• No results found

MULTIDIMENSIONAL ADDITIVE SPLINE APPROXIMATION*

N/A
N/A
Protected

Academic year: 2021

Share "MULTIDIMENSIONAL ADDITIVE SPLINE APPROXIMATION*"

Copied!
22
0
0

Loading.... (view fulltext now)

Full text

(1)

SLAC PUB-2504 STAN-CS-80-799 May 1980

(M)

MULTIDIMENSIONAL ADDITIVE SPLINE APPROXIMATION* Jerome H. Friedman

Stanford Linear Accelerator Center Stanford, California 94305

Eric Grosse

Computer Science Department Stanford University

Stanford, California 94305 Werner Stuettle

Stanford Linear Accelerator Center and

Department of Statistics, Stanford University Stanford, California 94305

ABSTRACT

We describe an adaptive procedure that approximates a function of many . variables by a sum of (univariate) spline functions sm of selected linear combinations am-x of the coordinates

y(x) = c

l~~;rrts;M smbm4

The procedure is nonlinear in that not only the spline coefficients but also the linear combinations are optimized for the particular problem. The sample need not lie on a regular grid, and the approximation is affine

ion invariant, smooth, and lends itself to graph

values, derivatives, and integrals are cheap

ical interpretation. Funct to evaluate.

*Work partially supported by the Department of Energy under contract DE-AC03-76SF00515, and by the National Science Foundation under grant MCS 78-17697.

(2)

1 1. Introdktion

Mu&dimensional surface approximation is recognized as an important prob- lem for which several methodologies have been developed. The aim is to con- struct an approximation 4(x) to a p-dimensional surface y = f(x) on the basis

of (possibly noisy) observations { (yi, xi)}l<icn. -- Most existing methods, such as

tensor product splines, kernels, and thin plate splines (for a survey, see Schumaker [1976]), are linear in that.

4(x) = c wyi,

l<i<n

where the weights ( wi} depend only on x and { xi}l<i< n, but not on { yi},< i< ,.,: --

These methods have the advantage that they are straightforward to compute and their theory is tractable. In pract.ice, however, they are limited because they

cannot take advantage of special properties of the surface. Due to the inherent

sparsity of high-dimensional sampling, procedures successful in high dimensions must be adaptive and thus nominear.

In this paper we describe an adaptive procedure that approximates f(x) by a sum of (univariate) spline functions sm of selected linear combinations a, * x of the coordinates

4(x) = C Sm(am s 4.

l<m<M

51)

The ‘procedure is nonlinear in that not only the spline coefficients but also the

linear combinations are optimized for the particular problem. *

2. The algorithm

The spline function sm along am s x is represented as a sum of j,,, B-splines

[de Boor, 1979) of order q

(3)

2

The approximation 4(x) (g’ iven by equations (1) and (2)) is specified by the direc-

tions tam)l<m<M, the knot sequences along am s x for 1 5 m 5 M, and the

B-spline^coefficients (Pmj}lCmCM,l<j<j,. For particular {a, ), the knots are ’

placed heuristically and then-the{ Pmj } are determined by (linear) least squares.

The residual sum of squares from this fit is taken to be the inverse figure of merit

for (Bmll<m<M*

- -

Following Friedman, Jacobson, and Stuetzle [1980], the approximation is con-

structed in a stepwise manner: given ( a, }1< m< M--l, find aM to optimize the

figure of merit of ( am >I< m< M. Terminate when the figure of merit - - is not

significantly improved.

3. Imp’lementation

The most difficult part of the algorithm is finding each direction am. We per- form a numerical search using a Rosenbrock’method [Rosenbrock, 1966) modified for the unit sphere, starting at the best coordinate direction. On any given search, there is no guarantee that the global optimum will be found. If the local optimum

is insignificant, the search is restarted at random dire.ctions. This guards against

premature termination, If the local optimum is significant but not identical to the global optimum, no great harm is done because a new search is performed in the next iteration on an object function for which the previous optima have been deflated. Each iteration of the optimizer requires 3.5 p function evaluations,

on the average, where p is the dimension of x. Two iterations are nearly always

sufficient.

