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Energy integrals involving both Slater-type and Gaussian atomic orbitals
D.M. Silver
To cite this version:
D.M. Silver. Energy integrals involving both Slater-type and Gaussian atomic orbitals. Journal de
Physique, 1971, 32 (2-3), pp.129-133. �10.1051/jphys:01971003202-3012900�. �jpa-00207033�
129
ENERGY INTEGRALS INVOLVING BOTH SLATER-TYPE
AND GAUSSIAN ATOMIC ORBITALS
D. M. SILVER
(*)
Centre
Européen
de CalculAtomique
etMoléculaire,
C. E. C. A. M.Bâtiment
506, 91, Campus d’Orsay,
France(Reçu
le 7 octobre1970,
révisé le 7 novembre1970)
Résumé. 2014 On
développe
des formulesexplicites
pour évaluer toutes lesintégrales d’énergie cinétique
etpotentielle,
pour un seul centre, et pour un ou deux électrons. Cesintégrales
sepré-
sentent
quand
on utilise comme fonctions de base à la fois des orbitales du type de Slater et du type Gaussien.Abstract. 2014
Explicit
formulas aredeveloped
for the evaluation of allsingle-center,
one andtwo-electron kinetic and
potential
energyintegrals arising
with the use of a basis setconsisting
of bothSlater-type
and Gaussian atomic orbitals.PHYSIQUE TOME 32, FÉVRIER-MARS 1971,
Classification
physics
Abstracts13.00
Introduction. -
Slater-type
and Gaussian atomicorbitals each have certain features that make their use
in molecular basis sets
advantageous. Slater-type
orbitals
(STO),
whoseradially
nodeless forms arederived
[1]
from associatedLaguerre
functions which in turn are solutions to theSchrôdinger equation
forthe
hydrogen
atom, are well suited to describe the atomic-like structure of atoms in molecules butgive
rise to rather difficult
multi-center, electron-repulsion integrals.
TheGaussian-type
orbital(GTO) presents
no
major
obstacle in terms ofintegral
evaluation[2, 3]
but is somewhat less suitable for
describing
molecularelectronic structure
[4].
The use of bothtypes
of orbital combined into asingle
basis set[5, 6]
offers thepossi- bility
ofincorporating
the better features of each scheme into asingle
calculation.For the
general
multi-center energyintegrals,
eachinvolving
both STO’s and GTO’s in various combi-nations,
the Gaussian transformtechnique [7]
isparti- cularly appropriate.
A transformation of thekind,
reduces the
exponential
radialdependence
of each ofthe STO’s to Gaussian form so that the
configuration
space
integrations
can beeasily
evaluated. As anexample,
anexchange integral
over four STO’s involves four suchintegral
transforms but for each GTOreplacing
an STO in theoriginal integrand,
one ofthese
integrations
is eliminated.Thus, augmenting
anSTO basis set
by adding
a collection ofGTO’s,
addsvarious
types
of mixed STO-GTO and pure GTO(*) Present Address : Applied Physics Laboratory, The Johns Hopkins University, Silver Spring, Maryland 20910, U. S. A.
integrals
which are ofincreasingly
more tractableform.
More direct
procedures
can beemployed
to handlethe one-center, mixed STO-GTO
integrals.
An auxi-liary
function defined to enable the evaluation ofoverlap integrals provides
akey
todeveloping
methodsof
treating
the various two-electronintegrals.
In thefollowing,
the one-electronintegrals
are first examinedand then the two-electron
integrals
are treated.I. One-electron
integrals.
- A. DÉFINITIONS. - The normalizedSlater-type
atomicorbital,
x, is taken to have theform,
where
YZm
is anormalized,
realspherical
harmonicand the radial normalization constant,
N,
isgiven by :
The normalized
Gaussian-type orbital,
ç, is to be written aswhere the radial normalization constant,
M,
is express-ed by
and F is the standard Gamma function.
