NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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NAVIGATION QUALITY FROM LAKE BAIKAL 1992 MULTICHANNEL SEISMICS CRUISE I04P 106' IIO°E 6°N LAKE BAIKAL MCS TRACKS 1989 MCS TRACKS 1992 MCS TRACKS by Deborah R. Hutchinson U.S. Geological Survey Woods Hole, MA 02543 Open-File Report #95-233 1995 This report is preliminary and has not been reviewed for conformity with U.S. Geological Survey editorial standards and nomenclature. Use of trade names is for purposes of identification only and does not constitute endorsement by the U.S. Geological Survey.

Transcript of NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Page 1: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

NAVIGATION QUALITY FROM LAKE BAIKAL 1992 MULTICHANNEL SEISMICS CRUISE

I04P 106' IIO°E 6°N

LAKE BAIKAL MCS TRACKS 1989 MCS TRACKS 1992 MCS TRACKS

by

Deborah R. Hutchinson U.S. Geological Survey Woods Hole, MA 02543

Open-File Report #95-233

1995

This report is preliminary and has not been reviewed for conformity with U.S. Geological Survey editorial standards and nomenclature. Use of trade names is for purposes of identification only and does not constitute endorsement by the U.S. Geological Survey.

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TABLE OF CONTENTS

Introduction .......... 3Acknowledgements ......... 3Cruise Summary ......... 3Field Procedures ......... 8

Navigation Logging ........ 8Multichannel Shot Logging ....... 8Calibration of Navigation and Shot Numbers .... 8

Sources and Magnitude of Navigation Error ..... 8Measurement Limitation ....... 8Shot-Time Calibration ....... 9Missed Shots ......... 10

Processing Strategy ......... 12Results .......... 15

Quality of the Raw Navigation ...... 15Quality of the Calibration Files ...... 15Quality of the Distance Between Shots . . . . . 16Quality of Shot Locations ....... 22Line Crossings ........ 22

Discussion .......... 22Conclusions .......... 27

References Cited ......... 28

Appendix 1: Plots of Raw GPS Navigation ..... 29Appendix 2: Plots of Shot-Time Calibration and Shot-Distance Information . 101Appendix 3: Line Crossings ....... 158

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INTRODUCTION

In August-September, 1992, a comprehensive multichannel seismic-reflection survey was conducted in Lake Baikal, Siberia (Figure 1), by U.S. and Russian scientists (Klitgord et al., 1993). Navigation utilized U.S.-supplied Global Positioning Satellite (GPS) receivers. Pre-cruise uncertainty in the availability and quality of the GPS positions at Lake Baikal together with limitations in both the ships layout and the navigation software resulted in (a) the seismic source being fired by increments of time rather than increments of distance and (b) navigation being acquired independently of the multichannel shot data. Because the navigation and multichannel data were not linked, the challenge in processing the shot point data was to assign an accurate time to each shot so that its position could be estimated from the raw navigation data.

The purpose of this report is to describe how times for each shot were derived, to describe how the positions were established for each shot number; and to assign a quality factor to the navigation for each line. The implications of these results for the geometry and processing of the multichannel seismic data are also discussed. This report complements other reports about the scientific objectives and operations of the cruise (Klitgord et al., 1993; Nichols et al., 1992) and the processing of the multichannel seismic profiles (Agena et al., 1994).

ACKNOWLEDGEMENTS

The success of the field program is due to the combined efforts of Russian and American scientists who participated in the R/V Balkhash multichannel cruise (Klitgord et al., 1993). I thank Warren Agena for his detailed accounting of missed shots based on observers logs and processing experience, Chris Schneider for developing the initial Matlab routines for displaying the navigation information, and Chuck Denham for advice and guidance in developing subsequent Matlab routines. Discussions with Barry Irwin, Uri ten Brink, and Chris Schneider helped focus many of the analyses presented here. Constructive reviews by Barry Irwin and Dave Foster are appreciated.

CRUISE SUMMARY

Approximately 2,250 km of multichannel seismic profiles were collected aboard R/V Balkhash in Lake Baikal in 1992 (Figure 1). Line numbers were assigned based on whether the lines were dip lines across the lake (even numbers) or tie lines along the lake (odd numbers). Because unequal numbers of dip and tie lines were shot, the line numbers are not sequential. There are 42 separate lines with numbers which range from 1 to 60. An additional 6 segments comprise reshot lines (3A, 10A, 17A, 40A, 50A, and 50B). Hence there are a total of 48 line segments for purposes of processing. The reshot lines have been given numerical designations of 61 - 66 (Table 1) for the purposes of navigation processing in this report but should otherwise be labelled by their A and B names officially, as shown on Plate 1. Line 17A (66) is a reshoot of line 17 with large-volume air guns and a slower firing rate (120 seconds) because of coincident recording of Ocean Bottom Seismometer data (ten Brink et al., 1993). The other A and B lines were reshot because of acquisition or navigation errors and are continuations of the original lines.

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!IO°E 56°N

90° 120° 150° 180

150 ACADEMICIAN RIDGELAKE BAIKAL

92 MCS TRACKS

MERCATOR PROJECTION

Figure 1. Map of Lake Baikal showing locations of 1992 multichannel seismic reflection lines. Detailed shot point map shown with locations of shot-time calibration points is shown at 1:1,000,000 in Plate 1.