For high dimensionality, the computation is dominated by the evaluations of the object fu.nction. Since it is not crucial to find the precise optimum, con-

siderable savings can be achieved by substituting a similar;but much less ex-

pensive figure of merit during the search for a new direction. For this figure of

merit not only the previously foun’d directions but also the corresponding spline

coefficients are held fixed. The new direction can thus be found by considering

(4)

3

residuals are modelled by a smooth based on local linear fits [Cleveland, 19791,

[Friedman, Jacobson, and Stuetzle, 19SOJ. The characteristic bandwidth (that is,

the aver^age fraction of observations used in each local fit) is taken to be inversely

proportional to the number of knots, The residual sum of squares from the smooth is the figure of merit used for the smooth. Solving the least squares problem for the original figure of merit requires

operations, while the new figure of merit can be evaluated in roughly n operations using updating formulas for the moving average. The least squares problem has

to be solved only once for each iteration to determine the new model after am has

been found.

To solve the least squares problem, we form the normal equations and use a

pseudo-inverse, since the design matrix might not:have full rank. The singularity which arises form the inclusion of a constant term for each direction is remedied by simply dropping one column per direction from the design matrix. Higher order singularities caused, for example, by the linear terms for three co-planar directions, are not explicitly taken care,of, but are handled by the pseudo-inverse.

Our knot placement procedure is motivated by the sequential nature of the

algorithm. At each iteration, the knot positions are required for the least squares fit, after the new direction has been found. Our model at this point is the spline fit of the previous iteration, plus the moving average smooth along the newly found direction. The’knot placement is based on the residuals { ri} from this model. Multidimensional structure in these residuals due to incompleteness of the model manifests itself as high lo.cal variability in the scatterplots of ri against a,,, . Xi. In order to preserve the ability of fitting this structure in further iterations, it is important to avoid accounting for it by spurious fits along existing directions. For

this reason we place fewer knots in regions of higher local variability. Since the

(5)

4

The knots along a direction am are placed as follows: the smooth described

above is applied to { (ri, am** xi) }l<i<n and the local variability vi at each point is --

taken to^be the average squared residual from its local linear fit. The Winsorized local variabilities are defined by

if Ui > 2U

if .Vi < it,

otherwise

(where u = ixl<i<, Vi), and then are scaled so that zlCiKn & = 1. The --

knots ( tr } are placed to divide the line into intervals with equal content of &:

for each I, 1 c 1

j,---q+l= am~xi~(wl+l) -. Wi

4. Examples

In this section we present and discuss the results of applying the Multidimensional Spline Approximation method (MASA) to four examples. (A

FORTRAN program implementing MASA is available from the authors.) The first three examples were suggested elsewhere for testing surface approximation procedures. The function in the fourth example was studied in connection with a problem in mathematical genetics.

The first exam.ple is taken from Friedman [1979]. In this example uniformly distributed random points { xi 1 1 5 i 5 200) were generated in the six- dimensional hypercube [O, I]“, Associated with each point Xi was a surface value

yi = 10 sin(Xzi(l)zi(2)) + 2O[Zi(3) -- 0.512 j- lOZi(4) + 5zi(5) + OZi(6) + Ci,

where the { ci} were independent identically distributed standard normal. The inverse figures of merit for the approximation with M = 1,. . ., 4 terms were 6.71,, 4.29,1.87,0.97. In three restarts, the figure of merit did not decrease below

(6)

5

0.86,. so h = 4 was chosen. The four linear combinations and the corresponding

spline functions are shown in figures 1.1-1.4. (For completeness, the program paramerers are also listed; see the program comments for a detailed explanation.) The spline along the first linear combination (figure 1.1) is seen to model the linear part of the surface. The second term in the approximation (Egure 1.2) models

the additive quadratic d.ependence on ~(3). The Enal two terms (figures 1.3, 1.4)

, model the interaction between ~(1) and z(2). The F2 norm of the error ]]f - $112 was 0.57.

Although the full advantages of MASA compared to other procedures are realized in higher dimensional or noisy settings, we applied it to two bivariate examples used by Franke [1979] to compare a number of interpolatory surface approximation schemes.. For both examples 100 uniformly distributed random points in. the unit square [0, 1]2 were generated. The function in Franke’s first example’ is - - f(s, y) = 0.75 exp[--- (” 2)2 I(” 2)2 ] + 0,75exp[- (9x + 1)2 - 9y + l].’ 1o + 0.5 exp[-(” ““1)1+(9y-3)21 -1 0.2 exp[-(92 - 4)2 ” (9y - 7)2].

Considerations similar to those in the previous example led to an approximation

with three terms. The linear combinations and corresponding spline functions are

shown in figures 2.1-2.3.