The
overlap integral,
between a GTO and an STO is to be evaluated from the
expression,
Article published online by EDP Sciences and available at http://dx.doi.org/10.1051/jphys:01971003202-3012900
130
where in the
auxiliary
function F is defined :In terms of this
function,
the nuclear attractionintegral,
can be
equated
toOf the two
equivalent
formspossible
for the kinetic energyintegral,
thefollowing
is to bepreferred :
B. AUXILIARY FUNCTION F. - The
auxiliary
func-tion F can be
computed
from the recursionrelation,
using
thestarting
values :where erfc denotes the standard
complimentary
errorfunction. Since the recursion
procedure
of eq.(12)
involves
differencing,
a check has been made to deter- mine thatregion
of theparameter
space of aand fl
where the function with the
highest
neededparameter k
can be
computed
with a certain level of accuracy.This has been
accomplished through
use of acomputer
programdesigned
to examine the number ofsignificant places
that are lost in eachstep
in the recursive proce- dure for a range of aand fl
from 0.15 to 28.0 andvalues of k as
high
as 12.Using
doubleprecision
arith-metic on an IBM
360/75,
it was found that ifB2/4
ahas a value less than about
13.0,
one would lose nomore than six
significant figures
out of the sixteendigit
word. Of course, asfl’/4
oc becomeslarger,
thedifferencing
errors continue to increase.Variants of the differential
formulas,
have proven to be useful within the context of two- electron
integral
formulations.II. Two-electron
integrals.
- A. PRELIMINARY. - The electronrepulsion integral, E,
between electrons p and q,where t/1
i denotes either a GTO(w)
or an STO(x)
with
corresponding
orbitalparameters having
subs-cripts i,
allows immediateintegration
over the fourangular
variablesleaving
the form :where
Ki
is theappropriate
normalization constant of eq.(3)
or(5),
the functions q lm and the restrictionson the summation indices
lA
MA andlB
MB and theirrelationships
to11
ml12
m2 and13
m314
m4 have been discussedpreviously [8]
and the two radialintegrations
are embodied in the function
Rtype,
which is to betreated in detail below.
Rtype
has thefollowing
sixmajor designations corresponding
to the sixintegral types
shown :where (p
and xcorrespond
to GTO’s and STO’srespectively. Hereafter,
thefollowing symbols
shallbe used :
B. INTEGRAL TYPE 1. - The radial
integrations corresponding
toRi,
are
easily performed analytically
and the results appear hereonly
forcompleteness :
C. INTEGRAL TYPE 2. - The
procedure required
toanalytically integrate type 2,
consists of
repeated partial integration using
eq.( 15b)
for the first term and inversion of the order of thet-integration
with that embedded in the function F for the second term. Aftergrouping
the various sum-mations,
one has the result :D. INTEGRAL TYPE 3. - The third
type
ofintegral,
is
disposed
ofby
the use of Gaussian numericalintegrations [9] :
where
and 11k
is the k-th zero of theLegendre functions, PN(11),
and thecorresponding weights
aregiven by :
Choosing
N togive
at least twelfth-orderintegra-
tions in eq.
(26) produces integrals having
at leasteight
decimalplace
accuracy over the range of orbitalparameters
studied here.E. INTEGRAL TYPE 4. -
Here,
two cases arisedepending
on the even-oddparity
of theparameters
nA + L. The situation in
which nA
+ L is an eveninteger
isdesignated
case A and thefollowing
expres- sion isintegrated :
Using
the relation in eq.(15a),
the first term canbe resolved
by partial integrations
while the secondterm can be
integrated by parts
afterinverting
theorder of the
t-integration
with that embedded in Fto
give :
If na + L is an odd
integer,
case B has the form :Both terms can be
integrated by parts
after inter-changing
the order ofintegrations.
Aftercombining summations, R4B is
obtained from :Eq. (32)
could be usedregardless
of theparity
ofnA +
L ; however,
eq.(30)
is to bepreferred
whenapplicable
since it involvesonly
the addition ofposi-
tive terms and is therefore
inherently
morecapable
ofnumerical accuracy.
F. INTEGRAL TYPE 5. - The
parity
of nA + Lgives
rise to two cases for thistype
ofintegral.
WhennA + L is even, case A is used :
132
The first term is
integrated numerically
as inType R3
and the second term isintegrated by parts using
eq.
(15a)
togive :
where the
weights,
w;, andpoints,
xi, are defined in eq.(27).
Case B ariseswhen nA
+ L is an oddinteger :
Now eq.
(1 5a)
enablespartial integration
of thefirst term and numerical
integrations
handle the secondterm :
In both cases, if the order N of the numerical
integrations
is taken to be at leasttwelve,
theaccuracy of the
integral
is assured to abouteight
decimals.