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FIELD PROCEDURES

Navigation LoggingNavigation data were taken from an Ashtech GPS Model XII Receiver, using frequency

band L-l (1575 MHz) and signal modulation code C/A. The Ashtech antenna was located on a cross tree above ship's bridge. Every 10 seconds, navigation information was transmitted through an RS-232 port to a personal computer for logging. Logged data consisted of date, time, latitude, longitude, ellipsoidal altitude, Horizontal Dilution of Precision (HDOP) value, speed, and heading. No raw GPS signal information was saved from the multichannel tracks. The personal computer also provided real time displays for use in navigating the ship, such as distance along line, distance off track, distance and time to next way point, etc. Archive media for the navigation data were floppy disks from the portable computer.

Multichannel Shot LoggingThe multichannel seismic acquisition system consisted of a Texas Instruments DPS V

computer with dual 1600-bpi tape drives. A Digital Timing Delay Generator, i.e., a calibrated digital clock, issued a master trigger to the DPS V which initiated the firing pulse to the air gun array. The desired shot interval of 50 m was approximated by matching the time between shots with averaged ship's speed. Shots were generally fired every 23 to 25 seconds corresponding to a ship's speed of 4.0 to 4.4 kts, although some lines had shot intervals as low as 22 s and as high as 27 s. Firing rates were generally not varied within single lines.

Individual shot numbers were logged as the record or file number written onto the DPS V tape drive. Shot numbers for this cruise are therefore exactly equivalent to Field File Identification (FFID) numbers used in processing the multichannel data.

Calibration of Navigation and Shot NumbersThe shot numbers were calibrated to the navigation data manually at 15-minute intervals.

The navigation watch stander logged the DPS V file number as an entry in the hand-written navigation log at 15-minute increments (about 35 to 40 shots). These entries were later typed as date-time-shot number files for processing the navigation, and are called shot-time calibration files.

SOURCES AND MAGNITUDE OF NAVIGATION ERROR

Three sources of error contribute to uncertainty in the Baikal navigation: (1) measurement limitation, (2) shot-time calibration, and (3) missing shots.

Measurement LimitationThis is error inherent in the hardware, software, and geometry of the GPS satellite and

receiver system. The most variable source of error comes from the geometry of the satellites used in calculating the navigation position, and is referred to as the Dilution of Precision (DOP) factor (Milliken and Zoller, 1980; Hum, 1989). OOP's are numerical values that can be recorded for 3-dimensional solutions (PDOP - Position Dilution of Precision), for 2-dimensional solutions (HDOP - Horizontal Dilution of Precision or VDOP - Vertical Dilution of Precision), and for time solutions (TDOP - Time Dilution of Precision). For the Baikal data, HDOP was recorded

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rather than PDOP because navigation solutions on a lake surface are essentially made at the same vertical elevation. This also allowed for 3-satellite solutions to be used if 4-satellite solutions were not available. HDOP values for good satellite geometries are generally between 1 and 4; values for poor geometry are much larger.

Other sources of measurement error are generally constant and are summarized below (Table 2):

TABLE 2: Typical Sources of Measurement Error1

SOURCE

Satellite Clock

Ephemeris

Receiver

Atmospheric/Ionospheric Effect

Selective Availability2

Root-Square Sum3

Baikal estimate

ERROR (M)

.6

.6

1.2

3.7

0-7.6

4-9

7

DESCRIPTION

Clock Drift

Uncertainty in satellite orbit

Clock synchronization with satellite

Signal propagation delays

Random signal degradation

Estimated Combined Error

Assumed mid-value

1 Source: Hum (1989).2 Selective Availability is unannounced degradation of the signal by Department of Defense. This is the most

unconstrained source of error. 7.6 m is considered worst case.3 Root-Square Sum is the square root of the sum of the squares.

Total measurement error is calculated by taking the product of the HDOP value with the root-square sum of the other sources of error (Hum, 1989). For the Baikal data, a representative root-square sum value of 7 m is assumed. The measurment error in meters is therefore taken as 7 times HDOP.

Shot-Time CalibrationThis refers to the logging of time and/or shot numbers at the 15-minute calibration points.

The magnitude of this error is related to human error in logging time and and/or shot number correctly at the calibration points. Ideally, the clock used to fire the airgun array should have been synchronized to the GPS clock and shot-time recorded automatically to a fractional second. In actuality, the (GPS) times at calibration points were logged to whole seconds (best case) or whole minutes (worst case). Logging time in whole minutes was most common at the beginning of the cruise because of language difficulties between some of the Russian and American watch standers. Very few of these human errors occurred in the latter part of the cruise.

These errors in time are given values of 1 s (for whole second logging) and 30 s (for whole minute logging, assuming time is rounded to the nearest whole minute). To convert these errors in time to position error in meters, the mean distance between 10-s positions was either divided by 10 (to get mean distance for 1-s interval) or multiplied by 3 (to get mean distance for 30-s interval). The magnitude of the uncertainty due to the 1-s error is about 2 m; that for the 30-s case is about 70 m.

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Shot-time errors could also occur if shot numbers were improperly logged. Occassionally, shots from the navigation log showed gross inconsistency with the multichannel observer's logs, indicating that the watch stander erroneously recorded the shot/file number. The more obvious errors could be corrected after comparison of the navigation logs with the multichannel observer's logs.

Missed ShotsThis refers to situations in the field in which the airgun array continued firing at even

increments of time even though the DPS V was not recording the shot or incrementing the file/shot number. The actual shot-time calibration points are based on the field file numbers from the DFS-V, rather than the actual firing of the airgun array, which means missed shots are not automatically counted. In the first half of the cruise, several poor quality tapes together with excessive parity errors on one of the tape drives resulted in missed shots. In the second half of the cruise, when only one tape drive was used, two firings were missed at every tape change because of the physical limitations in removing and reloading a single tape drive. For times in which missed shots occured, the navigation interpolation must include a correction for the additional shots that occurred in that interval.

