its derivatives are called differential equations. It becomes an initial value

More information

Minimum-Time Trajectory Optimization of Multiple Revolution Low-Thrust Earth-Orbit Transfers

Minimum-Time Trajectory Optimization of Multiple Revolution Low-Thrust Earth-Orbit Transfers Minimum-Time Trajectory Optimization o Multiple Revolution Low-Thrust Earth-Orbit Transers Kathryn F. Graham Anil V. Rao University o Florida Gainesville, FL 32611-625 Abstract The problem o determining

More information

Physics 5153 Classical Mechanics. Solution by Quadrature-1

Physics 5153 Classical Mechanics. Solution by Quadrature-1 October 14, 003 11:47:49 1 Introduction Physics 5153 Classical Mechanics Solution by Quadrature In the previous lectures, we have reduced the number o eective degrees o reedom that are needed to solve

More information

Mathematical Preliminaries. Developed for the Members of Azera Global By: Joseph D. Fournier B.Sc.E.E., M.Sc.E.E.

Mathematical Preliminaries. Developed for the Members of Azera Global By: Joseph D. Fournier B.Sc.E.E., M.Sc.E.E. Mathematical Preliminaries Developed or the Members o Azera Global B: Joseph D. Fournier B.Sc.E.E., M.Sc.E.E. Outline Chapter One, Sets: Slides: 3-27 Chapter Two, Introduction to unctions: Slides: 28-36

More information

Received: 30 July 2017; Accepted: 29 September 2017; Published: 8 October 2017

Received: 30 July 2017; Accepted: 29 September 2017; Published: 8 October 2017 mathematics Article Least-Squares Solution o Linear Dierential Equations Daniele Mortari ID Aerospace Engineering, Texas A&M University, College Station, TX 77843, USA; mortari@tamu.edu; Tel.: +1-979-845-734

More information

Shai Avidan Tel Aviv University

Shai Avidan Tel Aviv University Image Editing in the Gradient Domain Shai Avidan Tel Aviv Universit Slide Credits (partial list) Rick Szeliski Steve Seitz Alosha Eros Yacov Hel-Or Marc Levo Bill Freeman Fredo Durand Slvain Paris Image

More information

18-660: Numerical Methods for Engineering Design and Optimization

18-660: Numerical Methods for Engineering Design and Optimization 8-66: Numerical Methods or Engineering Design and Optimization Xin Li Department o ECE Carnegie Mellon University Pittsburgh, PA 53 Slide Overview Linear Regression Ordinary least-squares regression Minima

More information

Estimation of the Vehicle Sideslip Angle by Means of the State Dependent Riccati Equation Technique

Estimation of the Vehicle Sideslip Angle by Means of the State Dependent Riccati Equation Technique Proceedings o the World Congress on Engineering 7 Vol II WCE 7, Jul 5-7, 7, London, U.K. Estimation o the Vehicle Sideslip Angle b Means o the State Dependent Riccati Equation Technique S. Strano, M. Terzo

More information

PRECISION ZEM/ZEV FEEDBACK GUIDANCE ALGORITHM UTILIZING VINTI S ANALYTIC SOLUTION OF PERTURBED KEPLER PROBLEM

PRECISION ZEM/ZEV FEEDBACK GUIDANCE ALGORITHM UTILIZING VINTI S ANALYTIC SOLUTION OF PERTURBED KEPLER PROBLEM AAS 16-345 PRECISION ZEM/ZEV FEEDBACK GUIDANCE ALGORITHM UTILIZING VINTI S ANALYTIC SOLUTION OF PERTURBED KEPLER PROBLEM Jaemyung Ahn, * Yanning Guo, and Bong Wie A new implementation o a zero-eort-miss/zero-eort-velocity

More information

THE CONVERGENCE AND ORDER OF THE 3-POINT BLOCK EXTENDED BACKWARD DIFFERENTIATION FORMULA

THE CONVERGENCE AND ORDER OF THE 3-POINT BLOCK EXTENDED BACKWARD DIFFERENTIATION FORMULA VOL 7 NO DEEMBER ISSN 89-668 6- Asian Research Publishing Networ (ARPN) All rights reserved wwwarpnournalscom THE ONVERGENE AND ORDER OF THE -POINT BLOK EXTENDED BAKWARD DIFFERENTIATION FORMULA H Musa