The function in Franke’s second example is

f(z, y) = i[tanh(Sy - 92) + I].

For this case the approximation used only one term, shown in figure 3.1.

Since different random points were used in Franke’s and our tests, precise

(7)

I

6

of magnitude larger errors than the best methods in Franke’s trials (global basis function methods) while on the second example, MASA gave an order of mag- nitude s%aller errors than the best methods. These results are not surprising.since the peak-shaped basis functions of the global basis methods are especially suited

for representing the peaks of the first example, whereas the ridge-shaped basis

functions of MASA are especially suited to the second example. Unfortunately, peak-shaped basis functions are not appropriate for moderate or higher dimen- sionality. The difficulty is that in order to achieve a smooth fit, the width of the basis peaks. needs to be comparable to the distance between data points. For

n uniformly distributed random points in a p-dimensional hypercube (0, l]“, the

typical nearest neighbor distance is (k)*. In particular for n = 1000 and p =

10, this distance ‘is 0.5, and.for p = 20 is 0.7. Thus variation of the surface

over distances small,compared to such large interpoint distances cannot be well approximated with these global basis functions methods.

Our fin.al example is a 19-dimensional function encountered by Carmelli and

Cavalli [1979]. An important question is the structure .of this function near its

minimum. We sam.pled the function at 200 points uniformly distributed in a small

hypercube centered at the minimum found by numerical optimization and applied

MASA. Th.e inverse figure of merit for the best constant Et was 13.3. The inverse

figure of merit for M = 1 was 0.78. In 30 restarts, the Egure of merit did not

decrease below 0.42. Figure 4.1 gives the linear combination and corresponding

spline function. This picture shows considerable structure that was not revealed

in. the original study.

5. Discussion

MASA can be expected to work well to the extent that the, surface can be

approximated by a function of the form (1). Of course in the limit M --+ co all

smooth su.rfaces can be represented by (l), but even for moderate M functions of this form constitute a rich class.

As seen in the previous section, an advantage of using essentially one-

(8)

7

entire mddel can be represented by graphing Sm(am s x) against a, - x and by

specifyin.g { a, } l<m<M ( per h p g phically for a s ra p = 2 or 3). Additionally, ade-

quacy o?’ thti knot placement can be judged using the M plots of ,the residuals from the final model against a, a x. Proper termination of the algorithm can be

assured by monitoring at each iteration*th.e plot of the residuals from the model

of the previous iteration along the newly found direction.

The problem of sparse sampling in high dimensions is not encountered, since

MASA is fitting one-dimensonal projections of the e&ire sample. The sample need

not’ lie on a regular grid, and the approximation is affine invariant ai;ld smooth.

Function values, derivatives, and integrals are cheap to evaluate. In addition, since the approximation is locally quadratic for Q = 3, optimization algorithms can be expected to converge rapidly.

Carl de Boor

[1978] A practical guide to spjines, Springer-Verlag.

1 Dorit Carmelli and L L Cavalli-Sforza

[1979] 772e genetic origin of the Jews: a multivariate approach, Human Biology

51, 41-61.

William S Cleveland

[1979] Robust locally weighted regression and smoothing scatterplots, J Amer

Stat Assoc 74, 829-836.

Richard Franke

[1979] A critical comparison of some methods for interpolation of scattered.

(9)

8

Jerome H’ Friedman, Mark- Jacobson, and Werner Stuetzle

[1980] Projection pursuit regression, submitted to,J Amer Stat Assoc.

H H Rosenbrock

[1960] An automatic method for finding the greatest or least value of a func-

tion, Computer J 3, 175-184.

‘Larry L Schumaker

[1976] Fitting surfaces to scattered data, in Approximation Theory, (G G

(10)

SP;I;;6;UNC$IC);gND

. . ~~s6ALO~G7~I~ECT~O~5~~ . . . --A. 0146 PLC%&TATI&TICS = 0. 0. 0. / 0. 9. 0. / 0. 0. 0. PRCJ ON Y 3000000000000000010~00000100000000001000000000000000000003 ---+--- --- +---+- ---4-- -+----.-- &XI3 7 ****I LEFT BIN ECGE **** j *** I *** I *** *** z ** *** z ** I ** + *** ** ; ** I ** *** z ** *** ** i *** I ** + t** ** II *** ** : *** I ** ** z ; *** I ** + *** I ** I *** I *** *** I *** I*** 1* t :3 + + + 3: -I-- ----_-- --- --- --- 00000000~l;t;;;0000000~~~~~~~~~~lllllll~~ii~i~llllllll . . . ...* 333334444555556666777778888999990000111112222333334444455556 135793468035791468025791368024791358024691357024681357924680 02468~246802468025791357913579135791357913579135791357913579 888888888999999990080000001111111112222222233333333344444444 ? figure 1.1
(11)