In order to compensate for the missed shots, the concept of a "pop" number is introduced for the processing. The pop number differs from the shot number in that the pop increments every time the air-gun array fires whereas the shot number increments only when the DPS V writes a file to tape. Missed shots (i.e., those not recorded on the DPS V) will introduce a systematic offset between the pop number and the shot number. Both pop and shot numbers should be identical for lines in which no recording errors (i.e., missed shots) occur. The concept of the pop number for the Baikal data is used only in the processing of the navigation information and is not logged in any of the final archive navigation files.

Figure 2 shows a hypothetical situation to emphasize the effects of poor logging and missed shots on estimating the time of each shot. Time is shown incrementing to the right, with a 15-minute calibration interval noted. (Assuming a constant ship's speed of 4.5 kts, this hypothetical time curve can also be equated with distance, or 15 minutes equals about 2.1 km). Suppose there are 15 shot numbers recorded from minute 1 to minute 15 (i.e., 15 files written on the DPS V). If there are no missing shots, then the shot number equals the pop number and configuration A holds for interpolating 15 even intervals for the shot times. However, if there are 5 missed shots (shown as *), then the pop number exceeds the shot number by 5 and configuration B (20 even time intervals) is the accurate representation for determining the shot times. If the missed shots are not accurately accounted for, then the shot time will be correct at the calibration points (shots 0 and 15), but will be misestimated (by up to 2.25 minutes for shot 6). This timing error for shot 6 equals a distance mislocation of 313 m in this example. In general, this error is greatest at the position of the missing shots and decreases toward the 15- minute calibration points.

If the time is not logged properly for the 15-minute calibration, then a shot-time calibration error is introduced. For whole minute logging, the timing error is assumed to be 30 s (i.e., watch stander recorded the whole minute to the nearest whole minute). The effect on estimating shot time is shown by configuration C in Figure 2, where one scenario is illustrated in which the whole minutes reported are considered to be off by 30 seconds at each calibration

10

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10

15

20

5 10

15

O

OO

OO

OO

OO

OO

OO

..I

i 1

.1

i

I .

i i

...

....

i ...

....

i.

..l

...

...i.

.. 1

i..

C.

B.

, A.

Who

le M

inut

e Lo

ggin

g

Mis

sing

Sho

ts

No

Err

ors

1015

Min

utes

Figu

re 2

. T

hree

sce

nario

s fo

r es

timat

ing

shot

tim

es i

n a

fift

een

min

ute

inte

rval

fro

m s

hot-

time

calib

ratio

n fil

es.

For

sim

plic

ity,

one

shot

per

min

ute

is a

ssum

ed.

Shot

poi

nts

are

show

n by

ope

n ci

rcle

s; m

issi

ng s

hots

(i.e

., w

hen

the

airg

un a

rray

fir

ed,

but

no f

ile w

as

reco

rded

on

the

DPS

V)

are

show

n by

*.

The

first

and

las

t po

int

for

each

of

the

thre

e co

nfig

urat

ions

is

the

logg

ed c

alib

ratio

n po

int

at m

inut

e 1

and

min

ute

15.

(A).

No

erro

rs:

In t

his

case

, th

e tw

o ca

libra

tion

poin

ts a

t m

inut

es 1

and

15

are

used

to

inte

rpol

ate

15

shot

s, o

r a

shot

at

each

min

ute.

Sh

ot n

umbe

r 5

(fill

ed c

ircle

) co

rres

pond

s to

min

ute

5.0.

(B

). M

issi

ng S

hots

: In

thi

s ca

se,

five

mis

sing

sho

ts (

*) o

ccur

bet

wee

n sh

ot 5

and

6.

The

cor

resp

ondi

ng p

op n

umbe

r is

sho

wn

bene

ath

the

row

of s

hots

. In

thi

s ca

se,

ther

e ar

e 20

sho

ts i

n th

e ca

libra

tion

inte

rval

and

sho

t 5

wou

ld b

e as

sign

ed a

tim

e of

4.0

min

utes

. (C

) W

hole

Min

ute

Log

ging

: Fo

r th

is

case

, if

the

act

ual

calib

ratio

n sh

ots

occu

rred

at

min

utes

1.5

an

d 15

.5 (

i.e.,

30 s

econ

ds a

fter

the

min

ute)

, th

en t

he t

imes

sho

uld

be

calc

ulat

ed a

s sh

own

here

. Sh

ot 5

occ

urs

at 5

.5 m

inut

es.

How

ever

, if

who

le m

inut

e lo

ggin

g w

as d

one,

the

sho

ts w

ould

be

calc

ulat

ed

sim

ilar

to c

ase

A.

Page 12: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

point. Configuration C shows what the actual shot times should have been; configuration A shows how they would be calculated in the absence of the seconds information. In this case, the calibration shots 0 and 15 would have an error of 30 seconds (69 m), as would all shots in that interval.

The missing-shot error is actually treated as a correction to the data rather than as an error; i.e., missing shots are accounted for in the processing, but no missing-shot error is calculated or assigned. This assumes that the missing shots were reasonably carefully logged and that any unlogged shots are not enough to bias an entire line. Most of the missing shots compensated in the processing are single or double shots (representing a timing correction of up to 45 s at the position of the missed shots, or up to about 100-m correction). The most missing shots that occurred at one interval are 17 on line 6. One or two missed shots generally has no visible-effect on fold coverage of the multichannel data. However, the 17-shot gap in line 6 was sufficient to cause a small data gap at SP 820-821.