More information

Time Series Analysis for Quality Improvement: a Soft Computing Approach

Time Series Analysis for Quality Improvement: a Soft Computing Approach ESANN'4 proceedings - European Smposium on Artiicial Neural Networks Bruges (Belgium), 8-3 April 4, d-side publi., ISBN -9337-4-8, pp. 19-114 ime Series Analsis or Qualit Improvement: a Sot Computing Approach

More information

2 Ordinary Differential Equations: Initial Value Problems

2 Ordinary Differential Equations: Initial Value Problems Ordinar Differential Equations: Initial Value Problems Read sections 9., (9. for information), 9.3, 9.3., 9.3. (up to p. 396), 9.3.6. Review questions 9.3, 9.4, 9.8, 9.9, 9.4 9.6.. Two Examples.. Foxes

More information

Objectives. By the time the student is finished with this section of the workbook, he/she should be able

Objectives. By the time the student is finished with this section of the workbook, he/she should be able FUNCTIONS Quadratic Functions......8 Absolute Value Functions.....48 Translations o Functions..57 Radical Functions...61 Eponential Functions...7 Logarithmic Functions......8 Cubic Functions......91 Piece-Wise

More information

Convergence of a Gauss Pseudospectral Method for Optimal Control

Convergence of a Gauss Pseudospectral Method for Optimal Control Convergence of a Gauss Pseudospectral Method for Optimal Control Hongyan Hou William W. Hager Anil V. Rao A convergence theory is presented for approximations of continuous-time optimal control problems

More information

Linear Quadratic Regulator (LQR) I

Linear Quadratic Regulator (LQR) I Optimal Control, Guidance and Estimation Lecture Linear Quadratic Regulator (LQR) I Pro. Radhakant Padhi Dept. o Aerospace Engineering Indian Institute o Science - Bangalore Generic Optimal Control Problem

More information

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are:

y R T However, the calculations are easier, when carried out using the polar set of co-ordinates ϕ,r. The relations between the co-ordinates are: Curved beams. Introduction Curved beams also called arches were invented about ears ago. he purpose was to form such a structure that would transfer loads, mainl the dead weight, to the ground b the elements

More information

y2 = 0. Show that u = e2xsin(2y) satisfies Laplace's equation.

y2 = 0. Show that u = e2xsin(2y) satisfies Laplace's equation. Review 1 1) State the largest possible domain o deinition or the unction (, ) = 3 - ) Determine the largest set o points in the -plane on which (, ) = sin-1( - ) deines a continuous unction 3) Find the

More information

Time-Frequency Analysis: Fourier Transforms and Wavelets

Time-Frequency Analysis: Fourier Transforms and Wavelets Chapter 4 Time-Frequenc Analsis: Fourier Transforms and Wavelets 4. Basics of Fourier Series 4.. Introduction Joseph Fourier (768-83) who gave his name to Fourier series, was not the first to use Fourier

More information

Lecture 8 Optimization

Lecture 8 Optimization 4/9/015 Lecture 8 Optimization EE 4386/5301 Computational Methods in EE Spring 015 Optimization 1 Outline Introduction 1D Optimization Parabolic interpolation Golden section search Newton s method Multidimensional

More information

and ( x, y) in a domain D R a unique real number denoted x y and b) = x y = {(, ) + 36} that is all points inside and on

and ( x, y) in a domain D R a unique real number denoted x y and b) = x y = {(, ) + 36} that is all points inside and on Mat 7 Calculus III Updated on 10/4/07 Dr. Firoz Chapter 14 Partial Derivatives Section 14.1 Functions o Several Variables Deinition: A unction o two variables is a rule that assigns to each ordered pair

More information

8.4 Inverse Functions

8.4 Inverse Functions Section 8. Inverse Functions 803 8. Inverse Functions As we saw in the last section, in order to solve application problems involving eponential unctions, we will need to be able to solve eponential equations