"'~1;~9"~1m9qND . . PLOT&TATASTICS = ON X AXIS 0.0006 I;'$; -0:4848 -3.0737 13,. ;;g -3:5591 r;* g;z -5:6626 :;-;;g -6:1481 -6.3099 -6.4717 LEFT BIN ECGE ? 10 0. 0. 0. / 0. NR ii.0 9. 0. / 0. 0. 0. 300000000000000000001000000000000001000000000000100000000003 $** ; T * T I .. I ** T * *t *T * *i; * *1 ** ** + * * I ** ** I * * I ** ** T ** * * ** ** * * ** ** ** ** * * ** ** * ** ** * ** ** * ** ** ** x* ** * ** ** ** ** ** ** ** ** *** ** *** ** *** *** ***** *** ******** + + + +3

+ --- ---em +- ---_ --- -I-- ---me 0000000~0000000000000000000000000000000000000000000000000001 . . . ..*...*... 000000011111122222333333444444555555666667777778888889999990 102457912468913568013578024579124689134680135780245790246791 074196318630852074297419631853085207429641963185307529742964 314825936047148259360~71482592603714815926037048159~69370481 PRQJ ON Y AXIS figure 1.2

(12)

11 SP~Ibk&JNC~IQ'JD k$JF5lAL!C$G0;;;ECT;Oi NR l . . . . 03.00*3 PLOTJTTATLSTICS = 0. 0. 0. / 0. 9. 0. / 0. 0. 0. ON X AXIS 300000000000000001000000000100~000000001~0000000~00000003 ?. ,222 2 $---t---3--- --- i I J..Z7”ktd 1.6641 I. 'I 83640 1.0638 7 x-3; ":1634 -~,.1368 2*%?

3;

:

1* I*** -I- *** ---f---y -- ******* *** *** *** *** ** *** *** ** **** *** ** * ** ** * ** * ** * ** * ** * * ** * * ** * * ** * * ** . * * I,.,J,A I -1.0373 I *** **** -A.3374 I ---- - ************* -l.bJ-lb I z$';;;g i: -2:5381 I r;=8,g ; -3:4386 I -3.7387 + -a;0389 I I~*~~~~ ; -4:9394 I I;-;;;: ; -5:8398 I -6.1400 I -6.4402 I -9.1416 I -9.4418 I -9.7419 +3 + + + 3-t

+- ---_--_ e-_-e- e-_--v-- ---_ --- ---es LEFT 000000000~0E10000"0~00000000~0000000~00011111~111~1111 BIN . . . EJXE 000111122222333334444555556666677777888899999000001111222223 579135802468035791357024680257913579246802469135791468024681 345789123467801245689023467801235679013457891235679012456890 147036036926925825814714703703693692582581481470470369369259 ? figure 1.3

(13)

12 S'~I~;O;UNC;IWND ~O&ALf;G0~~;ECT;O;6J . . . i.0072 PL;CY&TAT3&TICS = 0. 0. 0. / 0. 9. 0. / 0. 0. 0. PROJ ?00000000000000010000000000010000000001000000000000000000003 i&z ON X AXIS 5.1486 5.0070 4.8654 4.7238 t*2% 4:2991 t---l---t---f---3--- **********- ** *** *** *** ; ** *** :: ** *** ** *** * ** i ** *** : ** ** I ** ** + * *** ** ** * ** : ** ** * ** I ** ** ** ** II * ** I * ** ** ** + z * ** ** * I * ** ** 3; * ** I ** **I * *1 * ** z I EE 1:4674 SE; 1:0426 ;w PI:6179 ix% 0:1931 0.0515 -0.0900 z;- ;+g -0:5148 LEFT BIN ECGE ? + * I ** 7 1* I ,I,: i 1* 1* : 1* I z I' +3 + + + 3: -I- --- +- --- 1-1-- -l- ---e--+---e ---- --- 000000000000000000000000000000000000000~00000000000000000000 . . . . 222221111100000000001111122222333334444455555666667777788888 975319753197531024680246802468024680246802468024680246802468 444444333333333666677777777777777788888888888888899999999999 332110998776544788900122344566788900122344566789901123345567 figure 1.4

