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Chapter 1

Arithmetic

Definitions

 Bit =0 or 1 Byte =8 bits  Word = Reals: 4 bytes (single precision) 8 bytes (double precision) = Integers: 1,2,4, or 8 byte signed 1,2,4, or 8 byte unsigned 

Numbers with a decimal or binary point

 Decimal: 103102101100101102103104 Binary: 2322212021222324

Examples of binary numbers

 Decimal  Binary 1121031141000.50.11.51.1

numbers

{0,1,2,3,,9,10,11,12,13,14,15}={0,1,2,3..9,a,b,c,d,e,f}

unsigned integers as hex numbers

 Decimal  Binary  Hex 100011200102300113101010 a 151111 f 

single precision format:

image

where s=sign

e= biased exponent 

p=e127= exponent 

 1.f = significand (use binary point) 

Special numbers

Smallest exponent: Largest exponent:

image

reserved reserved

Smallest positive normal number

image

bin: 00000000000000000000000000000000

hex: 00000000

image

Examples of computer numbers

What is 1.0,2.0&1/2 in hex?

1.0=(1)0×2(127127)×1.0

Therefore, s=0,e=01111111,f=00000000000000000000000

bin: 00111111100000000000000000000000

hex: 3 f 800000

2.0=(1)0×2(128127)×1.0

Therefore, s=0,e=10000000,f=00000000000000000000000

bin: 010000000100000000000000000000000

hex: 40000000

1/2=(1)0×2(126127)×1.0

Therefore, s=0,e=01111110,f=00000000000000000000000

bin: 00111111000000000000000000000000

hex: 3 f00 0000

Inexact numbers

Example:

13=(1)0×14×(1+13)

so that p=e127=2 and e=125=1283, or in binary, e=01111101. How is f=1/3 represented in binary? To compute binary number, multiply successively by 2 as follows:

0.3330.0.6660.01.3330.010.6660.0101.3330.0101 etc. 

so that 1/3 exactly in binary is 0.010101 With only 23 bits to represent f, the number is inexact and we have

f=01010101010101010101011

where we have rounded to the nearest binary number (here, rounded up). The machine number 1/3 is then represented as

00111110101010101010101010101011

or in hex

 Зeaaaaab. 

smallest positive integer that is not exact in single pre- cision

Let N be the smallest positive integer that is not exact. Now, I claim that

N2=223×1.111

and

N1=224×1.000

The integer N would then require a one-bit in the 224 position, which is not available. Therefore, the smallest positive integer that is not exact is 224+1=16777217. In MATLAB, single (224) has the same value as single (224+1). Since single (224+1) is exactly halfway between the two consecutive machine numbers 224 and 224+2, MATLAB rounds to the number with a final zero-bit in f, which is 224.

Machine epsilon

Machine epsilon (ϵmach) is the distance between 1 and the next largest number. If 0δ<ϵmach/2, then 1+δ=1 in computer math. Also since

x+y=x(1+y/x)

if 0y/x<ϵmach/2, then x+y=x in computer math.

Find ϵmach 

The number 1 in the IEEE format is written as

1=20×1.0000,

with 230 s following the binary point. The number just larger than 1 has a 1 in the 23 rd position after the decimal point. Therefore,

ϵmach =2231.192×107

What is the distance between 1 and the number just smaller than 1? Here, the number just smaller than one can be written as

21×1.1111=21(1+(1223))=1224

Therefore, this distance is 224=ϵmach/2.

The spacing between numbers is uniform between powers of 2, with logarithmic spacing of the powers of 2 . That is, the spacing of numbers between 1 and 2 is 223, between 2 and 4 is 222, between 4 and 8 is 221, etc. This spacing changes for denormal numbers, where the spacing is uniform all the way down to zero.

Find the machine number just greater than 5

A rough estimate would be 5(1+ϵmach )=5+5ϵmach , but this is not exact. The exact answer can be found by writing

5=22(1+14)

so that the next largest number is

22(1+14+223)=5+221=5+4ϵmach 

double precision format

Most computations take place in double precision, where round-off error is reduced, and all of the above calculations in single precision can be repeated for double precision. The format is

image

where s=sign

e= biased exponent

p=e1023= exponent

1.f = significand (use binary point)

1.12 Roundoff error example

Consider solving the quadratic equation

x2+2bx1=0

where b is a parameter. The quadratic formula yields the two solutions

x±=b±b2+1

Consider the solution with b>0 and x>0 (the x+solution) given by

x=b+b2+1

As b

x=b+b2+1=b+b1+1/b2=b(1+1/b21)b(1+12b21)=12b.

Now in double precision, realmin 2.2×10308 and we would like x to be accurate to this value before it goes to 0 via denormal numbers. Therefore, x should be computed accurately to b1/(2× realmin )2×10307. What happens if we compute (1.1) directly? Then x=0 when b2+1=b2, or 1+1/b2=1. That is 1/b2=ϵmach /2, or b=2/ϵmach 108. For a subroutine written to compute the solution of a quadratic for a general user, this is not good enough. The way for a software designer to solve this problem is to compute the solution for x as

x=1b(1+1+1/b2)

In this form, if 1+1/b2=1, then x=1/2b which is the correct asymptotic form.

Chapter 2

Finding

Solve f(x)=0 for x, when an explicit analytical solution is impossible.

Bisection Method

The bisection method is the easiest to numerically implement and almost always works. The main disadvantage is that convergence is slow. If the bisection method results in a computer program that runs too slow, then other faster methods may be chosen; otherwise it is a good choice of method.

We want to construct a sequence x0,x1,x2, that converges to the root x=r that solves f(x)=0. We choose x0 and x1 such that x0<r<x1. We say that x0 and x1 bracket the root. With f(r)=0, we want f(x0) and f(x1) to be of opposite sign, so that f(x0)f(x1)<0. We then assign x2 to be the midpoint of x0 and x1, that is x2=(x0+x1)/2, or

x2=x0+x1x02

The sign of f(x2) can then be determined. The value of x3 is then chosen as either the midpoint of x0 and x2 or as the midpoint of x2 and x1, depending on whether x0 and x2 bracket the root, or x2 and x1 bracket the root. The root, therefore, stays bracketed at all times. The algorithm proceeds in this fashion and is typically stopped when the increment to the left side of the bracket (above, given by (x1 x0)/2 ) is smaller than some required precision.

2.2 Newton’s Method

This is the fastest method, but requires analytical computation of the derivative of f(x). Also, the method may not always converge to the desired root.

We can derive Newton’s Method graphically, or by a Taylor series. We again want to construct a sequence x0,x1,x2, that converges to the root x=r. Consider the xn+1 member of this sequence, and Taylor series expand f(xn+1) about the point xn. We have

f(xn+1)=f(xn)+(xn+1xn)f(xn)+.

To determine xn+1, we drop the higher-order terms in the Taylor series, and assume f(xn+1)=0. Solving for xn+1, we have

xn+1=xnf(xn)f(xn)

Starting Newton’s Method requires a guess for x0, hopefully close to the root x=r.

Secant Method

The Secant Method is second best to Newton’s Method, and is used when a faster convergence than Bisection is desired, but it is too difficult or impossible to take an analytical derivative of the function f(x). We write in place of f(xn),

f(xn)f(xn)f(xn1)xnxn1

Starting the Secant Method requires a guess for both x0 and x1.

Estimate 2=1.41421356 using Newton’s Method

The 2 is the zero of the function f(x)=x22. To implement Newton’s Method, we use f(x)=2x. Therefore, Newton’s Method is the iteration

xn+1=xnx2n22xn

We take as our initial guess x0=1. Then

x1=112=32=1.5x2=329423=1712=1.416667,x3=17121721222176=577408=1.41426.

Example of fractals using Newton’s Method

Consider the complex roots of the equation f(z)=0, where

f(z)=z31

These roots are the three cubic roots of unity. With

ei2πn=1,n=0,1,2,

the three unique cubic roots of unity are given by

1,ei2π/3,ei4π/3

With

eiθ=cosθ+isinθ,

and cos(2π/3)=1/2,sin(2π/3)=3/2, the three cubic roots of unity are

r1=1,r2=12+32i,r3=1232i

The interesting idea here is to determine which initial values of z0 in the complex plane converge to which of the three cubic roots of unity.

Newton’s method is

zn+1=znz3n13z2n

If the iteration converges to r1, we color z0 red; r2, blue; r3, green. The result will be shown in lecture.

Order of convergence

Let r be the root and xn be the nth approximation to the root. Define the error as

ϵn=rxn

If for large n we have the approximate relationship

|ϵn+1|=k|ϵn|p,

with k a positive constant, then we say the root-finding numerical method is of order p. Larger values of p correspond to faster convergence to the root. The order of convergence of bisection is one: the error is reduced by approximately a factor of 2 with each iteration so that

|ϵn+1|=12|ϵn|.

We now find the order of convergence for Newton’s Method and for the Secant Method.

Newton’s Method

We start with Newton’s Method

xn+1=xnf(xn)f(xn)

Subtracting both sides from r, we have

rxn+1=rxn+f(xn)f(xn)

Or

ϵn+1=ϵn+f(xn)f(xn)

We use Taylor series to expand the functions f(xn) and f(xn) about the root r, using f(r)=0. We have

f(xn)=f(r)+(xnr)f(r)+12(xnr)2f(r)+,=ϵnf(r)+12ϵ2nf(r)+;f(xn)=f(r)+(xnr)f(r)+12(xnr)2f(r)+,=f(r)ϵnf(r)+12ϵ2nf(r)+

To make further progress, we will make use of the following standard Taylor series:

11ϵ=1+ϵ+ϵ2+,

which converges for |ϵ|<1. Substituting (2.2) into (2.1), and using (2.3) yields

ϵn+1=ϵn+f(xn)f(xn)=ϵn+ϵnf(r)+12ϵ2nf(r)+f(r)ϵnf(r)+12ϵ2nf(r)+=ϵn+ϵn+12ϵ2nf(r)f(r)+1ϵnf(r)f(r)+=ϵn+(ϵn+12ϵ2nf(r)f(r)+)(1+ϵnf(r)f(r)+)=ϵn+(ϵn+ϵ2n(12f(r)f(r)f(r)f(r))+)=12f(r)f(r)ϵ2n+

Therefore, we have shown that

|ϵn+1|=k|ϵn|2

as n, with

k=12|f(r)f(r)|

provided f(r)0. Newton’s method is thus of order 2 at simple roots.

Secant Method

Determining the order of the Secant Method proceeds in a similar fashion. We start with

xn+1=xn(xnxn1)f(xn)f(xn)f(xn1)

We subtract both sides from r and make use of

xnxn1=(rxn1)(rxn)=ϵn1ϵn

and the Taylor series

f(xn)=ϵnf(r)+12ϵ2nf(r)+,f(xn1)=ϵn1f(r)+12ϵ2n1f(r)+,

so that

f(xn)f(xn1)=(ϵn1ϵn)f(r)+12(ϵ2nϵ2n1)f(r)+=(ϵn1ϵn)(f(r)12(ϵn1+ϵn)f(r)+)

We therefore have

ϵn+1=ϵn+ϵnf(r)+12ϵ2nf(r)+f(r)12(ϵn1+ϵn)f(r)+=ϵnϵn112ϵnf(r)f(r)+112(ϵn1+ϵn)f(r)f(r)+=ϵnϵn(112ϵnf(r)f(r)+)(1+12(ϵn1+ϵn)f(r)f(r)+)=12f(r)f(r)ϵn1ϵn+,

or to leading order

|ϵn+1|=12|f(r)f(r)||ϵn1||ϵn|

The order of convergence is not yet obvious from this equation, and to determine the scaling law we look for a solution of the form

|ϵn+1|=k|ϵn|p.