More information

Today. Introduction to optimization Definition and motivation 1-dimensional methods. Multi-dimensional methods. General strategies, value-only methods

Today. Introduction to optimization Definition and motivation 1-dimensional methods. Multi-dimensional methods. General strategies, value-only methods Optimization Last time Root inding: deinition, motivation Algorithms: Bisection, alse position, secant, Newton-Raphson Convergence & tradeos Eample applications o Newton s method Root inding in > 1 dimension

More information

Linear Quadratic Regulator (LQR) Design I

Linear Quadratic Regulator (LQR) Design I Lecture 7 Linear Quadratic Regulator LQR) Design I Dr. Radhakant Padhi Asst. Proessor Dept. o Aerospace Engineering Indian Institute o Science - Bangalore LQR Design: Problem Objective o drive the state

More information

Computational Methods for Domains with! Complex Boundaries-I!

Computational Methods for Domains with! Complex Boundaries-I! http://www.nd.edu/~gtrggva/cfd-course/ Computational Methods or Domains with Comple Boundaries-I Grétar Trggvason Spring For most engineering problems it is necessar to deal with comple geometries, consisting

More information

Feedback Linearization

Feedback Linearization Feedback Linearization Peter Al Hokayem and Eduardo Gallestey May 14, 2015 1 Introduction Consider a class o single-input-single-output (SISO) nonlinear systems o the orm ẋ = (x) + g(x)u (1) y = h(x) (2)

More information

Applications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element

Applications of Gauss-Radau and Gauss-Lobatto Numerical Integrations Over a Four Node Quadrilateral Finite Element Avaiable online at www.banglaol.info angladesh J. Sci. Ind. Res. (), 77-86, 008 ANGLADESH JOURNAL OF SCIENTIFIC AND INDUSTRIAL RESEARCH CSIR E-mail: bsir07gmail.com Abstract Applications of Gauss-Radau

More information

6.1 The Linear Elastic Model

6.1 The Linear Elastic Model Linear lasticit The simplest constitutive law or solid materials is the linear elastic law, which assumes a linear relationship between stress and engineering strain. This assumption turns out to be an

More information

Differential Equations

Differential Equations LOCUS Dierential Equations CONCEPT NOTES 0. Motiation 0. Soling Dierential Equations LOCUS Dierential Equations Section - MOTIVATION A dierential equation can simpl be said to be an equation inoling deriaties

More information

A Gauss Lobatto quadrature method for solving optimal control problems

A Gauss Lobatto quadrature method for solving optimal control problems ANZIAM J. 47 (EMAC2005) pp.c101 C115, 2006 C101 A Gauss Lobatto quadrature method for solving optimal control problems P. Williams (Received 29 August 2005; revised 13 July 2006) Abstract This paper proposes

More information

Probabilistic Optimisation applied to Spacecraft Rendezvous on Keplerian Orbits

Probabilistic Optimisation applied to Spacecraft Rendezvous on Keplerian Orbits Probabilistic Optimisation applied to pacecrat Rendezvous on Keplerian Orbits Grégory aive a, Massimiliano Vasile b a Université de Liège, Faculté des ciences Appliquées, Belgium b Dipartimento di Ingegneria

More information

Lecture : Feedback Linearization

Lecture : Feedback Linearization ecture : Feedbac inearization Niola Misovic, dipl ing and Pro Zoran Vuic June 29 Summary: This document ollows the lectures on eedbac linearization tought at the University o Zagreb, Faculty o Electrical

More information

Time-Frequency Analysis: Fourier Transforms and Wavelets

Time-Frequency Analysis: Fourier Transforms and Wavelets Chapter 4 Time-Frequenc Analsis: Fourier Transforms and Wavelets 4. Basics of Fourier Series 4.. Introduction Joseph Fourier (768-83) who gave his name to Fourier series, was not the first to use Fourier

More information

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x

UNCORRECTED. To recognise the rules of a number of common algebraic relations: y = x 1 y 2 = x 5A galler of graphs Objectives To recognise the rules of a number of common algebraic relations: = = = (rectangular hperbola) + = (circle). To be able to sketch the graphs of these relations. To be able