PROCESSING STRATEGY

Two basic inputs are used in processing the navigation: the raw 10-s locations and listings of the shot-time calibrations points. The steps in processing the navigation data (Figure 3) were:

(1) Inspect the overall quality of the raw navigation data by looking at gaps and calculating the distance between adjacent fixes for each 10-second recording point. Plot ellipsoidal height and HDOP value for general quality control.

(2) Evaluate the quality of the shot-time logging, which was done by calculating firing rate for each 15-minute calibration interval and inspecting the scatter. Ideally, with a constant firing rate of the airgun array, the recomputed firing times for each 15-minute period should also be constant, or vary slightly when the firing rate was infrequently adjusted for changes in the ship's speed.

(3) Edit the calibration files for obvious typographical errors based on the magnitude of the scatter observed in plots from step 2.

(4) Develop and merge the best estimates of the number and positions of missing shots with the calibration files. In this step, the pop numbers were defined.

(5) Generate final latitude/longitude positions by using the updated calibration files to interpolate times for each pop, which are then merged with the raw navigation files to interpolate latitude and longitude for the pop times. Final archive navigation drops the pop numbers which do not have accompanying shot numbers defined.

(6) Inspect the quality of the shot navigation by looking at the distance between adjacent pops for each line.

(7) Assign an error to each line based on the quality of the raw navigation and the errors introduced in the calibration files.

Plots showing the results of step 1 are given in Appendix 1 for each line. Plots resulting from steps 2, 4, 5, and 6, are given in Appendix 2 for each line.

12

Page 13: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

RAW GPS NAVIGATION

SHOT-TIMECALIBRATION

FILES

Analyze Raw GPS

I Edit

AddMissingShots

Interpolate Times For Each Shot

Interpolate Position For Each Shot

Analyze Shot Distances

FINAL PLOTS

Figure 3. Flow chart of the navigation processing.

13

Page 14: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

TABLES: DATA GAPS

Line No.

6

7

7

8

8

8

8

11

13

13

13

13

13

13

17

26

34

38

46

46

50

50

52

66

66

START OF GAP

Date

920826

920829

920829

920826

920827

920827

920827

920922

920920

920920

920921

920921

920921

920921

920916

920831

920922

920910

920913

920913

920912

920912

920922

920916

920917

Time

175622

190902

191032

233412

011652

012702

024802

195412

225812

234632

035032

035452

065652

121612

050002

174122

003132

134342

082032

083642

181132

193252

090112

164852

112842

END OF GAP

Date

920826

920829

920829

920826

920827

920827

920827

920922

920920

920920

920921

920921

920921

920921

920916

920831

920922

920910

920913

920913

920912

920912

920922

920916

920917

Time

180302

191012

191302

233522

012612

013242

025102

195632

230212

235302

035322

035722

070112

121822

054122

175132

003432

134642

082432

083802

181232

193352

090232

170832

113242

LENGTH(s)

400

70

150

70

560

340

180

140

240

390

170

150

260

130

2480

610

180

180

240

80

60

60

80

1180

240

SHOTS IN GAP

Total

16

2

6

2

23

14

7

6

10

15

7

6

11

6

108

25

6

7

10

3

2

2

4

9

2

SP Nos.

909-924

526-527

529-534

284-285

530-552

555-568

748-754

324-329

444-453

555-569

1107-1113

1117-1122

1543-1553

2353-2358

2866-2973

148-172

509-514

700-706

22-31

63-65

236-237

432-433

58-61

51-59

605-606

14

Page 15: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

RESULTS

Quality of the Raw NavigationRaw navigation information is illustrated in Appendix 1 with four plots for each line:

distance between each data point (top plot), time between each data point (second plot), HDOP value associated with each data point (third plot), and ellipsoidal height (bottom plot).

The plots of distance between each point show considerable scatter on some lines (e.g., line 4, with a standard deviation of 13.6 m) and remarkably little scatter on others (lines 23, with a standard deviation of 1.44 m). The 10-s positions average about 20 - 23 m apart throughout the cruise, and the standard deviations range from about 5 % (line 23) to more than 50 % (line 4).

In general, the scatter is correlated to changes in HDOP value (e.g., HDOP changes rapidly on line 4 and is less variable for line 23). This correlation suggests that the scatter is best explained by changes in satellites and/or satellite geometry used in computing successive positions along a track line.

Because data points were logged every ten seconds, the plot of time between data points should be constant at 10 s. Deviations from this represent data gaps. Note that data gaps in time are duplicated as large peaks in distance between points (e.g., line 8 at 3.75 - 4.0 hours). Table 3 summarizes the data gaps for the 14 lines with gaps of 1 minute or more (i.e., 6 or more data points lost). The two largest gaps were on lines 17 and 17A, in which data losses occurred of 41.3 and 19.6 minutes respectively.

Measurement error can be estimated directly from the raw navigation. Table 4 lists the mean measurement error for each line. As defined earlier, the measurment error is given as 7 x HDOP, where HDOP is the mean HDOP calculated for each line. These errors range from 7.49 m (lines 42 and 52) to 22.75 m (line 40). Figure 4 (top plot) illustrates these errors, shown as X's together with estimates of the scatter (standard deviation of the calculated distance between data points), shown as O's. In general, the two values are in good agreement. The error bars are the standard deviation of the error, and are primarily an indicator of the amount of scatter in the HDOP value.