From this ansatz, we also have

|ϵn|=k|ϵn1|p

and therefore

|ϵn+1|=kp+1|ϵn1|p2

Substitution into (2.4) results in

kp+1|ϵn1|p2=k2|f(r)f(r)||ϵn1|p+1

Equating the coefficient and the power of ϵn1 results in

kp=12|f(r)f(r)|

and

p2=p+1

The order of convergence of the Secant Method, given by p, therefore is determined to be the positive root of the quadratic equation p2p1=0, or

p=1+521.618

which coincidentally is a famous irrational number that is called The Golden Ratio, and goes by the symbol Φ. We see that the Secant Method has an order of convergence lying between the Bisection Method and Newton’s Method.

image

Chapter 3

Systems of equations

Consider the system of n linear equations and n unknowns, given by

a11x1+a12x2++a1nxn=b1a21x1+a22x2++a2nxn=b2an1x1+an2x2++annxn=bn

We can write this system as the matrix equation

Ax=b

with

A=(a11a12a1na21a22a2nan1an2ann),x=(x1x2xn),b=(b1b2bn)

Gaussian Elimination

The standard numerical algorithm to solve a system of linear equations is called Gaussian Elimination. We can illustrate this algorithm by example.

Consider the system of equations

3x1+2x2x3=16x16x2+7x3=73x14x2+4x3=6

To perform Gaussian elimination, we form an Augmented Matrix by combining the matrix A with the column vector b :

(321166773446)

Row reduction is then performed on this matrix. Allowed operations are (1) multiply any row by a constant, (2) add multiple of one row to another row, (3) interchange the order of any rows. The goal is to convert the original matrix into an upper-triangular matrix

We start with the first row of the matrix and work our way down as follows. First we multiply the first row by 2 and add it to the second row, and add the first row to the third row:

(321102590237)

We then go to the second row. We multiply this row by 1 and add it to the third row:

(321102590022)

The resulting equations can be determined from the matrix and are given by

3x1+2x2x3=12x2+5x3=92x3=2

These equations can be solved by backward substitution, starting from the last equation and working backwards. We have

2x3=2x3=12x2=95x3=4x2=23x1=12x2+x3=6x1=2

Therefore,

(x1x2x3)=(221)

U\) decomposition

The process of Gaussian Elimination also results in the factoring of the matrix A to

A=LU,

where L is a lower triangular matrix and U is an upper triangular matrix. Using the same matrix A as in the last section, we show how this factorization is realized. We have

(321667344)(321025023)=M1 A

where

M1 A=(100210101)(321667344)=(321025023)

Note that the matrix M1 performs row elimination on the first column. Two times the first row is added to the second row and one times the first row is added to the third row. The entries of the column of M1 come from 2=(6/3) and 1=(3/3) as required for row elimination. The number 3 is called the pivot.

The next step is

(321025023)(321025002)=M2(M1 A)

where

M2(M1 A)=(100010011)(321025023)=(321025002)

Here, M2 multiplies the second row by 1=(2/2) and adds it to the third row. The pivot is 2.

We now have

M2M1 A=U

or

A=M11M12U

The inverse matrices are easy to find. The matrix M1 multiples the first row by 2 and adds it to the second row, and multiplies the first row by 1 and adds it to the third row. To invert these operations, we need to multiply the first row by 2 and add it to the second row, and multiply the first row by 1 and add it to the third row. To check, with

M1M11=I

we have

(100210101)(100210101)=(100010001)

Similarly,

M12=(100010011)

Therefore,

L=M11M12

is given by

L=(100210101)(100010011)=(100210111)

which is lower triangular. The off-diagonal elements of M11 and M12 are simply combined to form L. Our LU decomposition is therefore

(321667344)=(100210111)(321025002).

Another nice feature of the LU decomposition is that it can be done by overwriting A, therefore saving memory if the matrix A is very large.

The LU decomposition is useful when one needs to solve Ax=b for x when A is fixed and there are many different b’s. First one determines L and U using Gaussian elimination. Then one writes

(LU)x=L(Ux)=b.

We let

y=Ux

and first solve

Ly=b

for y by forward substitution. We then solve

Ux=y

for x by backward substitution. When we count operations, we will see that solving (LU)x=b is significantly faster once L and U are in hand than solving Ax=b directly by Gaussian elimination.

We now illustrate the solution of LUx=b using our previous example, where

L=(100210111),U=(321025002),b=(176)

With y=Ux, we first solve Ly=b, that is

(100210111)(y1y2y3)=(176)

Using forward substitution

y1=1y2=7+2y1=9y3=6+y1y2=2

We now solve Ux=y, that is

(321025002)(x1x2x3)=(192)

Using backward substitution,

2x3=2x3=12x2=95x3=4x2=23x1=12x2+x3=6x1=2

and we have once again determined

(x1x2x3)=(221)

Partial pivoting

When performing Gaussian elimination, the diagonal element that one uses during the elimination procedure is called the pivot. To obtain the correct multiple, one uses the pivot as the divisor to the elements below the pivot. Gaussian elimination in this form will fail if the pivot is zero. In this situation, a row interchange must be performed.

Even if the pivot is not identically zero, a small value can result in big roundoff errors. For very large matrices, one can easily lose all accuracy in the solution. To avoid these round-off errors arising from small pivots, row interchanges are made, and this technique is called partial pivoting (partial pivoting is in contrast to complete pivoting, where both rows and columns are interchanged). We will illustrate by example the LU decomposition using partial pivoting. Consider

A=(221667384)

We interchange rows to place the largest element (in absolute value) in the pivot, or a11, position. That is,

A(667221384)=P12 A

where

P12=(010100001)

is a permutation matrix that when multiplied on the left interchanges the first and second rows of a matrix. Note that P112=P12. The elimination step is then

P12 A(667004/3051/2)=M1P12 A

where

M1=(1001/3101/201)

The final step requires one more row interchange:

M1P12 A(667051/2004/3)=P23M1P12 A=U

Since the permutation matrices given by P are their own inverses, we can write our result as

(P23M1P23)P23P12A=U

Multiplication of M on the left by P interchanges rows while multiplication on the right by P interchanges columns. That is,

P23(1001/3101/201)P23=(1001/2011/310)P23=(1001/2101/301)

The net result on M1 is an interchange of the nondiagonal elements 1/3 and 1/2.

We can then multiply by the inverse of (P23M1P23) to obtain

P23P12A=(P23M1P23)1U

which we write as

PA=LU

Instead of L, MATLAB will write this as

A=(P1 L)U

For convenience, we will just denote (P1 L) by L, but by L here we mean a permutated lower triangular matrix.

For example, in MATLAB, to solve Ax=b for x using Gaussian elimination, one types

x=Ab

where \solves for x using the most efficient algorithm available, depending on the form of A. If A is a general n×n matrix, then first the LU decomposition of A is found using partial pivoting, and then x is determined from permuted forward and backward substitution. If A is upper or lower triangular, then forward or backward substitution (or their permuted version) is used directly.

If there are many different right-hand-sides, one would first directly find the LU decomposition of A using a function call, and then solve using . That is, one would iterate for different b s the following expressions:

[LU]=lu( A)y=Lbx=Uy

where the second and third lines can be shortened to

x=U(Lb)

where the parenthesis are required. In lecture, I will demonstrate these solutions in MATLAB using the matrix A=[2,2,1;6,6,7;3,8,4]; which is the example in the notes.

3.4 Operation counts

To estimate how much computational time is required for an algorithm, one can count the number of operations required (multiplications, divisions, additions and subtractions). Usually, what is of interest is how the algorithm scales with the size of the problem. For example, suppose one wants to multiply two full n×n matrices. The calculation of each element requires n multiplications and n1 additions, or say 2n1 operations. There are n2 elements to compute so that the total operation count is n2(2n1). If n is large, we might want to know what will happen to the computational time if n is doubled. What matters most is the fastest-growing, leading-order term in the operation count. In this matrix multiplication example, the operation count is n2(2n1)=2n3n2, and the leading-order term is 2n3. The factor of 2 is unimportant for the scaling, and we say that the algorithm scales like O(n3), which is read as "big Oh of n cubed." When using the big-Oh notation, we will drop both lower-order terms and constant multipliers.

The big-Oh notation tells us how the computational time of an algorithm scales. For example, suppose that the multiplication of two large n×n matrices took a computational time of Tn seconds. With the known operation count going like O(n3), we can write

Tn=kn3

for some unknown constant k. To determine how much longer the multiplication of two 2n×2n matrices will take, we write

T2n=k(2n)3=8kn3=8Tn

so that doubling the size of the matrix is expected to increase the computational time by a factor of 23=8.

Running MATLAB on my computer, the multiplication of two 2048×2048 matrices took about 0.75sec. The multiplication of two 4096×4096 matrices took about 6sec, which is 8 times longer. Timing of code in MATLAB can be found using the built-in stopwatch functions tic and toc.

What is the operation count and therefore the scaling of Gaussian elimination? Consider an elimination step with the pivot in the i th row and i th column. There are both ni rows below the pivot and ni columns to the right of the pivot. To perform elimination of one row, each matrix element to the right of the pivot must be multiplied by a factor and added to the row underneath. This must be done for all the rows. There are therefore (ni)(ni) multiplication-additions to be done for this pivot. Since we are interested in only the scaling of the algorithm, I will just count a multiplication-addition as one operation.

To find the total operation count, we need to perform elimination using n1 pivots, so that

 op. counts =n1i=1(ni)2=(n1)2+(n2)2+(1)2=n1i=1i2

Three summation formulas will come in handy. They are

ni=11=nni=1i=12n(n+1)ni=1i2=16n(2n+1)(n+1)

which can be proved by mathematical induction, or derived by some tricks.

The operation count for Gaussian elimination is therefore

 op. counts =n1i=1i2=16(n1)(2n1)(n)

The leading-order term is therefore n3/3, and we say that Gaussian elimination scales like O(n3). Since LU decomposition with partial pivoting is essentially Gaussian elimination, that algorithm also scales like O(n3). However, once the LU decomposition of a matrix A is known, the solution of Ax=b can proceed by a forward and backward substitution. How does a backward substitution, say, scale? For backward substitution, the matrix equation to be solved is of the form

(a1,1a1,2a1,n1a1,n0a2,2a2,n1a2,n00an1,n1an1,n000an,n)(x1x2xn1xn)=(b1b2bn1bn)

The solution for xi is found after solving for xj with j>i. The explicit solution for xi is given by

xi=1ai,i(binj=i+1ai,jxj)

The solution for xi requires ni+1 multiplication-additions, and since this must be done for n such i s, we have

 op. counts =ni=1ni+1=n+(n1)++1=ni=1i=12n(n+1)

The leading-order term is n2/2 and the scaling of backward substitution is O(n2). After the LU decomposition of a matrix A is found, only a single forward and backward substitution is required to solve Ax=b, and the scaling of the algorithm to solve this matrix equation is therefore still O(n2). For large n, one should expect that solving Ax=b by a forward and backward substitution should be substantially faster than a direct solution using Gaussian elimination.

3.5 System of nonlinear equations

A system of nonlinear equations can be solved using a version of Newton’s Method. We illustrate this method for a system of two equations and two unknowns. Suppose that we want to solve

f(x,y)=0,g(x,y)=0

for the unknowns x and y. We want to construct two simultaneous sequences x0,x1,x2, and y0,y1,y2, that converge to the roots. To construct these sequences, we Taylor series expand f(xn+1,yn+1) and g(xn+1,yn+1) about the point (xn,yn). Using the partial derivatives fx=f/x,fy=f/y, etc., the twodimensional Taylor series expansions, displaying only the linear terms, are given by

f(xn+1,yn+1)=f(xn,yn)+(xn+1xn)fx(xn,yn)+(yn+1yn)fy(xn,yn)+

g(xn+1,yn+1)=g(xn,yn)+(xn+1xn)gx(xn,yn)

+(yn+1yn)gy(xn,yn)+

To obtain Newton’s method, we take f(xn+1,yn+1)=0,g(xn+1,yn+1)=0 and drop higher-order terms above linear. Although one can then find a system of linear equations for xn+1 and yn+1, it is more convenient to define the variables

Δxn=xn+1xn,Δyn=yn+1yn.

The iteration equations will then be given by

xn+1=xn+Δxn,yn+1=yn+Δyn

and the linear equations to be solved for Δxn and Δyn are given by

(fxfygxgy)(ΔxnΔyn)=(fg)

where f,g,fx,fy,gx, and gy are all evaluated at the point (xn,yn). The twodimensional case is easily generalized to n dimensions. The matrix of partial derivatives is called the Jacobian Matrix.