More information

CHAPTER-III CONVECTION IN A POROUS MEDIUM WITH EFFECT OF MAGNETIC FIELD, VARIABLE FLUID PROPERTIES AND VARYING WALL TEMPERATURE

CHAPTER-III CONVECTION IN A POROUS MEDIUM WITH EFFECT OF MAGNETIC FIELD, VARIABLE FLUID PROPERTIES AND VARYING WALL TEMPERATURE CHAPER-III CONVECION IN A POROUS MEDIUM WIH EFFEC OF MAGNEIC FIELD, VARIABLE FLUID PROPERIES AND VARYING WALL EMPERAURE 3.1. INRODUCION Heat transer studies in porous media ind applications in several

More information

Relating axial motion of optical elements to focal shift

Relating axial motion of optical elements to focal shift Relating aial motion o optical elements to ocal shit Katie Schwertz and J. H. Burge College o Optical Sciences, University o Arizona, Tucson AZ 857, USA katie.schwertz@gmail.com ABSTRACT In this paper,

More information

Introduction to Transverse Beam Optics. II.) Twiss Parameters & Lattice Design

Introduction to Transverse Beam Optics. II.) Twiss Parameters & Lattice Design Introduction to Transverse Beam Optics Bernhard Holzer, CERN II.) Twiss Parameters & Lattice esign ( Z X Y) Bunch in a storage ring Introduction to Transverse Beam Optics Bernhard Holzer, CERN... don't

More information

Optimal Control. with. Aerospace Applications. James M. Longuski. Jose J. Guzman. John E. Prussing

Optimal Control. with. Aerospace Applications. James M. Longuski. Jose J. Guzman. John E. Prussing Optimal Control with Aerospace Applications by James M. Longuski Jose J. Guzman John E. Prussing Published jointly by Microcosm Press and Springer 2014 Copyright Springer Science+Business Media New York

More information

AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS

AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS AUGMENTED POLYNOMIAL GUIDANCE FOR TERMINAL VELOCITY CONSTRAINTS Gun-Hee Moon*, Sang-Woo Shim*, and Min-Jea Tah* *Korea Advanced Institute Science and Technology Keywords: Polynomial guidance, terminal

More information

The region enclosed by the curve of f and the x-axis is rotated 360 about the x-axis. Find the volume of the solid formed.

The region enclosed by the curve of f and the x-axis is rotated 360 about the x-axis. Find the volume of the solid formed. Section A ln. Let g() =, for > 0. ln Use the quotient rule to show that g ( ). 3 (b) The graph of g has a maimum point at A. Find the -coordinate of A. (Total 7 marks) 6. Let h() =. Find h (0). cos 3.

More information

Chapter 3: Image Enhancement in the. Office room : 841

Chapter 3: Image Enhancement in the.   Office room : 841 Chapter 3: Image Enhancement in the Spatial Domain Lecturer: Jianbing Shen Email : shenjianbing@bit.edu.cn Oice room : 841 http://cs.bit.edu.cn/shenjianbing cn/shenjianbing Principle Objective o Enhancement

More information

4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY

4.7. Newton s Method. Procedure for Newton s Method HISTORICAL BIOGRAPHY 4. Newton s Method 99 4. Newton s Method HISTORICAL BIOGRAPHY Niels Henrik Abel (18 189) One of the basic problems of mathematics is solving equations. Using the quadratic root formula, we know how to

More information

References Ideal Nyquist Channel and Raised Cosine Spectrum Chapter 4.5, 4.11, S. Haykin, Communication Systems, Wiley.