Quality of the Calibration FilesPlots of the initial and final calibration files are shown as the upper two plots in the

figures in Appendix 2. The calibration curves are displayed as firing rates, calculated by dividing the time between control points by the number of shots between control points. The control points plotted in the edited (final) version use pops between control points to calculate the shot interval, although the information is plotted against shot numbers. Ideally, these lines should be constant and horizontal along the line, because the pops were fired by time, or they should show a small offset where the shot number may have been adjusted for small changes in the speed of the ship.

All of the plots of the initial calibration files show a boxy pattern, in which the shot interval varies between high (24 - 27 s) and low (21 - 23 s) values. This is a direct result of poor record keeping and missing shots. After editing, some of the lines have excellent (i.e., flat)

15

Page 16: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

curves (e.g., lines 54 and 58). Many of the lines show considerable improvement in the flatness of the calibration curves after editing (e.g., lines 11 and 13) whereas a few show little or no improvement (e.g., line 15). The final calibration curves have been assigned a rating of 1 (time logged to whole seconds) or 30 (time logged to whole minutes); these values are listed in Table 4, together with the calculated error in distance that these timing errors correspond to.

Lines in which some or all of the calibration points were logged to whole minutes were given ratings of 30, even if the final curves looked reasonable, because of the absolute uncertainty in shot time based on the poor time-keeping, as described with Figure 2. For example, line 6 is given a 30-s error value for the entire line even though whole minute logging occurred only in the first half of the line. Line 7, one of the long tie lines across the Selenga Delta, contains whole-minute logging for only about 25 % of the line (600 shots from about SP 1000 - 1600), but is also assigned a 30-s error for the whole line. The portions of lines which had whole-minute logging are clearly marked in Appendix 2, and should be inspected to clarify how much of any line is affected by the whole-minute logging.

The shot-time calibration error was combined with the measurement error using a root- square sum to yield total error for each line. Figure 4B shows the total error (i.e., for both measurement and shot-calibration errors). A comparison of this figure with the measurement error (Figure 4A) reveals the large contribution of the shot-time calibration error due to the whole-minute logging (30-s error). For example, line 4, which has a measurement error of 8.89 m, has a combined total error of about 74 m when the shot-time calibration is added. The difference between the measurement error and the total error for lines with a 1-s shot-time calibration error is generally negligible.

Quality of the Distance Between ShotsThe quality of both the raw navigation and the calibration files affects the calculations of

distances between shots. These distances are shown in two forms in Appendix 2 (lower two plots): as relative distance between shots along each line (third plot down) and a histogram of distances (lowest plot). The plot of distance between shots gives a good representation of the magnitude of the scatter along the line; the histogram illustrates the spread of the scatter. All plots are at the same scale for easy comparison. The standard deviations given on the plots are based on the relative distances between shots, rather than the uncertainty associated with the absolute position of the shot.

The scatter recorded for distances between shots essentially mirrors that of the raw navigation plots (compare plots for each line in Appendix 1 and Appendix 2). The distances between shots are important for evaluating the assumption of 50-m shots used to process the multichannel data. Figure 5 shows the mean distance between shots (X) together with the standard deviation (error bar) for each line. The ideal shot distance of 50 m is also shown as a horizontal line.

Except for line 30, the error bars encompass the 50-m ideal shot spacing. Hence the assumption of 50-m shots is valid for processing the data. Line 30 has a mean shot spacing of 57-m, but is a very short line (174 shots) and therefore is a very small element of the entire data set.

16

Page 17: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

A.

ME

AS

UR

EM

EN

T E

RR

OR

100

80 60

o> g

40CO

20

x- A

bsol

ute

Mea

sure

men

t E

rror

O

- E

rror

Mea

sure

d by

Sca

tter

O

O

1 2

3 4

6 7

8 9

10

11

12

13

14

15

16

17

18

19 20

21

22 23 24 25

26

28

30 32

34 36

38

0

42 44 46

48

50

52

54

56 58

60

61

62 63

64 65

Line

num

ber

10

0r

80 60 40 20

B. T

OT

AL

ER

RO

R

I f

X

1 2

3

xx

x

10

11

12

13

14

15

16

17

18

19 20

21

22

23 24 25

26

28 30 32

34

36

38

40

42 44

46 48

50

52

54

56 58

60

61

62 63

64

65

Line

num

ber

Figu

re 4

. Pl

ots5

of e

rror

. (A

) M

easu

rem

ent e

rror

for

eac

h lin

e (X

) pl

otte

d w

ith s

tand

ard

devi

atio

n (s

how

n as

the

err

or b

ar).

The

se m

easu

rem

ent e

rror

s ar

e al

so

tabu

late

d in

Tab

le 4

. Th

e st

anda

rd d

evia

tion

is pr

imar

ily a

ref

lect

ion

of th

e sc

atte

r in

the

HD

OP

valu

es.

The

sca

tter

in t

he d

ista

nce

betw

een

10-s

pos

ition

s (U

) is

also

plo

tted

for

each

lin

e an

d is

gene

rally

con

sist

ent

with

the

mea

sure

men

t er

ror.

A l

ight

dot

ted

line

is sh

own

alon

g th

e ze

ro v

alue

(B

) To

tal

erro

r gi

ven

as t

he e

rror

due

to b

oth

the

mea

sure

men

t and

sho

t-tim

e ca

libra

tion

valu

es.