We illustrate Newton’s Method by finding the steady state solution of the Lorenz equations, given by

σ(yx)=0rxyxz=0xybz=0

where x,y, and z are the unknown variables and σ,r, and b are the known parameters. Here, we have a three-dimensional homogeneous system f=0,g=0, and h=0, with

f(x,y,z)=σ(yx)g(x,y,z)=rxyxzh(x,y,z)=xybz.

The partial derivatives can be computed to be

fx=σ,fy=σ,fz=0,gx=rz,gy=1,gz=x,hx=y,hy=x,hz=b.

The iteration equation is therefore

(σσ0rzn1xnynxnb)(ΔxnΔynΔzn)=(σ(ynxn)rxnynxnznxnynbzn)

with

xn+1=xn+Δxnyn+1=yn+Δynzn+1=zn+Δzn

The MATLAB program that solves this system is contained in newton_system.m.

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Chapter 4

Least-squares approximation

The method of least-squares is commonly used to fit a parameterized curve to experimental data. In general, the fitting curve is not expected to pass through the data points, making this problem substantially different from the one of interpolation.

We consider here only the simplest case of the same experimental error for all the data points. Let the data to be fitted be given by (xi,yi), with i=1 to n.

Fitting a straight line

Suppose the fitting curve is a line. We write for the fitting curve

y(x)=αx+β.

The distance ri from the data point (xi,yi) and the fitting curve is given by

ri=yiy(xi)=yi(αxi+β).

A least-squares fit minimizes the sum of the squares of the ri ’s. This minimum can be shown to result in the most probable values of α and β.

We define

ρ=ni=1r2i=ni=1(yi(αxi+β))2

To minimize ρ with respect to α and β, we solve

ρα=0,ρβ=0

Taking the partial derivatives, we have

ρα=ni=12(xi)(yi(αxi+β))=0ρβ=ni=12(1)(yi(αxi+β))=0

These equations form a system of two linear equations in the two unknowns α and β, which is evident when rewritten in the form

αni=1x2i+βni=1xi=ni=1xiyiαni=1xi+βn=ni=1yi

These equations can be solved either analytically, or numerically in MATLAB, where the matrix form is

(ni=1x2ini=1ni=1xin)(αβ)=(ni=1xiyini=1yi).

A proper statistical treatment of this problem should also consider an estimate of the errors in α and β as well as an estimate of the goodness-of-fit of the data to the model. We leave these further considerations to a statistics class.

Fitting to a linear combination of functions

Consider the general fitting function

y(x)=mj=1cjfj(x)

where we assume m functions fj(x). For example, if we want to fit a cubic polynomial to the data, then we would have m=4 and take f1=1,f2=x,f3=x2 and f4=x3. Typically, the number of functions fj is less than the number of data points; that is, m<n, so that a direct attempt to solve for the cj s such that the fitting function exactly passes through the n data points would result in n equations and m unknowns. This would be an over-determined linear system that in general has no solution.

We now define the vectors

y=(y1y2yn),c=(c1c2cm)

and the n-by-m matrix

A=(f1(x1)f2(x1)fm(x1)f1(x2)f2(x2)fm(x2)f1(xn)f2(xn)fm(xn))

With m<n, the equation Ac=y is over-determined. We let

r=yAc

be the residual vector, and let

ρ=ni=1r2i

The method of least squares minimizes ρ with respect to the components of c. Now, using T to signify the transpose of a matrix, we have

ρ=rTr=(yAc)T(yAc)=yTycT ATyyT Ac+cT AT Ac.

Since ρ is a scalar, each term in the above expression must be a scalar, and since the transpose of a scalar is equal to the scalar, we have

cT ATy=(cT ATy)T=yT Ac.

Therefore,

ρ=yTy2yT Ac+cT AT Ac.

To find the minimum of ρ, we will need to solve ρ/cj=0 for j=1,,m. To take the derivative of ρ, we switch to a tensor notation, using the Einstein summation convention, where repeated indices are summed over their allowable range. We can write

ρ=yiyi2yi Aikck+ci ATik Aklcl

Taking the partial derivative, we have

ρcj=2yi Aikckcj+cicj ATik Aklcl+ci ATik Aklclcj

Now,

cicj={1, if i=j0, otherwise 

Therefore,

ρcj=2yi Aij+ATjk Aklcl+ci ATik Akj

Now,

ci ATik Akj=ci Aki Akj=Akj Akici=ATjk Akici=ATjk Aklcl

Therefore,

ρcj=2yi Aij+2 ATjk Aklcl

With the partials set equal to zero, we have

ATjk Aklcl=yi Aij

or

ATjk Aklcl=ATjiyi

In vector notation, we have

AT Ac=ATy.

Equation (4.2) is the so-called normal equation, and can be solved for c by Gaussian elimination using the MATLAB backslash operator. After constructing the matrix A given by (4.1), and the vector y from the data, one can code in MATLAB

c=(AA)(Ay)

But in fact the MATLAB back slash operator will automatically solve the normal equations when the matrix A is not square, so that the MATLAB code

c=Ay

yields the same result.

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Chapter 5

Interpolation

Consider the following problem: Given the values of a known function y=f(x) at a sequence of ordered points x0,x1,,xn, find f(x) for arbitrary x. When x0 xxn, the problem is called interpolation. When x<x0 or x>xn the problem is called extrapolation.

With yi=f(xi), the problem of interpolation is basically one of drawing a smooth curve through the known points (x0,y0),(x1,y1),,(xn,yn). This is not the same problem as drawing a smooth curve that approximates a set of data points that have experimental error. This latter problem is called least-squares approximation.

Here, we will consider three interpolation algorithms: (1) polynomial interpolation; (2) piecewise linear interpolation, and; (3) cubic spline interpolation.

Polynomial interpolation

The n+1 points (x0,y0),(x1,y1),,(xn,yn) can be interpolated by a unique polynomial of degree n. When n=1, the polynomial is a linear function; when n=2, the polynomial is a quadratic function. There are three standard algorithms that can be used to construct this unique interpolating polynomial, and we will present all three here, not so much because they are all useful, but because it is interesting to learn how these three algorithms are constructed.

When discussing each algorithm, we define Pn(x) to be the unique nth degree polynomial that passes through the given n+1 data points.

Vandermonde polynomial

This Vandermonde polynomial is the most straightforward construction of the interpolating polynomial Pn(x). We simply write

Pn(x)=c0xn+c1xn1++cn.

Then we can immediately form n+1 linear equations for the n+1 unknown coefficients c0,c1,,cn using the n+1 known points:

y0=c0xn0+c1xn10++cn1x0+cny2=c0xn1+c1xn11++cn1x1+cnyn=c0xnn+c1xn1n++cn1xn+cn

The system of equations in matrix form is

(xn0xn10x01xn1xn11x11xnnxn1nxn1)(c0c1cn)=(y0y1yn)

The matrix is called the Vandermonde matrix, and can be constructed using the MATLAB function vander.m. The system of linear equations can be solved in MATLAB using the \operator, and the MATLAB function polyval.m can used to interpolate using the c coefficients. I will illustrate this in class and place the code on the website.

Lagrange polynomial

The Lagrange polynomial is the most clever construction of the interpolating polynomial Pn(x), and leads directly to an analytical formula. The Lagrange polynomial is the sum of n+1 terms and each term is itself a polynomial of degree n. The full polynomial is therefore of degree n. Counting from 0 , the i th term of the Lagrange polynomial is constructed by requiring it to be zero at xj with ji, and equal to yi when j=i. The polynomial can be written as

Pn(x)=(xx1)(xx2)(xxn)y0(x0x1)(x0x2)(x0xn)+(xx0)(xx2)(xxn)y1(x1x0)(x1x2)(x1xn)++(xx0)(xx1)(xxn1)yn(xnx0)(xnx1)(xnxn1).

It can be clearly seen that the first term is equal to zero when x=x1,x2,,xn and equal to y0 when x=x0; the second term is equal to zero when x=x0,x2,xn and equal to y1 when x=x1; and the last term is equal to zero when x=x0,x1,xn1 and equal to yn when x=xn. The uniqueness of the interpolating polynomial implies that the Lagrange polynomial must be the interpolating polynomial.

Newton polynomial

The Newton polynomial is somewhat more clever than the Vandermonde polynomial because it results in a system of linear equations that is lower triangular, and therefore can be solved by forward substitution. The interpolating polynomial is written in the form

Pn(x)=c0+c1(xx0)+c2(xx0)(xx1)++cn(xx0)(xxn1)

which is clearly a polynomial of degree n. The n+1 unknown coefficients given by the c s can be found by substituting the points (xi,yi) for i=0,,n :

y0=c0y1=c0+c1(x1x0)y2=c0+c1(x2x0)+c2(x2x0)(x2x1)yn=c0+c1(xnx0)+c2(xnx0)(xnx1)++cn(xnx0)(xnxn1)

This system of linear equations is lower triangular as can be seen from the matrix form

(10001(x1x0)001(xnx0)(xnx0)(xnx1)(xnx0)(xnxn1))(c0c1cn)

and so theoretically can be solved faster than the Vandermonde polynomial. In practice, however, there is little difference because polynomial interpolation is only useful when the number of points to be interpolated is small.

Piecewise linear interpolation

Instead of constructing a single global polynomial that goes through all the points, one can construct local polynomials that are then connected together. In the the section following this one, we will discuss how this may be done using cubic polynomials. Here, we discuss the simpler case of linear polynomials. This is the default interpolation typically used when plotting data.

Suppose the interpolating function is y=g(x), and as previously, there are n+1 points to interpolate. We construct the function g(x) out of n local linear polynomials. We write

g(x)=g_{i}(x), \quad \text { for } x_{i} \leq x \leq x_{i+1} \nonumber

where

g_{i}(x)=a_{i}\left(x-x_{i}\right)+b_{i} \nonumber

and i=0,1, \ldots, n-1.

We now require y=g_{i}(x) to pass through the endpoints \left(x_{i}, y_{i}\right) and \left(x_{i+1}, y_{i+1}\right). We have

\begin{aligned} y_{i} &=b_{i} \\ y_{i+1} &=a_{i}\left(x_{i+1}-x_{i}\right)+b_{i} . \end{aligned} \nonumber

Therefore, the coefficients of g_{i}(x) are determined to be

a_{i}=\frac{y_{i+1}-y_{i}}{x_{i+1}-x_{i}}, \quad b_{i}=y_{i} \nonumber

Although piecewise linear interpolation is widely used, particularly in plotting routines, it suffers from a discontinuity in the derivative at each point. This results in a function which may not look smooth if the points are too widely spaced. We next consider a more challenging algorithm that uses cubic polynomials.

Cubic spline interpolation

The n+1 points to be interpolated are again

\left(x_{0}, y_{0}\right),\left(x_{1}, y_{1}\right), \ldots\left(x_{n}, y_{n}\right) \nonumber

Here, we use n piecewise cubic polynomials for interpolation,

g_{i}(x)=a_{i}\left(x-x_{i}\right)^{3}+b_{i}\left(x-x_{i}\right)^{2}+c_{i}\left(x-x_{i}\right)+d_{i}, \quad i=0,1, \ldots, n-1, \nonumber

with the global interpolation function written as

g(x)=g_{i}(x), \quad \text { for } x_{i} \leq x \leq x_{i+1} . \nonumber

To achieve a smooth interpolation we impose that g(x) and its first and second derivatives are continuous. The requirement that g(x) is continuous (and goes through all n+1 points) results in the two constraints

\begin{gathered} g_{i}\left(x_{i}\right)=y_{i}, \quad i=0 \text { to } n-1 \\ g_{i}\left(x_{i+1}\right)=y_{i+1}, \quad i=0 \text { to } n-1 \end{gathered} \nonumber

The requirement that g^{\prime}(x) is continuous results in

g_{i}^{\prime}\left(x_{i+1}\right)=g_{i+1}^{\prime}\left(x_{i+1}\right), \quad i=0 \text { to } n-2 \nonumber

And the requirement that g^{\prime \prime}(x) is continuous results in

g_{i}^{\prime \prime}\left(x_{i+1}\right)=g_{i+1}^{\prime \prime}\left(x_{i+1}\right), \quad i=0 \text { to } n-2 \nonumber

There are n cubic polynomials g_{i}(x) and each cubic polynomial has four free coefficients; there are therefore a total of 4 n unknown coefficients. The number of constraining equations from (5.1)-(5.4) is 2 n+2(n-1)=4 n-2. With 4 n-2 constraints and 4 n unknowns, two more conditions are required for a unique solution. These are usually chosen to be extra conditions on the first g_{0}(x) and last g_{n-1}(x) polynomials. We will discuss these extra conditions later.