References Ideal Nyquist Channel and Raised Cosine Spectrum Chapter 4.5, 4.11, S. Haykin, Communication Systems, Wiley. Baseand Data Transmission III Reerences Ideal yquist Channel and Raised Cosine Spectrum Chapter 4.5, 4., S. Haykin, Communication Systems, iley. Equalization Chapter 9., F. G. Stremler, Communication Systems,

More information

The Force Table Introduction: Theory:

The Force Table Introduction: Theory: 1 The Force Table Introduction: "The Force Table" is a simple tool for demonstrating Newton s First Law and the vector nature of forces. This tool is based on the principle of equilibrium. An object is

More information

y,z the subscript y, z indicating that the variables y and z are kept constant. The second partial differential with respect to x is written x 2 y,z

y,z the subscript y, z indicating that the variables y and z are kept constant. The second partial differential with respect to x is written x 2 y,z 8 Partial dierentials I a unction depends on more than one variable, its rate o change with respect to one o the variables can be determined keeping the others ied The dierential is then a partial dierential

More information

RATIONAL FUNCTIONS. Finding Asymptotes..347 The Domain Finding Intercepts Graphing Rational Functions

RATIONAL FUNCTIONS. Finding Asymptotes..347 The Domain Finding Intercepts Graphing Rational Functions RATIONAL FUNCTIONS Finding Asymptotes..347 The Domain....350 Finding Intercepts.....35 Graphing Rational Functions... 35 345 Objectives The ollowing is a list o objectives or this section o the workbook.

More information

Comments on Problems. 3.1 This problem offers some practice in deriving utility functions from indifference curve specifications.

Comments on Problems. 3.1 This problem offers some practice in deriving utility functions from indifference curve specifications. CHAPTER 3 PREFERENCES AND UTILITY These problems provide some practice in eamining utilit unctions b looking at indierence curve maps and at a ew unctional orms. The primar ocus is on illustrating the

More information

HYDROMAGNETIC DIVERGENT CHANNEL FLOW OF A VISCO- ELASTIC ELECTRICALLY CONDUCTING FLUID

HYDROMAGNETIC DIVERGENT CHANNEL FLOW OF A VISCO- ELASTIC ELECTRICALLY CONDUCTING FLUID Rita Choudhury et al. / International Journal o Engineering Science and Technology (IJEST) HYDROAGNETIC DIVERGENT CHANNEL FLOW OF A VISCO- ELASTIC ELECTRICALLY CONDUCTING FLUID RITA CHOUDHURY Department

More information

Relating axial motion of optical elements to focal shift

Relating axial motion of optical elements to focal shift Relating aial motion o optical elements to ocal shit Katie Schwertz and J. H. Burge College o Optical Sciences, University o Arizona, Tucson AZ 857, USA katie.schwertz@gmail.com ABSTRACT In this paper,

More information

Pre-AP Physics Chapter 1 Notes Yockers JHS 2008

Pre-AP Physics Chapter 1 Notes Yockers JHS 2008 Pre-AP Physics Chapter 1 Notes Yockers JHS 2008 Standards o Length, Mass, and Time ( - length quantities) - mass - time Derived Quantities: Examples Dimensional Analysis useul to check equations and to

More information

Lecture Outline. Basics of Spatial Filtering Smoothing Spatial Filters. Sharpening Spatial Filters

Lecture Outline. Basics of Spatial Filtering Smoothing Spatial Filters. Sharpening Spatial Filters 1 Lecture Outline Basics o Spatial Filtering Smoothing Spatial Filters Averaging ilters Order-Statistics ilters Sharpening Spatial Filters Laplacian ilters High-boost ilters Gradient Masks Combining Spatial

More information

Controlling the Heat Flux Distribution by Changing the Thickness of Heated Wall

Controlling the Heat Flux Distribution by Changing the Thickness of Heated Wall J. Basic. Appl. Sci. Res., 2(7)7270-7275, 2012 2012, TextRoad Publication ISSN 2090-4304 Journal o Basic and Applied Scientiic Research www.textroad.com Controlling the Heat Flux Distribution by Changing

More information

Proper Orthogonal Decomposition Extensions For Parametric Applications in Transonic Aerodynamics

Proper Orthogonal Decomposition Extensions For Parametric Applications in Transonic Aerodynamics Proper Orthogonal Decomposition Etensions For Parametric Applications in Transonic Aerodnamics T. Bui-Thanh, M. Damodaran Singapore-Massachusetts Institute of Technolog Alliance (SMA) School of Mechanical

More information

Differential Equaitons Equations

Differential Equaitons Equations Welcome to Multivariable Calculus / Dierential Equaitons Equations The Attached Packet is or all students who are planning to take Multibariable Multivariable Calculus/ Dierential Equations in the all.