G. INTEGRAL TYPE 6. - The pure GTO
integrals split
into three casesdepending
on the even-oddparity
of both nA +L and nB
+ L. Case A is the most familiar situation where both nA + L and nB + L are evenintegers :
. Because
of theparity requirements
on the para-meters, both terms can be
integrated by parts
toyield :
Less familiar is case
B,
where both nA + L and nB + L are oddintegers :
Because of the
parity
restrictions is this case, each term in eq.(39)
can beintegrated by parts yielding :
The most tractable manner of
handling
caseC, where nA
+ L is oddand nB
+ L is even, is to defineR6 c
as follows :Although
the second term canagain
beintegrated by parts
as in caseA,
the first term is mosteasily
handled
by performing
ther-integration analytically
and
using
numericalintegration
for theremaining t-integration :
where wi and xi are defined in eq.
(27). Only
a very lowintegration order, N,
isrequired
if(B
is smallerthan 03BEA
but in the most difficultsituations, where (B
is much
larger
than03BEA,
an order ashigh
as sixteenmight
berequired
to achieveeight
decimal accuracy.Only
case A arises when the orbitals are restrictedto the
classes,
1 s, 3 s, ..., 12 p,
4 p, ...,3 d,
etc. The other two cases enteronly
when the orbitals2 s, 4 s, ...,
3 p, 5 p, ..., 4
d,
etc. are introduced.H. DISCUSSION. - The
auxiliary
functionFn(a, P)
defined in eq.
(8) provides
the means oftransforming
the mixed STO-GTO two-electron
integrals
intotractable forms for
computer
evaluation. Since thecomputed
accuracy of F isgreatest
whenP2/4
a issmall,
the choice of finalexpressions
isalways governed by
this criteria.A number of the
integral types
allow for more thanone
possible integration
scheme and moreover, aside from thelabelling
of orbitalparameters,
many of the finalexpressions
arequite
similar in form.Thus,
certain blocks of
computer
code can be used for thepartial
evaluation of more than oneintegral type.
Also,
an alternative form of agiven integral
can beevaluated for
checking
purposesby using appropriate
blocks of
computer
code written for some otherintegral type.
In this way, cross checks areprovided
for the formulations and their
subsequent
translation for thecomputer.
Although
thetechnique
oftransforming
exponen- tials into Gaussian formthrough
eq.(1) might
prove to be the most usefulapproach
to the multi-centerintegrals,
itsapplication
in thesingle
center case wouldbe cumbersome
compared
to thepresent schemes ;
in
particular,
this is true since one wouldplan
toperform
the transformintegrations
of eq.(1)
nume-rically.
Thedevelopment
of multi-centerprocedures
would be facilitated
by having
availableindependent expressions
forspecial
situations such as those pre- sented here for thelimiting
case where all of the orbital centers coalesce.For calculations of atomic
wavefunctions,
theSlater-type
orbital is theoptimal
choice of basisfunction since the STO’s
give
better characterizations of atomicproperties
than GTO’s and theintegrals
that arise are the easiest to evaluate. For
molecules,
a combination of STO’s and GTO’smight
prove togive
the bestcompromise
between an accurate des-cription
of molecularproperties
and the least timeconsuming integral
evaluation and datahandling
processes. In this case, it would be desireable to have available the most direct means of
processing
eachof the
types
ofintegrals
involvedincluding
the varioussingle-center integrals
examined here. The formulasgiven
areparticularly
well suited to automaticcomputer
calculation and have been used toperform
aprelimi-
nary
study
of SCF wavefunctions for several small atomsusing
basis setscomposed
of both Gaussian andSlater-type
atomic orbitals[5].
Acknowledgements.
- Gratitude isexpressed
toDr. Carl Moser and the Centre National de la Recher- che
Scientifique
for the interest andsupport
which enabled this research to be conducted.References
[1]
SLATER(J. C.), Phys.
Rev.,1930, 36,
57.[2]
BOYS(S. F.),
Proc. Roy. Soc.(London),
1950, A200,
542.
[3]
MCWEENEY(R.),
Nature, 1950,166,
21.[4]
HUZINAGA(S.),
J. Chem.Phys., 1965, 42,
1293.[5]
SILVER(D. M.),
Chem.Phys.
Letters,1970, 7,
511.[6]
ALLEN(L. C.),
J. Chem.Phys., 1959,
31, 736.[7]
SHAVITT(I.)
and KARPLUS(M.),
J. Chem.Phys.,
1965,43,
398.[8]
SILVER(D. M.)
and RUEDENBERG(K.),
J. Chem.Phys., 1968, 49, 4306 ;
eq.(11)
to(14)
and table I.[9]
« Handbook of MathematicalTables)),
ABRAMOWITZ(M.)
and STEGUN(I. A.),
Eds.(Natl.
Bur. Std.Appl.
Math.Ser.,
55,Washington,
D. C.,1964),
p. 887, eq.