We now proceed to determine equations for the unknown coefficients of the cubic polynomials. The polynomials and their first two derivatives are given by

\begin{aligned} g_{i}(x) &=a_{i}\left(x-x_{i}\right)^{3}+b_{i}\left(x-x_{i}\right)^{2}+c_{i}\left(x-x_{i}\right)+d_{i} \\ g_{i}^{\prime}(x) &=3 a_{i}\left(x-x_{i}\right)^{2}+2 b_{i}\left(x-x_{i}\right)+c_{i} \\ g_{i}^{\prime \prime}(x) &=6 a_{i}\left(x-x_{i}\right)+2 b_{i} \end{aligned} \nonumber

We will consider the four conditions (5.1)-(5.4) in turn. From (5.1) and (5.5), we have

d_{i}=y_{i}, \quad i=0 \text { to } n-1, \nonumber

which directly solves for all of the d-coefficients.

To satisfy (5.2), we first define

h_{i}=x_{i+1}-x_{i} \nonumber

and

f_{i}=y_{i+1}-y_{i} \nonumber

Now, from (5.2) and (5.5), using (5.8), we obtain the n equations

a_{i} h_{i}^{3}+b_{i} h_{i}^{2}+c_{i} h_{i}=f_{i}, \quad i=0 \text { to } n-1 \nonumber

From (5.3) and (5.6) we obtain the n-1 equations

3 a_{i} h_{i}^{2}+2 b_{i} h_{i}+c_{i}=c_{i+1}, \quad i=0 \text { to } n-2 \nonumber

From (5.4) and (5.7) we obtain the n-1 equations

3 a_{i} h_{i}+b_{i}=b_{i+1} \quad i=0 \text { to } n-2 \nonumber

It is will be useful to include a definition of the coefficient b_{n}, which is now missing. (The index of the cubic polynomial coefficients only go up to n-1 . ) We simply extend (5.11) up to i=n-1 and so write

3 a_{n-1} h_{n-1}+b_{n-1}=b_{n} \nonumber

which can be viewed as a definition of b_{n}.

We now proceed to eliminate the sets of a - and c-coefficients (with the d-coefficients already eliminated in (5.8)) to find a system of linear equations for the b-coefficients. From (5.11) and (5.12), we can solve for the n a-coefficients to find

a_{i}=\frac{1}{3 h_{i}}\left(b_{i+1}-b_{i}\right), \quad i=0 \text { to } n-1 \nonumber

From (5.9), we can solve for the n c-coefficients as follows:

\begin{aligned} c_{i} &=\frac{1}{h_{i}}\left(f_{i}-a_{i} h_{i}^{3}-b_{i} h_{i}^{2}\right) \\ &=\frac{1}{h_{i}}\left(f_{i}-\frac{1}{3 h_{i}}\left(b_{i+1}-b_{i}\right) h_{i}^{3}-b_{i} h_{i}^{2}\right) \\ &=\frac{f_{i}}{h_{i}}-\frac{1}{3} h_{i}\left(b_{i+1}+2 b_{i}\right), \quad i=0 \text { to } n-1 . \end{aligned} \nonumber

We can now find an equation for the b-coefficients by substituting (5.8), (5.13) and (5.14) into (5.10) :

\begin{gathered} 3\left(\frac{1}{3 h_{i}}\left(b_{i+1}-b_{i}\right)\right) h_{i}^{2}+2 b_{i} h_{i}+\left(\frac{f_{i}}{h_{i}}-\frac{1}{3} h_{i}\left(b_{i+1}+2 b_{i}\right)\right) \\ =\left(\frac{f_{i+1}}{h_{i+1}}-\frac{1}{3} h_{i+1}\left(b_{i+2}+2 b_{i+1}\right)\right) \end{gathered} \nonumber

which simplifies to

\frac{1}{3} h_{i} b_{i}+\frac{2}{3}\left(h_{i}+h_{i+1}\right) b_{i+1}+\frac{1}{3} h_{i+1} b_{i+2}=\frac{f_{i+1}}{h_{i+1}}-\frac{f_{i}}{h_{i}} \nonumber

an equation that is valid for i=0 to n-2. Therefore, (5.15) represent n-1 equations for the n+1 unknown b-coefficients. Accordingly, we write the matrix equa- tion for the b-coefficients, leaving the first and last row absent, as

\left(\begin{array}{cccccccc} \cdots & \cdots & \cdots & \cdots & \text { missing } & \cdots & \cdots \\ \frac{1}{3} h_{0} & \frac{2}{3}\left(h_{0}+h_{1}\right) & \frac{1}{3} h_{1} & \cdots & 0 & 0 & 0 \\ \vdots & \vdots & \vdots & \ddots & \vdots & \vdots & \vdots \\ 0 & 0 & 0 & \cdots & \frac{1}{3} h_{n-2} & \frac{2}{3}\left(h_{n-2}+h_{n-1}\right) & \frac{1}{3} h_{n-1} \\ \cdots & \cdots & \cdots & \cdots & \text { missing } & \cdots & \cdots \end{array}\right)\left(\begin{array}{c} b_{0} \\ b_{1} \\ \vdots \\ b_{n-1} \\ b_{n} \end{array}\right)\left(\begin{array}{c} \operatorname{missing} \\ \frac{f_{1}}{h_{1}}-\frac{f_{0}}{h_{0}} \\ \vdots \\ \frac{f_{n-1}}{h_{n-1}}-\frac{f_{n-2}}{h_{n-2}} \\ \operatorname{missing} \end{array}\right) \nonumber

Once the missing first and last equations are specified, the matrix equation for the b-coefficients can be solved by Gaussian elimination. And once the b-coefficients are determined, the a - and c-coefficients can also be determined from (5.13) and (5.14), with the d-coefficients already known from (5.8). The piecewise cubic polynomials, then, are known and g(x) can be used for interpolation to any value x satisfying x_{0} \leq x \leq x_{n}

The missing first and last equations can be specified in several ways, and here we show the two ways that are allowed by the MATLAB function spline.m. The first way should be used when the derivative g^{\prime}(x) is known at the endpoints x_{0} and x_{n}; that is, suppose we know the values of \alpha and \beta such that

g_{0}^{\prime}\left(x_{0}\right)=\alpha, \quad g_{n-1}^{\prime}\left(x_{n}\right)=\beta . \nonumber

From the known value of \alpha, and using (5.6) and (5.14), we have

\begin{aligned} \alpha &=c_{0} \\ &=\frac{f_{0}}{h_{0}}-\frac{1}{3} h_{0}\left(b_{1}+2 b_{0}\right) \end{aligned} \nonumber

Therefore, the missing first equation is determined to be

\frac{2}{3} h_{0} b_{0}+\frac{1}{3} h_{0} b_{1}=\frac{f_{0}}{h_{0}}-\alpha . \nonumber

From the known value of \beta, and using (5.6),(5.13), and (5.14), we have

\begin{aligned} \beta &=3 a_{n-1} h_{n-1}^{2}+2 b_{n-1} h_{n-1}+c_{n-1} \\ &=3\left(\frac{1}{3 h_{n-1}}\left(b_{n}-b_{n-1}\right)\right) h_{n-1}^{2}+2 b_{n-1} h_{n-1}+\left(\frac{f_{n-1}}{h_{n-1}}-\frac{1}{3} h_{n-1}\left(b_{n}+2 b_{n-1}\right)\right), \end{aligned} \nonumber

which simplifies to

\frac{1}{3} h_{n-1} b_{n-1}+\frac{2}{3} h_{n-1} b_{n}=\beta-\frac{f_{n-1}}{h_{n-1}} \nonumber

to be used as the missing last equation.

The second way of specifying the missing first and last equations is called the not- a-knot condition, which assumes that

g_{0}(x)=g_{1}(x), \quad g_{n-2}(x)=g_{n-1}(x) \nonumber

Considering the first of these equations, from (5.5) we have

\begin{aligned} a_{0}\left(x-x_{0}\right)^{3}+b_{0}\left(x-x_{0}\right)^{2}+c_{0}(x&\left.-x_{0}\right)+d_{0} \\ &=a_{1}\left(x-x_{1}\right)^{3}+b_{1}\left(x-x_{1}\right)^{2}+c_{1}\left(x-x_{1}\right)+d_{1} \end{aligned} \nonumber

Now two cubic polynomials can be proven to be identical if at some value of x, the polynomials and their first three derivatives are identical. Our conditions of continuity at x=x_{1} already require that at this value of x these two polynomials and their first two derivatives are identical. The polynomials themselves will be identical, then, if their third derivatives are also identical at x=x_{1}, or if

a_{0}=a_{1} \nonumber

From (5.13), we have

\frac{1}{3 h_{0}}\left(b_{1}-b_{0}\right)=\frac{1}{3 h_{1}}\left(b_{2}-b_{1}\right) \nonumber

or after simplification

h_{1} b_{0}-\left(h_{0}+h_{1}\right) b_{1}+h_{0} b_{2}=0 \nonumber

which provides us our missing first equation. A similar argument at x=x_{n}-1 also provides us with our last equation,

h_{n-1} b_{n-2}-\left(h_{n-2}+h_{n-1}\right) b_{n-1}+h_{n-2} b_{n}=0 . \nonumber

The MATLAB subroutines spline.m and ppval.m can be used for cubic spline interpolation (see also interp1.m). I will illustrate these routines in class and post sample code on the course web site.

Multidimensional interpolation

Suppose we are interpolating the value of a function of two variables,

z=f(x, y) \nonumber

The known values are given by

z_{i j}=f\left(x_{i}, y_{j}\right) \nonumber

with i=0,1, \ldots, n and j=0,1, \ldots, n. Note that the (x, y) points at which f(x, y) are known lie on a grid in the x-y plane.

Let z=g(x, y) be the interpolating function, satisfying z_{i j}=g\left(x_{i}, y_{j}\right) . A twodimensional interpolation to find the value of g at the point (x, y) may be done by first performing n+1 one-dimensional interpolations in y to find the value of g at the n+1 points \left(x_{0}, y\right),\left(x_{1}, y\right), \ldots,\left(x_{n}, y\right), followed by a single one-dimensional interpolation in x to find the value of g at (x, y).

In other words, two-dimensional interpolation on a grid of dimension (n+1) \times (n+1) is done by first performing n+1 one-dimensional interpolations to the value y followed by a single one-dimensional interpolation to the value x. Twodimensional interpolation can be generalized to higher dimensions. The MATLAB functions to perform two-and three-dimensional interpolation are interp2.m and interp3.m. 5.4. MULTIDIMENSIONAL INTERPOLATION

Chapter 6

Integration

We want to construct numerical algorithms that can perform definite integrals of the form

I=\int_{a}^{b} f(x) d x \nonumber

Calculating these definite integrals numerically is called numerical integration, numerical quadrature, or more simply quadrature.