More information

U- FUNCTION IN APPLICATIONS

U- FUNCTION IN APPLICATIONS Ushaov I. U-FUNKTION IN ALIATIONS RT&A # 0 6 Vol.7 0 September U- FUNTION IN ALIATIONS Igor Ushaov Sun Diego aliornia e-mail: igusha@gmail.com The ethod o Universal Generating Functions U-unctions was

More information

OPTIMIZATION AND EXPERIMENT OF COMPOSITE SQUARE BEAM

OPTIMIZATION AND EXPERIMENT OF COMPOSITE SQUARE BEAM THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS OPTIMIZATION AND EXPERIMENT OF COMPOSITE SQUARE BEAM T.Lili 1*, Y. Mingsen 1 1 College o Aerospace and Civil Engineering, Harbin Engineering Universit,

More information

Introduction to Differential Equations. National Chiao Tung University Chun-Jen Tsai 9/14/2011

Introduction to Differential Equations. National Chiao Tung University Chun-Jen Tsai 9/14/2011 Introduction to Differential Equations National Chiao Tung Universit Chun-Jen Tsai 9/14/011 Differential Equations Definition: An equation containing the derivatives of one or more dependent variables,

More information

Mathematical Notation Math Calculus & Analytic Geometry III

Mathematical Notation Math Calculus & Analytic Geometry III Mathematical Notation Math 221 - alculus & Analytic Geometry III Use Word or WordPerect to recreate the ollowing documents. Each article is worth 10 points and should be emailed to the instructor at james@richland.edu.

More information

One-Dimensional Motion Review IMPORTANT QUANTITIES Name Symbol Units Basic Equation Name Symbol Units Basic Equation Time t Seconds Velocity v m/s

One-Dimensional Motion Review IMPORTANT QUANTITIES Name Symbol Units Basic Equation Name Symbol Units Basic Equation Time t Seconds Velocity v m/s One-Dimensional Motion Review IMPORTANT QUANTITIES Name Symbol Units Basic Equation Name Symbol Units Basic Equation Time t Seconds Velocity v m/s v x t Position x Meters Speed v m/s v t Length l Meters

More information

( x) f = where P and Q are polynomials.

( x) f = where P and Q are polynomials. 9.8 Graphing Rational Functions Lets begin with a deinition. Deinition: Rational Function A rational unction is a unction o the orm ( ) ( ) ( ) P where P and Q are polynomials. Q An eample o a simple rational

More information

4452 Mathematical Modeling Lecture 13: Chaos and Fractals

4452 Mathematical Modeling Lecture 13: Chaos and Fractals Math Modeling Lecture 13: Chaos and Fractals Page 1 442 Mathematical Modeling Lecture 13: Chaos and Fractals Introduction In our tetbook, the discussion on chaos and fractals covers less than 2 pages.

More information

Math Review and Lessons in Calculus

Math Review and Lessons in Calculus Math Review and Lessons in Calculus Agenda Rules o Eponents Functions Inverses Limits Calculus Rules o Eponents 0 Zero Eponent Rule a * b ab Product Rule * 3 5 a / b a-b Quotient Rule 5 / 3 -a / a Negative

More information

Strain Transformation and Rosette Gage Theory

Strain Transformation and Rosette Gage Theory Strain Transformation and Rosette Gage Theor It is often desired to measure the full state of strain on the surface of a part, that is to measure not onl the two etensional strains, and, but also the shear

More information

KEY IDEAS. Chapter 1 Function Transformations. 1.1 Horizontal and Vertical Translations Pre-Calculus 12 Student Workbook MHR 1

KEY IDEAS. Chapter 1 Function Transformations. 1.1 Horizontal and Vertical Translations Pre-Calculus 12 Student Workbook MHR 1 Chapter Function Transformations. Horizontal and Vertical Translations A translation can move the graph of a function up or down (vertical translation) and right or left (horizontal translation). A translation

More information

Differentiation. The main problem of differential calculus deals with finding the slope of the tangent line at a point on a curve.