The

dif

fere

nce

betw

een

the

mea

sure

men

t err

or (

show

n in

the

uppe

r pl

ot)

and

the

tota

l er

ror

(sho

wn

in t

he lo

wer

plo

t) is

due

to

the

cont

ribut

ion

of th

e la

rge

shot

-tim

e ca

libra

tion

erro

r fo

r 13

lin

es

Page 18: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

TABLE 4: NAVIGATION ERROR AND DATA QUALITY

LINE NUMBER

I

2

3

4

6

7

8

9

10

11

12

13

14

15

16

17

18

19

20

21

22

23

24

25

26

28

30

32

34

MEAN SHOT DISTANCE1

52.84

54.47

49.47

54.83

50.59

50.74

53.02

49.95

55.33

50.03

47.86

51.71

45.37

51.06

46.74

49.22

49.45

52.21

50.76

55.93

52.49

52.21

50.87

51.57

53.26

47.06

57.32

51.35

50.98

MEASURE­MENT

ERROR2

7.98

9.17

8.68

8.89

8.33

10.15

8.05

9.38

7.70

9.10

10.43

8.89

7.63

7.77

7.84

9.31

12.25

11.27

9.31

12.46

9.31

6.93

8.68

9.80

11.13

12.95

12.04

9.17

8.12

SHOT-TIME CALIB.

Factor3

30

30

30

30

30

30

30

1

30

1

1

1

1

1

30

1

1

1

30

1

30

1

1

1

1

1

1

1

1

Error4

60.51

64.14

58.50

73.68

64.83

61.50

69.84

2.01

70.71

2.23

1.99

2.15

1.85

2.20

56.40

2.28

2.02

2.27

61.53

2.37

64.89

2.09

2.04

2.27

2.31

1.93

2.22

2.19

2.33

TOTAL ERROR5

61.03

64.79

59.14

74.21

65.36

62.33

70.30

9.59

71.13

9.37

10.62

9.15

7.85

8.07

56.94

9.58

12.41

11.50

62.23

12.68

65.55

7.24

8.92

10.06

11.37

13.09

12.24

9.43

8.45

RATING6

Poor

Poor

Poor

Poor

Poor

Poor

Poor

Excellent

Poor

Excellent

Excellent

Excellent

Excellent

Excellent

Poor

Excellent

Good

Excellent

Poor

Good

Poor

Excellent

Excellent

Excellent

Excellent

Good

Good

Excellent

Excellent

18

Page 19: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

36

38

40

42

44

46

48

50

52

54

56

58

60

61/10A

62/3A

63/40A

64/50A

65/50B

66/1 7 A

53.18

50.97

56.18

52.74

51.08

51.93

54.45

54.27

50.81

50.49

50.16

51.16

52.66

49.49

53.33

52.46

50.51

50.15

257.15

17.08

7.70

22.75

7.49

8.96

7.84

8.33

12.67

7.49

7.84

8.19

9.17

7.84

10.01

8.75

8.68

6.37

8.12

8.61

1

1

1

1

1

1

1

1

1

1

1

1

1

30

30

1

1

1

1

2.39

2.06

2.28

2.22

2.08

2.20

2.21

2.22

2.19

2.20

2.18

2.14

2.22

60.90

65.52

2.20

2.02

2.17

2.19

17.25

7.97

22.86

7.81

9.20

8.14

8.62

12.86

7.80

8.14

8.47

9.42

8.15

61.72

66.10

8.95

6.68

8.40

8.88

Good

Excellent

Good

Excellent

Excellent

Excellent

Excellent

Good

Excellent

Excellent

Excellent

Excellent

Excellent

Poor

Poor

Excellent

Excellent

Excellent

Excellent

'Mean Shot Distance - Mean distance between successive firings of the airgun array after taking into account allmissing shots. This same number is given in Appendix 2 on the top plot for each line.

:Measurment Error - Error due to inherent limitations of the satellite-receiver system. This number is taken to be7 times mean HDOP, as discussed in the text.

3Shot-Time Calibration Factor - This is the factor assigned to each line based on the quality of the shot-timecalibrations. 1 refers to times recorded to whole seconds; 30 is for times recorded to nearest whole minute.

4Shot-Time Calibration Error - This error is given as the average distance between 10-s navigation locations (top plotof Appendix 1) multiplied by .1 (1-s factor) or 3 (30-s factor).

5Total Error - Taken as the root-square sum of the measurement and shot-calibration errors. 6Rating - Excellent is for error of 6-12 m; Good is for errors of 12-24 m; Poor is for errors > 50 m.

19

Page 20: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 22: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Quality of Shot LocationsFor the purposes of this report, an error estimate is assigned to each line based on the

mean characteristics of the line (e.g., mean HDOP), rather than assigning an error estimate to each individual shot. This gives a general guide for interpreting the navigation quality for each multichannel profile.

Figure 6A gives the total position uncertainty for each line plotted as an error bar around the mean shot distance. The value of the error bar is taken as the total error (X) shown on Figure 4B and tabulated in Table 4. The lines with whole-minute logging of the shot-time calibration points are ovvious because of their large error bars (e.g., lines 1-8).

A quality rating has been assigned to each line based on the size of the total error and is illustrated in Figure 6B. The lines have been arranged in order of increasing error-bar size. Lines with error bars of 6-12 m are considered to have excellent navigation; those with error bars of 12-24 m (i.e., up to half a shot interval) are considered to have good navigation; and those with error bars in excess of 50 m (i.e., one shot interval) are considered to have poor navigation.

Line CrossingsLine crossing information has been compiled from the processed navigation locations for

each multichannel line and is given in Appendix 3.

