
6.3 The Boundary Locus Method 87
Hence, the first term Ar
n
+
in the solution (6.5) approximates the exact solution
to within O(h
2
) while the second term satisfies
Br
n
−
= −
1
12
h
3
(−1)
n
e
−λt
∗
+ O(h
4
).
It is this term that causes problems: it is exponentially growing when <(λ) < 0
(and the exact solution is exponentially decaying) and the factor (−1)
n
causes
it to alternate in sign on consecutive steps (producing the oscillations evident
in Figure 6.9). On a positive note, it has an amplitude proportional to h
3
, so
becomes negligible compared with the dominant O(h
2
) term in the GE when
h is sufficiently small.
Other Nystr¨om and Milne–Simpson methods have similar properties, so
cannot be recommended for solving problems with damping (<(λ) < 0). How-
ever, it is a different story if λ is purely imaginary (oscillatory problems)—see
Section 7.3.
6.3 The Boundary Locus M ethod
It is, in general, quite difficult to determine the region of absolute stability of an
LMM since we have to decide, for each
b
h ∈ C, whether the roots of the stability
polynomial satisfy the strict root condition (|r| < 1). It is more attractive to
look for the boundary of the region, because at least one of the roots of p(r)
on the boundary has modulus |r| = 1. Thus, the boundary is a subset of the
points
b
h ∈ C for which r = e
is
, where s ∈ R. Substituting r = e
is
into the
stability polynomial and solving for
b
h we obtain
b
h =
b
h(s) and plotting the
locus in the complex plane gives a curve, part of which will be the required
boundary. We illustrate the process with an example that contains most of the
important features.
Example 6.13
Use the boundary locus method to determine the boundary of the region of
absolute stability of the LMM x
n+2
− x
n+1
= hf
n
(see Example 6.11).
With r = e
is
the stability polynomial (6.4) gives
b
h = r
2
− r, and so
b
h(s) = e
2is
− e
is
= [cos(2s) − cos(s)] + i[sin(2s) − sin(s)].
Plotting the locus of the points bx(s) = cos(2s) −cos(s), by(s) = sin(2s) −sin(s)
for 0 ≤ s < 2π we obtain the curve shown in Figure 6.10, which divides the
plane into three subregions—it remains to decide which subregion is the region