Differentiation. The main problem of differential calculus deals with finding the slope of the tangent line at a point on a curve. Dierentiation The main problem o dierential calculus deals with inding the slope o the tangent line at a point on a curve. deinition() : The slope o a curve at a point p is the slope, i it eists, o the

More information

4.1 & 4.2 Student Notes Using the First and Second Derivatives. for all x in D, where D is the domain of f. The number f()

4.1 & 4.2 Student Notes Using the First and Second Derivatives. for all x in D, where D is the domain of f. The number f() 4.1 & 4. Student Notes Using the First and Second Derivatives Deinition A unction has an absolute maimum (or global maimum) at c i ( c) ( ) or all in D, where D is the domain o. The number () c is called

More information

( 1) ( 2) ( 1) nan integer, since the potential is no longer simple harmonic.

( 1) ( 2) ( 1) nan integer, since the potential is no longer simple harmonic. . Anharmonic Oscillators Michael Fowler Landau (para 8) considers a simple harmonic oscillator with added small potential energy terms mα + mβ. We ll simpliy slightly by dropping the term, to give an equation

More information

Gauss Pseudospectral Method for Solving Infinite-Horizon Optimal Control Problems

Gauss Pseudospectral Method for Solving Infinite-Horizon Optimal Control Problems AIAA Guidance, Navigation, and Control Conference 2-5 August 21, Toronto, Ontario Canada AIAA 21-789 Gauss Pseudospectral Method for Solving Infinite-Horizon Optimal Control Problems Divya Garg William

More information

This is only a list of questions use a separate sheet to work out the problems. 1. (1.2 and 1.4) Use the given graph to answer each question.

This is only a list of questions use a separate sheet to work out the problems. 1. (1.2 and 1.4) Use the given graph to answer each question. Mth Calculus Practice Eam Questions NOTE: These questions should not be taken as a complete list o possible problems. The are merel intended to be eamples o the diicult level o the regular eam questions.

More information

1 Relative degree and local normal forms

1 Relative degree and local normal forms THE ZERO DYNAMICS OF A NONLINEAR SYSTEM 1 Relative degree and local normal orms The purpose o this Section is to show how single-input single-output nonlinear systems can be locally given, by means o a

More information

Topic 4b. Open Methods for Root Finding

Topic 4b. Open Methods for Root Finding Course Instructor Dr. Ramond C. Rump Oice: A 337 Phone: (915) 747 6958 E Mail: rcrump@utep.edu Topic 4b Open Methods or Root Finding EE 4386/5301 Computational Methods in EE Outline Open Methods or Root

More information

Engineering Notes. NUMERICAL methods for solving optimal control problems fall

Engineering Notes. NUMERICAL methods for solving optimal control problems fall JOURNAL OF GUIANCE, CONTROL, AN YNAMICS Vol. 9, No. 6, November ecember 6 Engineering Notes ENGINEERING NOTES are short manuscripts describing ne developments or important results of a preliminary nature.

More information

Numerical Solution of Ordinary Differential Equations in Fluctuationlessness Theorem Perspective

Numerical Solution of Ordinary Differential Equations in Fluctuationlessness Theorem Perspective Numerical Solution o Ordinary Dierential Equations in Fluctuationlessness Theorem Perspective NEJLA ALTAY Bahçeşehir University Faculty o Arts and Sciences Beşiktaş, İstanbul TÜRKİYE TURKEY METİN DEMİRALP

More information

Topic02_PDE. 8/29/2006 topic02_pde 1. Computational Fluid Dynamics (AE/ME 339) MAE Dept., UMR

Topic02_PDE. 8/29/2006 topic02_pde 1. Computational Fluid Dynamics (AE/ME 339) MAE Dept., UMR MEAE 9 Computational Fluid Dnamics Topic0_ 89006 topic0_ Partial Dierential Equations () (CLW: 7., 7., 7.4) s can be linear or nonlinear Order : Determined b the order o the highest derivative. Linear,