DISCUSSION

A map of the navigation quality rating of each line (Figure 7) shows that lines on the southern side of the Selenga Delta have the worst ("Poor") navigation whereas those around Academician Ridge have the best ("Excellent") navigation. The reason for this geographic distribution can be explained because the Selenga Delta survey was completed first, when the most communication problems and human error occured in logging.

In as much as the purpose of the cruise was to collect multichannel seismic data, a relevant issue is how the quality of the navigation data affects the multichannel data, specifically the multichannel geometry. The marine multichannel technique is based on repetition of regular geometries that allow sorting and reconstruction of common depth point seismic gathers for velocity analysis and stack (e.g., Yilmaz, 1987). Perturbations of this geometry, such as that which occurs when shots are not at the target 50-m spacing, introduce artifacts and complications in processing the data.

For the Baikal data, the shots were ideally 50-m apart to preserve the optimum geometry for recovering 24-fold data (Agena et al., 1994). The actual mean distance between shots ranged from 45 m (line 14) to 57 m (line 30). For all lines except line 30, the uncertainty (i.e., the scatter around the mean shot spacing) includes 50 m, and the assumption of 50-m firing intervals for processing the data is therefore within the estimated navigational uncertainty.

Because of the low frequencies used in the multichannel seismic survey (less than 60 Hz), velocity estimations will not be affected by using a geometry of 50-m firing intervals instead of the actual mean intervals of between 45 and 57 m. The region insonified on the lake floor by

22

Page 23: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

NO°E 56°N

DfiTfl QUflLITV

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150 ACADEMICIAN RIDGE

LAKE BAIKAL '92 MCS TRACKS

MERCATOR PROJECTION

Figure 7. Map showing the distribution of the navigation quality for the lines in Lake Baikal. The lines with the lowest "Poor" rating are generally in the region of the south Selenga Delta, where shot-time calibration logging was poorest at the beginning of the cruise.

23

Page 24: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

to

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Page 25: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

the seismic signal, i.e., the fresnel zone, at these frequencies is on the order of tens of meters. Shot intervals up to 7 m different than the ideal interval (i.e., 57-m shot intervals) would be inconsequential in velocity calculations.

A consequence of the navigational uncertainties is that some horizontal smearing of the data will occur, particlulary for lines where the mean firing rate differs from 50 m by more than 5 m. Figure 8 shows the fold coverage calculated using the Baikal multichannel source-receiver configuration (Agena et al., 1994) for 100 shots at 3 firing intervals: 45 m (top), 50 m (middle), and 55 m (bottom). In the ideal case (50 m), the fold coverage increases from 0 to 24 over common depth point (cdp) intervals of 12.5 m. For the 45-m case, the fold increases in a jerky pattern up to 6, and fluctuates between 4 and 6 for the bulk of the line with a cdp interval of 2.5 m. Similarly, the 55-m case only reaches maximum fold of 5 and fluctuates between 3 and 5, also with a cdp interval of 2.5 m. Merging 4 adjacent cdps from the 45-m and 55-m cases would produce 12.5-m binned cdps containing 24 traces, similar to the ideal 50-m case. The result is spatial smearing of the data horizontally. The low frequencies and size of the fresnel zone render most of this smearing inconsequential. However, the effect will be most pronounced in regions of steep relief, which are common in Lake Baikal along Academician Ridge and at the sides of the lake.

Another consequence of the navigational uncertainty is miscalculation of total line length and distances between cdps on the multichannel profiles. Figure 5 shows that the total line length for the line shot with 45-m intervals is 5645 m, whereas it is 6150 m and 6635 m for the 50-m and 55-m cases respectively. Distances measured off the seismic profiles should be corrected for the mean shot interval. Table 1 gives the best estimates of mean shot interval and line lengths for each line in Baikal.

The two missed shots associated with each tape change during the second half of the cruise require a small geometry correction in sorting and stacking the multichannel data. A comparison between a part of line 13 processed with and without the missed shots (Figure 9) shows that the character of the seismic data is essentially unchanged, but that certain details of the profile, for example, offset and overlap along a fault surface (arrow), differ. The fault trace that lines up with the arrow is sharper and more distinct on the profile with the corrections (Figure 9B). This emphasizes the importance of accurate navigation for processing of the multichannel data, particularly in structurally complex regions.

25

Page 26: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

to

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Page 27: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

CONCLUSIONS

The navigation data collected on the 1992 Lake Baikal multichannel seismic reflection cruise posed a challenge to processing because of difficulties in assigning times to shot points. The salient conclusions that have resulted from this study are:

(1) Three sources contributed to uncertainty in navigation: inherent measurement limitations, poor logging of the shot-time calibration points, and missing shots. The measurement error varies from 6 - 22 m. The error associated with shot-time logging ranges from about 2 m (whole second logging) to 70 m (whole minute logging). Error associated with the missing shots is greatest at the position of the missed shots and decreases toward the shot- time calibration points.

(2) The scatter associated with the raw GPS data varies between lines and can be very noisy (>10 m per each 10-s interval) or very quiet (<2 m per each 10-s interval). Most of the scatter in the raw navigation is a function of variations in HDOP value and reflects uncertainty introduced by changing satellite geometries used to compute successive locations.

(3) After careful editing and processing of the raw navigation and calibration files, the quality of each line was assigned a rating of:

Excellent: 28 lines 6-12 m uncertainty Good: 7 lines 12-24 m uncertainty Poor: 13 lines >50 m uncertainty

(4) The lines rated "Poor" generally occur in the southern Selenga Delta area. This is because the southern Selenga Delta was the first region profiled and includes the largest shot-time calibration errors.