Elementary formulas

We first consider integration from 0 to h, with h small, to serve as the building blocks for integration over larger domains. We here define I_{h} as the following integral:

I_{h}=\int_{0}^{h} f(x) d x . \nonumber

To perform this integral, we consider a Taylor series expansion of f(x) about the value x=h / 2 :

\begin{aligned} f(x)=f(h / 2)+(x-h / 2) f^{\prime} &(h / 2)+\frac{(x-h / 2)^{2}}{2} f^{\prime \prime}(h / 2) \\ &+\frac{(x-h / 2)^{3}}{6} f^{\prime \prime \prime}(h / 2)+\frac{(x-h / 2)^{4}}{24} f^{\prime \prime \prime \prime}(h / 2)+\ldots \end{aligned} \nonumber

Midpoint rule

The midpoint rule makes use of only the first term in the Taylor series expansion. Here, we will determine the error in this approximation. Integrating,

\begin{aligned} I_{h}=h f(h / 2)+\int_{0}^{h}(&(x-h / 2) f^{\prime}(h / 2)+\frac{(x-h / 2)^{2}}{2} f^{\prime \prime}(h / 2) \\ &\left.+\frac{(x-h / 2)^{3}}{6} f^{\prime \prime \prime}(h / 2)+\frac{(x-h / 2)^{4}}{24} f^{\prime \prime \prime \prime}(h / 2)+\ldots\right) d x . \end{aligned} \nonumber

Changing variables by letting y=x-h / 2 and d y=d x, and simplifying the integral depending on whether the integrand is even or odd, we have

\begin{aligned} I_{h}=& h f(h / 2) \\ &+\int_{-h / 2}^{h / 2}\left(y f^{\prime}(h / 2)+\frac{y^{2}}{2} f^{\prime \prime}(h / 2)+\frac{y^{3}}{6} f^{\prime \prime \prime}(h / 2)+\frac{y^{4}}{24} f^{\prime \prime \prime \prime}(h / 2)+\ldots\right) d y \\ =& h f(h / 2)+\int_{0}^{h / 2}\left(y^{2} f^{\prime \prime}(h / 2)+\frac{y^{4}}{12} f^{\prime \prime \prime \prime}(h / 2)+\ldots\right) d y \end{aligned} \nonumber

The integrals that we need here are

\int_{0}^{\frac{h}{2}} y^{2} d y=\frac{h^{3}}{24}, \quad \int_{0}^{\frac{h}{2}} y^{4} d y=\frac{h^{5}}{160} \nonumber

Therefore,

I_{h}=h f(h / 2)+\frac{h^{3}}{24} f^{\prime \prime}(h / 2)+\frac{h^{5}}{1920} f^{\prime \prime \prime \prime}(h / 2)+\ldots \nonumber

Trapezoidal rule

From the Taylor series expansion of f(x) about x=h / 2, we have

f(0)=f(h / 2)-\frac{h}{2} f^{\prime}(h / 2)+\frac{h^{2}}{8} f^{\prime \prime}(h / 2)-\frac{h^{3}}{48} f^{\prime \prime \prime}(h / 2)+\frac{h^{4}}{384} f^{\prime \prime \prime \prime}(h / 2)+\ldots, \nonumber

and

f(h)=f(h / 2)+\frac{h}{2} f^{\prime}(h / 2)+\frac{h^{2}}{8} f^{\prime \prime}(h / 2)+\frac{h^{3}}{48} f^{\prime \prime \prime}(h / 2)+\frac{h^{4}}{384} f^{\prime \prime \prime \prime}(h / 2)+\ldots \ldots \nonumber

Adding and multiplying by h / 2 we obtain

\frac{h}{2}(f(0)+f(h))=h f(h / 2)+\frac{h^{3}}{8} f^{\prime \prime}(h / 2)+\frac{h^{5}}{384} f^{\prime \prime \prime \prime}(h / 2)+\ldots . \nonumber

We now substitute for the first term on the right-hand-side using the midpoint rule formula:

\begin{array}{r} \frac{h}{2}(f(0)+f(h))=\left(I_{h}-\frac{h^{3}}{24} f^{\prime \prime}(h / 2)-\frac{h^{5}}{1920} f^{\prime \prime \prime \prime}(h / 2)\right) \\ +\frac{h^{3}}{8} f^{\prime \prime}(h / 2)+\frac{h^{5}}{384} f^{\prime \prime \prime \prime}(h / 2)+\ldots, \end{array} \nonumber

and solving for I_{h}, we find

I_{h}=\frac{h}{2}(f(0)+f(h))-\frac{h^{3}}{12} f^{\prime \prime}(h / 2)-\frac{h^{5}}{480} f^{\prime \prime \prime \prime}(h / 2)+\ldots \nonumber

Simpson’s rule

To obtain Simpson’s rule, we combine the midpoint and trapezoidal rule to eliminate the error term proportional to h^{3}. Multiplying (6.3) by two and adding to (6.4), we obtain

3 I_{h}=h\left(2 f(h / 2)+\frac{1}{2}(f(0)+f(h))\right)+h^{5}\left(\frac{2}{1920}-\frac{1}{480}\right) f^{\prime \prime \prime \prime}(h / 2)+\ldots, \nonumber

or

I_{h}=\frac{h}{6}(f(0)+4 f(h / 2)+f(h))-\frac{h^{5}}{2880} f^{\prime \prime \prime \prime}(h / 2)+\ldots . \nonumber

Usually, Simpson’s rule is written by considering the three consecutive points 0, h and 2 h. Substituting h \rightarrow 2 h, we obtain the standard result

I_{2 h}=\frac{h}{3}(f(0)+4 f(h)+f(2 h))-\frac{h^{5}}{90} f^{\prime \prime \prime \prime}(h)+\ldots \nonumber

Composite rules

We now use our elementary formulas obtained for (6.2) to perform the integral given by (6.1)

Trapezoidal rule

We suppose that the function f(x) is known at the n+1 points labeled as x_{0}, x_{1}, \ldots, x_{n}, with the endpoints given by x_{0}=a and x_{n}=b. Define

f_{i}=f\left(x_{i}\right), \quad h_{i}=x_{i+1}-x_{i} \nonumber

Then the integral of (6.1) may be decomposed as

\begin{aligned} \int_{a}^{b} f(x) d x &=\sum_{i=0}^{n-1} \int_{x_{i}}^{x_{i+1}} f(x) d x \\ &=\sum_{i=0}^{n-1} \int_{0}^{h_{i}} f\left(x_{i}+s\right) d s \end{aligned} \nonumber

where the last equality arises from the change-of-variables s=x-x_{i}. Applying the trapezoidal rule to the integral, we have

\int_{a}^{b} f(x) d x=\sum_{i=0}^{n-1} \frac{h_{i}}{2}\left(f_{i}+f_{i+1}\right) \nonumber

If the points are not evenly spaced, say because the data are experimental values, then the h_{i} may differ for each value of i and (6.6) is to be used directly.

However, if the points are evenly spaced, say because f(x) can be computed, we have h_{i}=h, independent of i. We can then define

x_{i}=a+i h, \quad i=0,1, \ldots, n \nonumber

and since the end point b satisfies b=a+n h, we have

h=\frac{b-a}{n} \nonumber

The composite trapezoidal rule for evenly space points then becomes

\begin{aligned} \int_{a}^{b} f(x) d x &=\frac{h}{2} \sum_{i=0}^{n-1}\left(f_{i}+f_{i+1}\right) \\ &=\frac{h}{2}\left(f_{0}+2 f_{1}+\cdots+2 f_{n-1}+f_{n}\right) \end{aligned} \nonumber

The first and last terms have a multiple of one; all other terms have a multiple of two; and the entire sum is multiplied by h / 2.

Simpson’s rule

We here consider the composite Simpson’s rule for evenly space points. We apply Simpson’s rule over intervals of 2 h, starting from a and ending at b :

\begin{aligned} \int_{a}^{b} f(x) d x=\frac{h}{3}\left(f_{0}+4 f_{1}+f_{2}\right)+\frac{h}{3}\left(f_{2}+4 f_{3}+f_{4}\right)+& \ldots \\ &+\frac{h}{3}\left(f_{n-2}+4 f_{n-1}+f_{n}\right) \end{aligned} \nonumber

Note that n must be even for this scheme to work. Combining terms, we have

\int_{a}^{b} f(x) d x=\frac{h}{3}\left(f_{0}+4 f_{1}+2 f_{2}+4 f_{3}+2 f_{4}+\cdots+4 f_{n-1}+f_{n}\right) \nonumber

The first and last terms have a multiple of one; the even indexed terms have a multiple of 2 ; the odd indexed terms have a multiple of 4 ; and the entire sum is multiplied by h / 3.

Local versus global error

Consider the elementary formula (6.4) for the trapezoidal rule, written in the form

\int_{0}^{h} f(x) d x=\frac{h}{2}(f(0)+f(h))-\frac{h^{3}}{12} f^{\prime \prime}(\xi) \nonumber

where \xi is some value satisfying 0 \leq \xi \leq h, and we have used Taylor’s theorem with the mean-value form of the remainder. We can also represent the remainder as

-\frac{h^{3}}{12} f^{\prime \prime}(\xi)=\mathrm{O}\left(h^{3}\right) \nonumber

where \mathrm{O}\left(h^{3}\right) signifies that when h is small, halving of the grid spacing h decreases the error in the elementary trapezoidal rule by a factor of eight. We call the terms represented by \mathrm{O}\left(h^{3}\right) the Local Error.

More important is the Global Error which is obtained from the composite formula (6.7) for the trapezoidal rule. Putting in the remainder terms, we have

\int_{a}^{b} f(x) d x=\frac{h}{2}\left(f_{0}+2 f_{1}+\cdots+2 f_{n-1}+f_{n}\right)-\frac{h^{3}}{12} \sum_{i=0}^{n-1} f^{\prime \prime}\left(\xi_{i}\right) \nonumber

where \xi_{i} are values satisfying x_{i} \leq \xi_{i} \leq x_{i+1}. The remainder can be rewritten as

-\frac{h^{3}}{12} \sum_{i=0}^{n-1} f^{\prime \prime}\left(\xi_{i}\right)=-\frac{n h^{3}}{12}\left\langle f^{\prime \prime}\left(\xi_{i}\right)\right\rangle \nonumber

where \left\langle f^{\prime \prime}\left(\xi_{i}\right)\right\rangle is the average value of all the f^{\prime \prime}\left(\xi_{i}\right)^{\prime} s. Now,

n=\frac{b-a}{h} \nonumber

so that the error term becomes

\begin{aligned} -\frac{n h^{3}}{12}\left\langle f^{\prime \prime}\left(\xi_{i}\right)\right\rangle &=-\frac{(b-a) h^{2}}{12}\left\langle f^{\prime \prime}\left(\xi_{i}\right)\right\rangle \\ &=\mathrm{O}\left(h^{2}\right) \end{aligned} \nonumber

Therefore, the global error is \mathrm{O}\left(h^{2}\right). That is, a halving of the grid spacing only decreases the global error by a factor of four.

Similarly, Simpson’s rule has a local error of \mathrm{O}\left(h^{5}\right) and a global error of \mathrm{O}\left(h^{4}\right).

image

Figure 6.1: Adaptive Simpson quadrature: Level 1 .

Adaptive integration

The useful MATLAB function quad.m performs numerical integration using adaptive Simpson quadrature. The idea is to let the computation itself decide on the grid size required to achieve a certain level of accuracy. Moreover, the grid size need not be the same over the entire region of integration.

We begin the adaptive integration at what is called Level 1 . The uniformly spaced points at which the function f(x) is to be evaluated are shown in Fig. 6.1. The distance between the points a and b is taken to be 2 h, so that

h=\frac{b-a}{2} \nonumber

Integration using Simpson’s rule (6.5) with grid size h yields

I=\frac{h}{3}(f(a)+4 f(c)+f(b))-\frac{h^{5}}{90} f^{\prime \prime \prime \prime}(\xi) \nonumber

where \xi is some value satisfying a \leq \xi \leq b.

Integration using Simpson’s rule twice with grid size h / 2 yields

I=\frac{h}{6}(f(a)+4 f(d)+2 f(c)+4 f(e)+f(b))-\frac{(h / 2)^{5}}{90} f^{\prime \prime \prime \prime}\left(\xi_{l}\right)-\frac{(h / 2)^{5}}{90} f^{\prime \prime \prime \prime}\left(\xi_{r}\right) \nonumber

with \xi_{l} and \xi_{r} some values satisfying a \leq \xi_{l} \leq c and c \leq \xi_{r} \leq b.