More information

Sec 3.1. lim and lim e 0. Exponential Functions. f x 9, write the equation of the graph that results from: A. Limit Rules

Sec 3.1. lim and lim e 0. Exponential Functions. f x 9, write the equation of the graph that results from: A. Limit Rules Sec 3. Eponential Functions A. Limit Rules. r lim a a r. I a, then lim a and lim a 0 3. I 0 a, then lim a 0 and lim a 4. lim e 0 5. e lim and lim e 0 Eamples:. Starting with the graph o a.) Shiting 9 units

More information

SWEEP METHOD IN ANALYSIS OPTIMAL CONTROL FOR RENDEZ-VOUS PROBLEMS

SWEEP METHOD IN ANALYSIS OPTIMAL CONTROL FOR RENDEZ-VOUS PROBLEMS J. Appl. Math. & Computing Vol. 23(2007), No. 1-2, pp. 243-256 Website: http://jamc.net SWEEP METHOD IN ANALYSIS OPTIMAL CONTROL FOR RENDEZ-VOUS PROBLEMS MIHAI POPESCU Abstract. This paper deals with determining

More information

Mathematics 309 Conic sections and their applicationsn. Chapter 2. Quadric figures. ai,j x i x j + b i x i + c =0. 1. Coordinate changes

Mathematics 309 Conic sections and their applicationsn. Chapter 2. Quadric figures. ai,j x i x j + b i x i + c =0. 1. Coordinate changes Mathematics 309 Conic sections and their applicationsn Chapter 2. Quadric figures In this chapter want to outline quickl how to decide what figure associated in 2D and 3D to quadratic equations look like.

More information

Support Vector Machines

Support Vector Machines Support Vector Machines Optimall deined decision surace Tpicall nonlinear in the input space Linear in a higher dimensional space Implicitl deined b a kernel unction What are Support Vector Machines Used

More information

Mat 267 Engineering Calculus III Updated on 9/19/2010

Mat 267 Engineering Calculus III Updated on 9/19/2010 Chapter 11 Partial Derivatives Section 11.1 Functions o Several Variables Deinition: A unction o two variables is a rule that assigns to each ordered pair o real numbers (, ) in a set D a unique real number

More information

Solving Second Order Linear Dirichlet and Neumann Boundary Value Problems by Block Method

Solving Second Order Linear Dirichlet and Neumann Boundary Value Problems by Block Method IAENG International Journal o Applied Matematics 43: IJAM_43 04 Solving Second Order Linear Diriclet and Neumann Boundar Value Problems b Block Metod Zanaria Abdul Majid Mod Mugti Hasni and Norazak Senu

More information

Mathematics. Mathematics 1. hsn.uk.net. Higher HSN21000

Mathematics. Mathematics 1. hsn.uk.net. Higher HSN21000 Higher Mathematics UNIT Mathematics HSN000 This document was produced speciall for the HSN.uk.net website, and we require that an copies or derivative works attribute the work to Higher Still Notes. For

More information

BOUNDARY LAYER ANALYSIS ALONG A STRETCHING WEDGE SURFACE WITH MAGNETIC FIELD IN A NANOFLUID

BOUNDARY LAYER ANALYSIS ALONG A STRETCHING WEDGE SURFACE WITH MAGNETIC FIELD IN A NANOFLUID Proceedings o the International Conerence on Mechanical Engineering and Reneable Energy 7 (ICMERE7) 8 December, 7, Chittagong, Bangladesh ICMERE7-PI- BOUNDARY LAYER ANALYSIS ALONG A STRETCHING WEDGE SURFACE

More information

520 Chapter 9. Nonlinear Differential Equations and Stability. dt =

520 Chapter 9. Nonlinear Differential Equations and Stability. dt = 5 Chapter 9. Nonlinear Differential Equations and Stabilit dt L dθ. g cos θ cos α Wh was the negative square root chosen in the last equation? (b) If T is the natural period of oscillation, derive the

More information