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Annual Report 2000 - WIT

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!¥”“Z• Ç ¤<br />

ɨ§<br />

—<br />

‘<br />

• Ç u<br />

¡<br />

ÿ Ú<br />

²<br />

£ ’<br />

<br />

ý<br />

<br />

Ç<br />

¦<br />

‘ %$ ’ ‘ ¥”“'& ¤ ¡ Ú ‘ ($ ’ ‘£¢ « »¨¼ Ú ‘ ($<br />

Ú<br />

Í<br />

¢<br />

<br />

224<br />

tion introduced by (Bortfeld, 1989). (Hubral et al., 1992) give the normalized geometrical<br />

spreading in terms of the matrices of second order derivatives of traveltimes. This<br />

is<br />

ú ´<br />

‘<br />

(C-1)<br />

where œƒž œ1 the angles are the emergence<br />

ܾ<br />

Š angle at and the incidence Š angle at<br />

and can be determined from the slownesses at ¸ these positions. is the KMAH-index of<br />

the<br />

Ý<br />

Š<br />

ray connecting .<br />

œƒž9¨šA› œ1 ŸšA› £ |~} ¦ § î î<br />

| ²#³<br />

žãù<br />

ݾ<br />

For a 2.5-D situation we find that<br />

|Ÿ}±¦ § • ¦ § ÚÚZû ¦ § ’’<br />

(see Appendix B) and therefore<br />

£<br />

expression (C-1) can be reduced to the simple form<br />

Ü<br />

and Š<br />

• Ç ü<br />

¡<br />

ú ´ <br />

(C-2)<br />

œ·ž9ŸšA› œ1 ¨š› § ÚÚ î îo¦<br />

|²#³<br />

This result is no surprise since (Bleistein, 1986) found the relationship between the outof-plane<br />

spreading commonly denoted by þ and the second order traveltime derivative<br />

in out-of-plane direction. Thus we have<br />

§ ’’<br />

ž–ù<br />

• Ç<br />

¦ § ’’ þ<br />

(C-3)<br />

So far, however, it was common practice to determine the out-of-plane spreading from<br />

the integral along the ray Š from<br />

½ª¿<br />

½<br />

to Š<br />

þ •$ÿ £ ܃¡<br />

(C-4)<br />

with Ü being the arclength and ¡ the velocity. We compute this quantity from traveltimes<br />

and do not have to trace rays to determine þ .<br />

APPENDIX D<br />

Equations (4) and (5) are expressions for weight functions if the diffraction stack is<br />

carried out over the aperture in<br />

Ú<br />

and<br />

’<br />

. Since in the 2.5-D case we have only data<br />

from a single acquisition line (assumed to coincide with the<br />

Ú<br />

coordinate), we only<br />

integrate<br />

Ú<br />

over . In this case we ¡ Ú ‘ ’¨‘£¢ “±• ¡ Ú ‘ ‰ ’ ‘£¢ “<br />

have where the asterisk<br />

denotes the stationary point. Inserting the according expression for the input traces (2)<br />

into the stack integral (1) then leads to<br />

¢ “<br />

(D-1)<br />

¦¥”“Z• Ã Ç ¤ ÿ© £<br />

ɨ§<br />

‘ ’¨‘ ¥”“ ü Ú<br />

Í<br />

Carrying out the integration over<br />

’<br />

following (Martins et al., 1997) we get<br />

Ž<br />

¢¢¢¢¢<br />

¦ Ò ú Ò <br />

ÿ © £ Ú Â’£" #<br />

’ ‘ ¥”““ ¯ (D-2)

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