We now define

\begin{aligned} &S_{1}=\frac{h}{3}(f(a)+4 f(c)+f(b)) \\ &S_{2}=\frac{h}{6}(f(a)+4 f(d)+2 f(c)+4 f(e)+f(b)), \\ &E_{1}=-\frac{h^{5}}{90} f^{\prime \prime \prime \prime}(\xi), \\ &E_{2}=-\frac{h^{5}}{2^{5} \cdot 90}\left(f^{\prime \prime \prime \prime}\left(\xi_{l}\right)+f^{\prime \prime \prime \prime}\left(\xi_{r}\right)\right) . \end{aligned} \nonumber

Now we ask whether S_{2} is accurate enough, or must we further refine the calculation and go to Level 2? To answer this question, we make the simplifying approximation that all of the fourth-order derivatives of f(x) in the error terms are equal; that is,

f^{\prime \prime \prime \prime}(\xi)=f^{\prime \prime \prime \prime}\left(\xi_{l}\right)=f^{\prime \prime \prime \prime}\left(\xi_{r}\right)=C . \nonumber

CHAPTER 6. INTEGRATION

Then

\begin{aligned} &E_{1}=-\frac{h^{5}}{90} C \\ &E_{2}=-\frac{h^{5}}{2^{4} \cdot 90} C=\frac{1}{16} E_{1} \end{aligned} \nonumber

Then since

S_{1}+E_{1}=S_{2}+E_{2} \nonumber

and

E_{1}=16 E_{2} \nonumber

we have for our estimate for the error term E_{2},

E_{2}=\frac{1}{15}\left(S_{2}-S_{1}\right) \nonumber

Therefore, given some specific value of the tolerance tol, if

\left|\frac{1}{15}\left(S_{2}-S_{1}\right)\right|<\text { tol } \nonumber

then we can accept S_{2} as I. If the tolerance is not achieved for I, then we proceed to Level 2 .

The computation at Level 2 further divides the integration interval from a to b into the two integration intervals a to c and c to b, and proceeds with the above procedure independently on both halves. Integration can be stopped on either half provided the tolerance is less than tol/2 (since the sum of both errors must be less than tol). Otherwise, either half can proceed to Level 3, and so on.

As a side note, the two values of I given above (for integration with step size h and h / 2 ) can be combined to give a more accurate value for I given by

I=\frac{16 S_{2}-S_{1}}{15}+\mathrm{O}\left(h^{7}\right) \nonumber

where the error terms of \mathrm{O}\left(h^{5}\right) approximately cancel. This free lunch, so to speak, is called Richardson’s extrapolation.

Chapter 7

Ordinary differential equations

We now discuss the numerical solution of ordinary differential equations. These include the initial value problem, the boundary value problem, and the eigenvalue problem. Before proceeding to the development of numerical methods, we review the analytical solution of some classic equations.

Examples of analytical solutions

Initial value problem

One classic initial value problem is the R C circuit. With R the resistor and C the capacitor, the differential equation for the charge q on the capacitor is given by

R \frac{d q}{d t}+\frac{q}{C}=0 . \nonumber

If we consider the physical problem of a charged capacitor connected in a closed circuit to a resistor, then the initial condition is q(0)=q_{0}, where q_{0} is the initial charge on the capacitor.

The differential equation (7.1) is separable, and separating and integrating from time t=0 to t yields

\int_{q_{0}}^{q} \frac{d q}{q}=-\frac{1}{R C} \int_{0}^{t} d t \nonumber

which can be integrated and solved for q=q(t) :

q(t)=q_{0} e^{-t / R C} . \nonumber

The classic second-order initial value problem is the R L C circuit, with differential equation

L \frac{d^{2} q}{d t^{2}}+R \frac{d q}{d t}+\frac{q}{C}=0 . \nonumber

Here, a charged capacitor is connected to a closed circuit, and the initial conditions satisfy

q(0)=q_{0}, \quad \frac{d q}{d t}(0)=0 \nonumber

The solution is obtained for the second-order equation by the ansatz

q(t)=e^{r t} \nonumber

which results in the following so-called characteristic equation for r :

L r^{2}+R r+\frac{1}{C}=0 \nonumber

If the two solutions for r are distinct and real, then the two found exponential solutions can be multiplied by constants and added to form a general solution. The constants can then be determined by requiring the general solution to satisfy the two initial conditions. If the roots of the characteristic equation are complex or degenerate, a general solution to the differential equation can also be found.

Boundary value problems

The dimensionless equation for the temperature y=y(x) along a linear heatconducting rod of length unity, and with an applied external heat source f(x), is given by the differential equation

-\frac{d^{2} y}{d x^{2}}=f(x) \nonumber

with 0 \leq x \leq 1. Boundary conditions are usually prescribed at the end points of the rod, and here we assume that the temperature at both ends are maintained at zero so that

y(0)=0, \quad y(1)=0 \nonumber

The assignment of boundary conditions at two separate points is called a twopoint boundary value problem, in contrast to the initial value problem where the boundary conditions are prescribed at only a single point. Two-point boundary value problems typically require a more sophisticated algorithm for a numerical solution than initial value problems.

Here, the solution of (7.2) can proceed by integration once f(x) is specified. We assume that

f(x)=x(1-x) \nonumber

so that the maximum of the heat source occurs in the center of the rod, and goes to zero at the ends.

The differential equation can then be written as

\frac{d^{2} y}{d x^{2}}=-x(1-x) \nonumber

The first integration results in

\begin{aligned} \frac{d y}{d x} &=\int\left(x^{2}-x\right) d x \\ &=\frac{x^{3}}{3}-\frac{x^{2}}{2}+c_{1} \end{aligned} \nonumber

where c_{1} is the first integration constant. Integrating again,

\begin{aligned} y(x) &=\int\left(\frac{x^{3}}{3}-\frac{x^{2}}{2}+c_{1}\right) d x \\ &=\frac{x^{4}}{12}-\frac{x^{3}}{6}+c_{1} x+c_{2} \end{aligned} \nonumber

where c_{2} is the second integration constant. The two integration constants are determined by the boundary conditions. At x=0, we have

0=c_{2} \nonumber

and at x=1, we have

0=\frac{1}{12}-\frac{1}{6}+c_{1} \nonumber

so that c_{1}=1 / 12. Our solution is therefore

\begin{aligned} y(x) &=\frac{x^{4}}{12}-\frac{x^{3}}{6}+\frac{x}{12} \\ &=\frac{1}{12} x(1-x)\left(1+x-x^{2}\right) \end{aligned} \nonumber

The temperature of the rod is maximum at x=1 / 2 and goes smoothly to zero at the ends.

Eigenvalue problem

The classic eigenvalue problem obtained by solving the wave equation by separation of variables is given by

\frac{d^{2} y}{d x^{2}}+\lambda^{2} y=0 \nonumber

with the two-point boundary conditions y(0)=0 and y(1)=0. Notice that y(x)=0 satisfies both the differential equation and the boundary conditions. Other nonzero solutions for y=y(x) are possible only for certain discrete values of \lambda. These values of \lambda are called the eigenvalues of the differential equation.

We proceed by first finding the general solution to the differential equation. It is easy to see that this solution is

y(x)=A \cos \lambda x+B \sin \lambda x \nonumber

Imposing the first boundary condition at x=0, we obtain

A=0 \nonumber

The second boundary condition at x=1 results in

B \sin \lambda=0 \nonumber

Since we are searching for a solution where y=y(x) is not identically zero, we must have

\lambda=\pi, 2 \pi, 3 \pi, \ldots \nonumber

The corresponding negative values of \lambda are also solutions, but their inclusion only changes the corresponding values of the unknown B constant. A linear superposition of all the solutions results in the general solution

y(x)=\sum_{n=1}^{\infty} B_{n} \sin n \pi x . \nonumber

For each eigenvalue n \pi, we say there is a corresponding eigenfunction \sin n \pi x. When the differential equation can not be solved analytically, a numerical method should be able to solve for both the eigenvalues and eigenfunctions.

Numerical methods: initial value problem

We begin with the simple Euler method, then discuss the more sophisticated RungeKutta methods, and conclude with the Runge-Kutta-Fehlberg method, as implemented in the MATLAB function ode45.m. Our differential equations are for x= x(t), where the time t is the independent variable, and we will make use of the notation \dot{x}=d x / d t. This notation is still widely used by physicists and descends directly from the notation originally used by Newton.

Euler method

The Euler method is the most straightforward method to integrate a differential equation. Consider the first-order differential equation

\dot{x}=f(t, x), \nonumber

with the initial condition x(0)=x_{0}. Define t_{n}=n \Delta t and x_{n}=x\left(t_{n}\right). A Taylor series expansion of x_{n+1} results in

\begin{aligned} x_{n+1} &=x\left(t_{n}+\Delta t\right) \\ &=x\left(t_{n}\right)+\Delta t \dot{x}\left(t_{n}\right)+\mathrm{O}\left(\Delta t^{2}\right) \\ &=x\left(t_{n}\right)+\Delta t f\left(t_{n}, x_{n}\right)+\mathrm{O}\left(\Delta t^{2}\right) \end{aligned} \nonumber

The Euler Method is therefore written as

x_{n+1}=x\left(t_{n}\right)+\Delta t f\left(t_{n}, x_{n}\right) \nonumber

We say that the Euler method steps forward in time using a time-step \Delta t, starting from the initial value x_{0}=x(0). The local error of the Euler Method is \mathrm{O}\left(\Delta t^{2}\right). The global error, however, incurred when integrating to a time T, is a factor of 1 / \Delta t larger and is given by \mathrm{O}(\Delta t). It is therefore customary to call the Euler Method a first-order method.

Modified Euler method

This method is of a type that is called a predictor-corrector method. It is also the first of what are Runge-Kutta methods. As before, we want to solve (7.3). The idea is to average the value of \dot{x} at the beginning and end of the time step. That is, we would like to modify the Euler method and write

x_{n+1}=x_{n}+\frac{1}{2} \Delta t\left(f\left(t_{n}, x_{n}\right)+f\left(t_{n}+\Delta t, x_{n+1}\right)\right) \nonumber

The obvious problem with this formula is that the unknown value x_{n+1} appears on the right-hand-side. We can, however, estimate this value, in what is called the predictor step. For the predictor step, we use the Euler method to find

x_{n+1}^{p}=x_{n}+\Delta t f\left(t_{n}, x_{n}\right) \nonumber

The corrector step then becomes

x_{n+1}=x_{n}+\frac{1}{2} \Delta t\left(f\left(t_{n}, x_{n}\right)+f\left(t_{n}+\Delta t, x_{n+1}^{p}\right)\right) \nonumber

The Modified Euler Method can be rewritten in the following form that we will later identify as a Runge-Kutta method:

\begin{aligned} k_{1} &=\Delta t f\left(t_{n}, x_{n}\right) \\ k_{2} &=\Delta t f\left(t_{n}+\Delta t, x_{n}+k_{1}\right) \\ x_{n+1} &=x_{n}+\frac{1}{2}\left(k_{1}+k_{2}\right) \end{aligned} \nonumber

Second-order Runge-Kutta methods

We now derive all second-order Runge-Kutta methods. Higher-order methods can be similarly derived, but require substantially more algebra.

We consider the differential equation given by (7.3). A general second-order Runge-Kutta method may be written in the form

\begin{aligned} k_{1} &=\Delta t f\left(t_{n}, x_{n}\right) \\ k_{2} &=\Delta t f\left(t_{n}+\alpha \Delta t, x_{n}+\beta k_{1}\right) \\ x_{n+1} &=x_{n}+a k_{1}+b k_{2} \end{aligned} \nonumber

with \alpha, \beta, a and b constants that define the particular second-order Runge-Kutta method. These constants are to be constrained by setting the local error of the second-order Runge-Kutta method to be \mathrm{O}\left(\Delta t^{3}\right). Intuitively, we might guess that two of the constraints will be a+b=1 and \alpha=\beta.