(14)

13

MULTIDIMENSIONAL ADDITIVE SPLINE APPROXIMATION (4/19/80) ;$V&METERS FOR2;;IS RUN

NPRED MODE MAXTRY MAXPRO PPCONV MAXIT KORDER EEE? IPRINT 6 2

74

.150000 4 93 2-002000

KR%

1

$VERAGE SQ"ARi? RESIDUAL AROUND THE MEAN 26.7495 .

(15)

14

?

KNOTS ALONG DIRECTION NR 1 PLOT STATI5TICS PROJ ON X AXIS 0.4576 FEE 0:4188 = 0. 0. 0. / 0. 11. 0. / 0. 0. 0. PRCU Ah, v "LY I 3000000~0000000000001000000000010010000010000000000100000003 AXIS + ---I-- -t- ---+---+----+--- I***** i ** *** i I ** T ** T 0.3412

+

---I-- ---+---+----+---

-t-

I*****

i **

***

i

:

**

**

:

:

**

**

z

:

**

**

**

**

z

:

*

*

+

**

**

:

**

**

i

*

*

i

**

**

:

**

**

I

*

*

**

**

z

*

*

:

I ** ** I * * + ** ** * * z ** ** I * * z I ** ** ** ** s :: * * ** ** I I ** ** I + *** *** **** **** + I **** ** **** ** ** ** : I * * ********* *1 II ** ** ** ********I * * *** I

I

**

i

:

**

I I : : i I I t 0.0564 E'%z 0:0176 0.0047 -0.0083 :;* ;g -0:0471 -0.0600

z

+

i

:

z

:

I + z z s I I + : ********* *1 ** ********I *** I T ** ** f

****

1

T . . . . . . . . 111112222233333344444555556666677777788888999990000011111122 134680246802357913579134680246802457913579134680246802457913 009876543210987665432109876543211098765432109877654321098765 900122344566788900122344556778990112334556778990112334556778 figure 2.1
(16)

15 PLOT STATISTICS = PRoJ 0. 0. 0. / 0. 11. 0. / 0. 0. 0. PROJ ON X AXIS 30000000000000010000000~010000000100000001000000000010000003 &: 0.4584 $---t---+---3---+---+---~-

KNOTS ALONG DIRECTION NR 2

0.4454 I ****** C%E : ** ** 0:4066 I ** ** * * 0.3936 I ** ** z*z% : ** * * 0:3548 I ** ** * 0.3418 I * ** ** * * * ** ** * * ** * * * * ** * * ** * * ** * ** * ** ** **** pm; f *,* **** PI:0568 I * *** ** ** ***i ** ** I ** *** ** *** I *** *** I ***** z + + + + + 3: -I-- --- -t- --- ---+---+---+--- LEFT --- BIN 000000000000000000000000000000000000000000000000000000000000 ECGE . . . ..*...*.... 000000000001111122222233333344444555555666666777777888889999 75420124689135680235790246791346801357802457912468913568~235 792470752075308530853085308530853085308530853186318631863186 272724949495050505161616272727283838384949495050505161616272 ? figure 2.2

(17)

16

SPL01bJ;g;UNC;I~;5ND KNOTS ALONG DIRECTION NR 3

. . PLOT&TATpjTICS = 0. 0. 0. / 0. 11. 0. / 0. 0. 0. --a- ON X AXIS 0.2831 EE 0: 2509 PKUJ ON Y 300000000001000000001000000001000000000000010001000000000003 AXIS ? 0.1223 LEFT BIN ECGE +- --- --- +- ---+- --- t _--- ---- : ****** ** ** : I ** ** i * * ** ** ; 3; * * 3E ** ** II * * ** * i t * ** + ** II ; * * : I ** ** : * * ; ** ; .z * * : g : ** * z + ** ** ****** + I 1* * ***** *** I" ** ***** *** 1** ** **** ** : 1* ****** ** I* * i 1* . ** 1* ** I z * i ** I + ** + II * ** I I : *1 *1 I **1 I *1 *1 : i +3 + + + + + 3+ --- -e-D-- ---+---+---+-we- 000000000~0000000~00000000000000000000000000000000000000 . . . ..*... 000000111111222222333333444444555555666666777777888888999999 134679124679124679124679124679124679124679124679124679124679 306396396296295295285285185185184184174174074073073073063063 306284062840639517395173952840628406284173951739517306284062 figure 2.3