We compute the Taylor series of x_{n+1} directly, and from the Runge-Kutta method, and require them to be the same to order \Delta t^{2}. First, we compute the Taylor series of x_{n+1}. We have

\begin{aligned} x_{n+1} &=x\left(t_{n}+\Delta t\right) \\ &=x\left(t_{n}\right)+\Delta t \dot{x}\left(t_{n}\right)+\frac{1}{2}(\Delta t)^{2} \ddot{x}\left(t_{n}\right)+\mathrm{O}\left(\Delta t^{3}\right) \end{aligned} \nonumber

Now,

\dot{x}\left(t_{n}\right)=f\left(t_{n}, x_{n}\right) . \nonumber

The second derivative is more complicated and requires partial derivatives. We have

\begin{aligned} \ddot{x}\left(t_{n}\right) &\left.=\frac{d}{d t} f(t, x(t))\right]_{t=t_{n}} \\ &=f_{t}\left(t_{n}, x_{n}\right)+\dot{x}\left(t_{n}\right) f_{x}\left(t_{n}, x_{n}\right) \\ &=f_{t}\left(t_{n}, x_{n}\right)+f\left(t_{n}, x_{n}\right) f_{x}\left(t_{n}, x_{n}\right) \end{aligned} \nonumber

Therefore,

x_{n+1}=x_{n}+\Delta t f\left(t_{n}, x_{n}\right)+\frac{1}{2}(\Delta t)^{2}\left(f_{t}\left(t_{n}, x_{n}\right)+f\left(t_{n}, x_{n}\right) f_{x}\left(t_{n}, x_{n}\right)\right) \nonumber

Second, we compute x_{n+1} from the Runge-Kutta method given by (7.5). Substituting in k_{1} and k_{2}, we have

x_{n+1}=x_{n}+a \Delta t f\left(t_{n}, x_{n}\right)+b \Delta t f\left(t_{n}+\alpha \Delta t, x_{n}+\beta \Delta t f\left(t_{n}, x_{n}\right)\right) . \nonumber

We Taylor series expand using

\begin{aligned} f\left(t_{n}+\alpha \Delta t, x_{n}+\beta \Delta t f\left(t_{n}, x_{n}\right)\right) & \\ =f\left(t_{n}, x_{n}\right)+\alpha \Delta t f_{t}\left(t_{n}, x_{n}\right)+\beta \Delta t f\left(t_{n}, x_{n}\right) f_{x}\left(t_{n}, x_{n}\right)+\mathrm{O}\left(\Delta t^{2}\right) \end{aligned} \nonumber

The Runge-Kutta formula is therefore

\begin{aligned} x_{n+1}=x_{n}+(a+b) & \Delta t f\left(t_{n}, x_{n}\right) \\ &+(\Delta t)^{2}\left(\alpha b f_{t}\left(t_{n}, x_{n}\right)+\beta b f\left(t_{n}, x_{n}\right) f_{x}\left(t_{n}, x_{n}\right)\right)+\mathrm{O}\left(\Delta t^{3}\right) \end{aligned} \nonumber

Comparing (7.6) and (7.7), we find

\begin{aligned} a+b &=1 \\ \alpha b &=1 / 2 \\ \beta b &=1 / 2 \end{aligned} \nonumber

There are three equations for four parameters, and there exists a family of secondorder Runge-Kutta methods.

The Modified Euler Method given by (7.4) corresponds to \alpha=\beta=1 and a= b=1 / 2. Another second-order Runge-Kutta method, called the Midpoint Method, corresponds to \alpha=\beta=1 / 2, a=0 and b=1 . This method is written as

\begin{aligned} k_{1} &=\Delta t f\left(t_{n}, x_{n}\right) \\ k_{2} &=\Delta t f\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{1}\right) \\ x_{n+1} &=x_{n}+k_{2} \end{aligned} \nonumber

Higher-order Runge-Kutta methods

The general second-order Runge-Kutta method was given by (7.5). The general form of the third-order method is given by

\begin{aligned} k_{1} &=\Delta t f\left(t_{n}, x_{n}\right) \\ k_{2} &=\Delta t f\left(t_{n}+\alpha \Delta t, x_{n}+\beta k_{1}\right) \\ k_{3} &=\Delta t f\left(t_{n}+\gamma \Delta t, x_{n}+\delta k_{1}+\epsilon k_{2}\right) \\ x_{n+1} &=x_{n}+a k_{1}+b k_{2}+c k_{3} \end{aligned} \nonumber

The following constraints on the constants can be guessed: \alpha=\beta, \gamma=\delta+\epsilon, and a+b+c=1. Remaining constraints need to be derived.

The fourth-order method has a k_{1}, k_{2}, k_{3} and k_{4}. The fifth-order method requires up to k_{6}. The table below gives the order of the method and the number of stages required.

order 2 3 4 5 6 7 8
minimum # stages 2 3 4 6 7 9 11

Because of the jump in the number of stages required between the fourth-order and fifth-order method, the fourth-order Runge-Kutta method has some appeal. The general fourth-order method starts with 13 constants, and one then finds 11 constraints. A particularly simple fourth-order method that has been widely used is given by

\begin{aligned} k_{1} &=\Delta t f\left(t_{n}, x_{n}\right) \\ k_{2} &=\Delta t f\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{1}\right) \\ k_{3} &=\Delta t f\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{2}\right) \\ k_{4} &=\Delta t f\left(t_{n}+\Delta t, x_{n}+k_{3}\right) \\ x_{n+1} &=x_{n}+\frac{1}{6}\left(k_{1}+2 k_{2}+2 k_{3}+k_{4}\right) \end{aligned} \nonumber

Adaptive Runge-Kutta Methods

As in adaptive integration, it is useful to devise an ode integrator that automatically finds the appropriate \Delta t. The Dormand-Prince Method, which is implemented in MATLAB’s ode45.m, finds the appropriate step size by comparing the results of a fifth-order and fourth-order method. It requires six function evaluations per time step, and constructs both a fifth-order and a fourth-order method from these function evaluations.

Suppose the fifth-order method finds x_{n+1} with local error \mathrm{O}\left(\Delta t^{6}\right), and the fourth-order method finds x_{n+1}^{\prime} with local error \mathrm{O}\left(\Delta t^{5}\right). Let \varepsilon be the desired error tolerance of the method, and let e be the actual error. We can estimate e from the difference between the fifth-and fourth-order methods; that is,

e=\left|x_{n+1}-x_{n+1}^{\prime}\right| \nonumber

Now e is of \mathrm{O}\left(\Delta t^{5}\right), where \Delta t is the step size taken. Let \Delta \tau be the estimated step size required to get the desired error \varepsilon. Then we have

e / \varepsilon=(\Delta t)^{5} /(\Delta \tau)^{5} \nonumber

or solving for \Delta \tau,

\Delta \tau=\Delta t\left(\frac{\varepsilon}{e}\right)^{1 / 5} \nonumber

On the one hand, if e<\varepsilon, then we accept x_{n+1} and do the next time step using the larger value of \Delta \tau. On the other hand, if e>\varepsilon, then we reject the integration step and redo the time step using the smaller value of \Delta \tau. In practice, one usually increases the time step slightly less and decreases the time step slightly more to prevent the waste of too many failed time steps.

System of differential equations

Our numerical methods can be easily adapted to solve higher-order differential equations, or equivalently, a system of differential equations. First, we show how a second-order differential equation can be reduced to two first-order equations. Consider

\ddot{x}=f(t, x, \dot{x}) . \nonumber

This second-order equation can be rewritten as two first-order equations by defining u=\dot{x} . We then have the system

\begin{aligned} &\dot{x}=u, \\ &\dot{u}=f(t, x, u) . \end{aligned} \nonumber

This trick also works for higher-order equation. For another example, the thirdorder equation

\dddot x=f(t, x, \dot{x}, \ddot{x}), \nonumber

can be written as

\begin{aligned} &\dot{x}=u \\ &\dot{u}=v \\ &\dot{v}=f(t, x, u, v) . \end{aligned} \nonumber

Now, we show how to generalize Runge-Kutta methods to a system of differential equations. As an example, consider the following system of two odes,

\begin{aligned} &\dot{x}=f(t, x, y), \\ &\dot{y}=g(t, x, y), \end{aligned} \nonumber

with the initial conditions x(0)=x_{0} and y(0)=y_{0}. The generalization of the commonly used fourth-order Runge-Kutta method would be

\begin{aligned} k_{1} &=\Delta t f\left(t_{n}, x_{n}, y_{n}\right) \\ l_{1} &=\Delta t g\left(t_{n}, x_{n}, y_{n}\right) \\ k_{2} &=\Delta t f\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{1}, y_{n}+\frac{1}{2} l_{1}\right) \\ l_{2} &=\Delta t g\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{1}, y_{n}+\frac{1}{2} l_{1}\right) \\ y_{3} &=\Delta t f\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{2}, y_{n}+\frac{1}{2} l_{2}\right) \\ l_{3} &=\Delta t g\left(t_{n}+\frac{1}{2} \Delta t, x_{n}+\frac{1}{2} k_{2}, y_{n}+\frac{1}{2} l_{2}\right) \\ y_{n+1} &=y_{n}+\frac{1}{6}\left(l_{1}+2 l_{2}+2 l_{3}+l_{4}\right) \\ k_{4} &=\Delta t f\left(t_{n}+\Delta t, x_{n}+k_{3}, y_{n}+l_{3}\right) \\ l_{4} &=\Delta t g\left(t_{n}+\Delta t, x_{n}+k_{3}, y_{n}+l_{3}\right) \\ &=x_{n}+\frac{1}{6}\left(k_{1}+2 k_{2}+2 k_{3}+k_{4}\right) \\ &=\Delta \end{aligned} \nonumber

Numerical methods: boundary value problem

Finite difference method

We consider first the differential equation

-\frac{d^{2} y}{d x^{2}}=f(x), \quad 0 \leq x \leq 1 \nonumber

with two-point boundary conditions

y(0)=A, \quad y(1)=B \text {. } \nonumber

Equation (7.8) can be solved by quadrature, but here we will demonstrate a numerical solution using a finite difference method.

We begin by discussing how to numerically approximate derivatives. Consider the Taylor series approximation for y(x+h) and y(x-h), given by

\begin{aligned} &y(x+h)=y(x)+h y^{\prime}(x)+\frac{1}{2} h^{2} y^{\prime \prime}(x)+\frac{1}{6} h^{3} y^{\prime \prime \prime}(x)+\frac{1}{24} h^{4} y^{\prime \prime \prime \prime}(x)+\ldots, \\ &y(x-h)=y(x)-h y^{\prime}(x)+\frac{1}{2} h^{2} y^{\prime \prime}(x)-\frac{1}{6} h^{3} y^{\prime \prime \prime}(x)+\frac{1}{24} h^{4} y^{\prime \prime \prime \prime}(x)+\ldots \end{aligned} \nonumber

The standard definitions of the derivatives give the first-order approximations

\begin{aligned} &y^{\prime}(x)=\frac{y(x+h)-y(x)}{h}+\mathrm{O}(h) \\ &y^{\prime}(x)=\frac{y(x)-y(x-h)}{h}+\mathrm{O}(h) \end{aligned} \nonumber

The more widely-used second-order approximation is called the central difference approximation and is given by

y^{\prime}(x)=\frac{y(x+h)-y(x-h)}{2 h}+\mathrm{O}\left(h^{2}\right) \nonumber

The finite difference approximation to the second derivative can be found from considering

y(x+h)+y(x-h)=2 y(x)+h^{2} y^{\prime \prime}(x)+\frac{1}{12} h^{4} y^{\prime \prime \prime \prime}(x)+\ldots, \nonumber

from which we find

y^{\prime \prime}(x)=\frac{y(x+h)-2 y(x)+y(x-h)}{h^{2}}+\mathrm{O}\left(h^{2}\right) \text {. } \nonumber

Sometimes a second-order method is required for x on the boundaries of the domain. For a boundary point on the left, a second-order forward difference method requires the additional Taylor series

y(x+2 h)=y(x)+2 h y^{\prime}(x)+2 h^{2} y^{\prime \prime}(x)+\frac{4}{3} h^{3} y^{\prime \prime \prime}(x)+\ldots \nonumber

We combine the Taylor series for y(x+h) and y(x+2 h) to eliminate the term proportional to h^{2} :

y(x+2 h)-4 y(x+h)=-3 y(x)-2 h y^{\prime}(x)+\mathrm{O}\left(\mathrm{h}^{3}\right) \nonumber

Therefore,

y^{\prime}(x)=\frac{-3 y(x)+4 y(x+h)-y(x+2 h)}{2 h}+\mathrm{O}\left(h^{2}\right) \nonumber

For a boundary point on the right, we send h \rightarrow-h to find

y^{\prime}(x)=\frac{3 y(x)-4 y(x-h)+y(x-2 h)}{2 h}+\mathrm{O}\left(h^{2}\right) \nonumber

We now write a finite difference scheme to solve (7.8). We discretize x by defining x_{i}=i h, i=0,1, \ldots, n+1. Since x_{n+1}=1, we have h=1 /(n+1). The functions y(x) and f(x) are discretized as y_{i}=y\left(x_{i}\right) and f_{i}=f\left(x_{i}\right) . The second-order differential equation (7.8) then becomes for the interior points of the domain