(18)

17

MULTIDIMENSiONAL ADDITIVE SPLINE APPROXIMATION (4/19/80) PARAMETERS FORIT;IS RUN

NOBS gg? a liEsoy : 12 PFCONV MAXIT

l 15?000

KORDER !EE? 3 IPRINT 1.~~000 kzE&i 13

GVERAGE SQ"ARi! RESIDUAL AROUND THE MEAN .109703 .

(19)

5 ;;: w c

W + + + ; + + + W W $ + + + + + QJ tHHHHHHHHH+HHHHHHHHH+HHHHHHHHH+HHHHHHHHH

(20)

19

MULTIDIMENSIONAL ADDITIVE SPLINE APPROXIMATION (J/19/80) NOBS. PARAMETERS - FORIT;IS RUN

z PFCONV f MAXIT KORDER l IsYaO 3 .*2000 !ERS 13

eVERAGE SQUAti: RESIDUAL AROUND THE MEAN

(21)

20

S';I;;2;UNd;I;N AND ~~22AL~~G2~~~EC~~O~3~~ -;:;242 : -E039 PI:0556 -A 5495 -0:0384 -0:0141 0:0 fE351 . . -0.0660 -0.0153 -0.0235 PLOT&TA&TICS = 0. 0. 0. / 0. 11. 0. / 0. 0. 0. ON X PROJ AXIS 400000000000000000010000000000000001000001000000000000000004 %I: 29.8919 t---t---t---1---(----1-1+---1--- 29.6401 I* ***** 29.3884 29.1366 28.8848 28.6331 1* *** I* ** 1** ** 1* ** I ** * ** *** I *;**;* I + I ** ** * ** * ** * * ** * I I 27.1225 26.8707 f ** * * ** * * ** * * ** * * ** * * ** * ** * * ** I I I I ; ; z z + + : : : : : : : : I I + + jE jE i i z z i i *+ *+ ***I ***I ,***** ,***** *** *** 1 1 ***** ***** : : ****

;m; II

*

*** 21:0802 I

**

** ** ** %E: E I ** ***

T

20:3249 I **t I 20.0731 I 19.8214 +4 -_-- --- + ---+--- + + 4+ I --- --- LEFT ---I--- BIN EIXE 111111111111111111111111110000000000000000000000000000000000 . . . ...*... 111110000000000000000000009999999999999999999998888888888888 211009988777665544332211009988777665544332211009988877665544 272838394940505161627273838494950506161727283839495050616172 257025803580358036813681368146914691469247924792570257025703 ? figure 4.1
(22)

21

MULTIDIMENSiONAL ADDITIVE SPLINE APPROXIIMATION (4/19/80) PARAMETERS FOR2;;IS RUN

NO%S gg? -cI 19 MAXTRY MAXPRO z PPCONV MAXIT .15:000 KORDER i 1.+;000 EiEE 13

$VERAGE SQ"ARh: RESIDUAL AROUND THE MEAN 13.2975 .

References

Related documents

The threshold into the stadium is through a series of layers which delaminate from the geometry of the field to the geometry of the city and creates zones of separation,

Spending remained relatively stable despite the sharp drop in available impressions precipitated by the rollout of IQ — proof positive that the invalid traffic wiped from

Configuring the Global Default Properties of the JMS Provider Service You can configure global properties of JMS virtual providers via the Config Tool1. Start the Config Tool

Ste.. Leslie Johnson, Jr.. David Abernethy P.O.. Scott Lindsay P.O.. Craven Bernard Bush P.O.. Mark Warren P.O.. Marietta Street [email protected].. Gastonia,

We observe that leverage is statistically significant, thus suggesting a negative relation between leverage and average wages, but only when considering the specification that

Conversion factors used to determine fee schedule payments for anesthesia services furnished by qualified nonphysician anesthetists on or after January 1, 1992, are determined

• 2011: Patients with peripheral T-cell lymphoma (PTCL) who received at least one prior therapy. – Two phase 2, single-arm, open-label trials in

To account for the difference in the number of choker chains between the main and tagline, the cycle element times for travel empty and loaded, and load size of the