-y_{i-1}+2 y_{i}-y_{i+1}=h^{2} f_{i}, \quad i=1,2, \ldots n, \nonumber

with the boundary conditions y_{0}=A and y_{n+1}=B. We therefore have a linear system of equations to solve. The first and nth equation contain the boundary conditions and are given by

\begin{aligned} 2 y_{1}-y_{2} &=h^{2} f_{1}+A \\ -y_{n-1}+2 y_{n} &=h^{2} f_{n}+B \end{aligned} \nonumber

The second and third equations, etc., are

\begin{aligned} &-y_{1}+2 y_{2}-y_{3}=h^{2} f_{2} \\ &-y_{2}+2 y_{3}-y_{4}=h^{2} f_{3} \end{aligned} \nonumber

In matrix form, we have

\left(\begin{array}{rrrrrrrr} 2 & -1 & 0 & 0 & \cdots & 0 & 0 & 0 \\ -1 & 2 & -1 & 0 & \cdots & 0 & 0 & 0 \\ 0 & -1 & 2 & -1 & \cdots & 0 & 0 & 0 \\ \vdots & \vdots & \vdots & \vdots & \ddots & \vdots & \vdots & \vdots \\ 0 & 0 & 0 & 0 & \cdots & -1 & 2 & -1 \\ 0 & 0 & 0 & 0 & \cdots & 0 & -1 & 2 \end{array}\right)\left(\begin{array}{c} y_{1} \\ y_{2} \\ y_{3} \\ \vdots \\ y_{n-1} \\ y_{n} \end{array}\right)=\left(\begin{array}{c} h^{2} f_{1}+A \\ h^{2} f_{2} \\ h^{2} f_{3} \\ \vdots \\ h^{2} f_{n-1} \\ h^{2} f_{n}+B \end{array}\right) \nonumber

The matrix is tridiagonal, and a numerical solution by Guassian elimination can be done quickly. The matrix itself is easily constructed using the MATLAB function diag.m and ones.m. As excerpted from the MATLAB help page, the function call ones (\mathrm{m}, \mathrm{n}) returns an m-by-n matrix of ones, and the function call \operatorname{diag}(\mathrm{v}, \mathrm{k}), when \mathrm{v} is a vector with \mathrm{n} components, is a square matrix of order \mathrm{n}+\mathrm{abs}(\mathrm{k}) with the elements of \mathrm{v} on the \mathrm{k}-th diagonal: k=0 is the main diagonal, k>0 is above the main diagonal and k<0 is below the main diagonal. The n \times n matrix above can be constructed by the MATLAB code

M=\operatorname{diag}(-\text { ones }(n-1,1),-1)+\operatorname{diag}\left(2^{*} \text { ones }(n, 1), 0\right)+\operatorname{diag}(-\text { ones }(n-1,1), 1) ; \nonumber

The right-hand-side, provided \mathrm{f} is a given n-by-1 vector, can be constructed by the MATLAB code

\mathrm{b}=\mathrm{h}^{\wedge} 2^{*} \mathrm{f} ; \mathrm{b}(1)=\mathrm{b}(1)+\mathrm{A} ; \mathrm{b}(\mathrm{n})=\mathrm{b}(\mathrm{n})+\mathrm{B} \nonumber

and the solution for u is given by the MATLAB code

\mathrm{y}=\mathrm{M} \backslash \mathrm{b} \nonumber

Shooting method

The finite difference method can solve linear odes. For a general ode of the form

\frac{d^{2} y}{d x^{2}}=f(x, y, d y / d x) \nonumber

with y(0)=A and y(1)=B, we use a shooting method. First, we formulate the ode as an initial value problem. We have

\begin{aligned} &\frac{d y}{d x}=z \\ &\frac{d z}{d x}=f(x, y, z) \end{aligned} \nonumber

The initial condition y(0)=A is known, but the second initial condition z(0)=b is unknown. Our goal is to determine b such that y(1)=B.

In fact, this is a root-finding problem for an appropriately defined function. We define the function F=F(b) such that

F(b)=y(1)-B \nonumber

In other words, F(b) is the difference between the value of y(1) obtained from integrating the differential equations using the initial condition z(0)=b, and B. Our root-finding routine will want to solve F(b)=0. (The method is called shooting because the slope of the solution curve for y=y(x) at x=0 is given by b, and the solution hits the value y(1) at x=1. This looks like pointing a gun and trying to shoot the target, which is B.)

To determine the value of b that solves F(b)=0, we iterate using the Secant method, given by

b_{n+1}=b_{n}-F\left(b_{n}\right) \frac{b_{n}-b_{n-1}}{F\left(b_{n}\right)-F\left(b_{n-1}\right)} \nonumber

We need to start with two initial guesses for b, solving the ode for the two corresponding values of y(1). Then the Secant Method will give us the next value of b to try, and we iterate until |y(1)-B|< tol, where tol is some specified tolerance for the error

Numerical methods: eigenvalue problem

For illustrative purposes, we develop our numerical methods for what is perhaps the simplest eigenvalue ode. With y=y(x) and 0 \leq x \leq 1, this simple ode is given by

y^{\prime \prime}+\lambda^{2} y=0 \nonumber

To solve (7.9) numerically, we will develop both a finite difference method and a shooting method. Furthermore, we will show how to solve (7.9) with homogeneous boundary conditions on either the function y or its derivative y^{\prime}.

Finite difference method

We first consider solving (7.9) with the homogeneous boundary conditions y(0)= y(1)=0 . In this case, we have already shown that the eigenvalues of (7.9) are given by \lambda=\pi, 2 \pi, 3 \pi, \ldots.

With n interior points, we have x_{i}=i h for i=0, \ldots, n+1, and h=1 /(n+1). Using the centered-finite-difference approximation for the second derivative, (7.9) becomes

y_{i-1}-2 y_{i}+y_{i+1}=-h^{2} \lambda^{2} y_{i} \nonumber

Applying the boundary conditions y_{0}=y_{n+1}=0, the first equation with i=1, and the last equation with i=n, are given by

\begin{aligned} -2 y_{1}+y_{2} &=-h^{2} \lambda^{2} y_{1} \\ y_{n-1}-2 y_{n} &=-h^{2} \lambda^{2} y_{n} \end{aligned} \nonumber

The remaining n-2 equations are given by (7.10) for i=2, \ldots, n-1 It is of interest to see how the solution develops with increasing n. The smallest possible value is n=1, corresponding to a single interior point, and since h=1 / 2 we have

-2 y_{1}=-\frac{1}{4} \lambda^{2} y_{1} \nonumber

so that \lambda^{2}=8, or \lambda=2 \sqrt{2}=2.8284. This is to be compared to the first eigenvalue which is \lambda=\pi. When n=2, we have h=1 / 3, and the resulting two equations written in matrix form are given by

\left(\begin{array}{rr} -2 & 1 \\ 1 & -2 \end{array}\right)\left(\begin{array}{l} y_{1} \\ y_{2} \end{array}\right)=-\frac{1}{9} \lambda^{2}\left(\begin{array}{l} y_{1} \\ y_{2} \end{array}\right) \nonumber

This is a matrix eigenvalue problem with the eigenvalue given by \mu=-\lambda^{2} / 9. The solution for \mu is arrived at by solving

\operatorname{det}\left(\begin{array}{cc} -2-\mu & 1 \\ 1 & -2-\mu \end{array}\right)=0 \nonumber

with resulting quadratic equation

(2+\mu)^{2}-1=0 \nonumber

The solutions are \mu=-1,-3, and since \lambda=3 \sqrt{-\mu}, we have \lambda=3,3 \sqrt{3}=5.1962. These two eigenvalues serve as rough approximations to the first two eigenvalues \pi and 2 \pi.

With A an n-by-n matrix, the MATLAB variable mu=eig(A) is a vector containing the n eigenvalues of the matrix A. The built-in function eig.m can therefore be used to find the eigenvalues. With n grid points, the smaller eigenvalues will converge more rapidly than the larger ones.

We can also consider boundary conditions on the derivative, or mixed boundary conditions. For example, consider the mixed boundary conditions given by y(0)=0 and y^{\prime}(1)=0. The eigenvalues of (7.9) can then be determined analytically to be \lambda_{i}=(i-1 / 2) \pi, with i a natural number.

The difficulty we now face is how to implement a boundary condition on the derivative. Our computation of y^{\prime \prime} uses a second-order method, and we would like the computation of the first derivative to also be second order. The condition y^{\prime}(1)=0 occurs on the right-most boundary, and we can make use of the secondorder backward-difference approximation to the derivative that we have previously derived. This finite-difference approximation for y^{\prime}(1) can be written as

y_{n+1}^{\prime}=\frac{3 y_{n+1}-4 y_{n}+y_{n-1}}{2 h} . \nonumber

Now, the nth finite-difference equation was given by

y_{n-1}-2 y_{n}+y_{n+1}=-h^{2} y_{n}, \nonumber

and we now replace the value y_{n+1} using (7.11); that is,

y_{n+1}=\frac{1}{3}\left(2 h y_{n+1}^{\prime}+4 y_{n}-y_{n-1}\right) . \nonumber

Implementing the boundary condition y_{n+1}^{\prime}=0, we have

y_{n+1}=\frac{4}{3} y_{n}-\frac{1}{3} y_{n-1} \nonumber

Therefore, the nth finite-difference equation becomes

\frac{2}{3} y_{n-1}-\frac{2}{3} y_{n}=-h^{2} \lambda^{2} y_{n} \nonumber

For example, when n=2, the finite difference equations become

\left(\begin{array}{rr} -2 & 1 \\ \frac{2}{3} & -\frac{2}{3} \end{array}\right)\left(\begin{array}{l} y_{1} \\ y_{2} \end{array}\right)=-\frac{1}{9} \lambda^{2}\left(\begin{array}{l} y_{1} \\ y_{2} \end{array}\right) \nonumber

The eigenvalues of the matrix are now the solution of

(\mu+2)\left(\mu+\frac{2}{3}\right)-\frac{2}{3}=0 \nonumber

Or

3 \mu^{2}+8 \mu+2=0 \nonumber

Therefore, \mu=(-4 \pm \sqrt{10}) / 3, and we find \lambda=1.5853,4.6354, which are approximations to \pi / 2 and 3 \pi / 2.

Shooting method

We apply the shooting method to solve (7.9) with boundary conditions y(0)= y(1)=0. The initial value problem to solve is

\begin{aligned} &y^{\prime}=z \\ &z^{\prime}=-\lambda^{2} y \end{aligned} \nonumber

with known boundary condition y(0)=0 and an unknown boundary condition on y^{\prime}(0). In fact, any nonzero boundary condition on y^{\prime}(0) can be chosen: the differential equation is linear and the boundary conditions are homogeneous, so that if y(x) is an eigenfunction then so is A y(x). What we need to find here is the value of \lambda such that y(1)=0 . In other words, choosing y^{\prime}(0)=1, we solve

F(\lambda)=0 \nonumber

where F(\lambda)=y(1), obtained by solving the initial value problem. Again, an iteration for the roots of F(\lambda) can be done using the Secant Method. For the eigenvalue problem, there are an infinite number of roots, and the choice of the two initial guesses for \lambda will then determine to which root the iteration will converge.

For this simple problem, it is possible to write explicitly the equation F(\lambda)=0. The general solution to (7.9) is given by

y(x)=A \cos (\lambda x)+B \sin (\lambda x) . \nonumber

The initial condition y(0)=0 yields A=0 . The initial condition y^{\prime}(0)=1 yields

B=1 / \lambda \nonumber

Therefore, the solution to the initial value problem is

y(x)=\frac{\sin (\lambda x)}{\lambda} \nonumber

The function F(\lambda)=y(1) is therefore given by

F(\lambda)=\frac{\sin \lambda}{\lambda} \nonumber

and the roots occur when \lambda=\pi, 2 \pi, \ldots .

If the boundary conditions were y(0)=0 and y^{\prime}(1)=0, for example, then we would simply redefine F(\lambda)=y^{\prime}(1). We would then have

F(\lambda)=\frac{\cos \lambda}{\lambda} \nonumber

and the roots occur when \lambda=\pi / 2,3 \pi / 2, \ldots

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