(5) The assumption of a 50-m firing interval used to process the multichannel seismic data is valid and within the navigational uncertainty associated with shot locations. Actual deviations from 50 m are not likely to affect velocity estimates, but will cause some spatial smearing of the data, particularly in regions of steep relief. Distances measured off the seismic profiles should be corrected for actual shot distances of each line, rather than the assumed distance of 50 m.

27

Page 28: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

REFERENCES CITED

Agena, W.F., Lee, M.W., Miller, J.J., and Hutchinson, D.R., 1994, Lake Baikal - 1992 - Processing of Multichannel Seismic Reflection Data: U.S. Geological Survey Open-File Report OF-94-263, 44 pp.

Hum, J., 1989, GPS - A guide to the next utility: Trimble Navigation, Sunnyvale, California, p. 1-47.

Klitgord, K.D., Golmshtok, A. Ja, Scholz, C.A., Akentiev, L., Nichols, D., Schneider, C, McGill, J., Foster, D., and Unger, D., 1993, Seismic Survey of Lake Baikal, Siberia - Cruise Report: RV Balkhash 25 August to 25 September 1992: U.S. Geological Survey Open- File Report OF-93-201, 25 pp.

Milliken, R.J., and Zoller, C.J., 1980, Principle of operation of NAVSTAR (GPS) and system characteristics, in Janiczek, P.M., ed., Global Positioning System: The Institute of Navigation, Washington, D.C., p. 3-14.

Nichols, D.R., Miller, G., and Akentiev, L., 1992, Seismic survey of Lake Baikal, Siberia: Operational technical summary for the RV Balkhash and RV Titov 15 August to 30 September 1992: U.S. Geological Survey Open-File Report OF-92-693, 21 pp.

ten Brink, U.S., Badardinov, A., Miller, G.K., and Coleman, D.F., 1993, Ocean Bottom Seismometers operation during the seismic survey of Lake Baikal, Siberia, Autumn, 1992: U.S. Geological Survey Open-File Report OF-93-7, 24 pp.

Yilmaz, O., 1987, Seismic data processing: Society of Exploration Geophysicists, Investigations in Geophysics No. 2, 526 pp.

28

Page 29: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

APPENDIX 1:

PLOTS OF RAW GPS NAVIGATION

29

Page 30: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

DESCRIPTION OF PLOTS OF RAW NAVIGATION DATA

This appendix contains plots of raw navigation from all of the Lake Baikal 1992 multichannel lines, organized by increasing line number. All of the data are plotted against number of hours from the start of the line; because all lines are plotted at the same horizontal scale (7 hours), some lines are plotted on more than one page. The GMT start of each line is labelled for each line.

GPS - Distance Between FixesThe top plot shows the estimated distance between adjacent (10-second) navigation

locations calculated using geodetic inverse formula based on geodesy by A.R. Clarke. Ideally, these plots of distance between fixes should be a flat line (assuming a constant or near constant speed of the ship). Examples of nearly flat plots are line 1, hours 2-3, line 13, hours 9-11). Several reasons can explain spikes on these plots:

(1) data gaps in the 10-second positions will cause abnormally large estimates of distance between fixes; these can be identified by coincident spikes on the plots of time between fixes plotted beneath the distance plots (e.g., line 7, 3.75 hours after the start of the line).

(2) variations in the speed of the ship will cause distance estimates to vary. These kinds of variations should be relatively smooth and of fairly long wavelength (i.e., changes occur over periods of a few minutes and are constant until the next speed adjustment). Changes in the speed of the ship were very small and are not likely to be resolvable on lines where large spikes contaminate the data.

(3) uncertainty in the absolute GPS locations will cause short-wavelength spikes. Most of the spikes seen on the data are due to this uncertainty (e.g., line 1, 0-2 hours, 3-4 hours) and are directly related to the Horizontal Dilution Of Precision (HDOP) value shown in the third plot.

GPS - Time Between FixesThe second plot shows the actual time between 10-second positions; spikes on this plot

indicate data gaps. Generally, data gaps less than 1 minute (6 fixes) are considered negligible. The positions of data gaps of one minute or more are given in Table 3 of the main paper.

GPS - DOPsThe third plot show the Horizontal Dilution of Precision (HDOP) value, which refers to

the horizontal error associated with the geometry of the satellites used to compute a fix. Each change in HDOP value indicates a different satellite geometry or different set of satellites used to compute a location. These changes in HDOP generally coincide with large scatter in the estimates of "Distance between fixes" (top plot for each line).

GPS - AltitudeThe bottom plot for each line shows ellipsoidal altitude associated with each position.

For some lines, altitude was calculated automatically as part of the GPS solution; these lines, at the beginning of the cruise, show large altitude fluctuations (e.g., line 6). For most of the cruise, ellipsoidal altitude was set to 455 m, so that 3-satellite solutions could be used when 4-satellite

30

Page 31: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

solutions were not available. (Full GPS capability was not implemented in 1992, and therefore 3-satellite solutions were usually required for one or more time intervals each day). The ellipsoidal altitude is a mathematical surface defined as the sum of the geoid (in m) and the height above sea level (also in m):

Ellipsoidal altitude = Geoid + Height above Sea Level

Because the lake surface is essentially a constant height (455 m), and the geoid for the lake is also approximately constant (-24 m, C. Bowin, personal communication), the ellipsoidal altitude should have been specified as -24 + 455 =431 m. This difference (24 m) should not have affected the accuracy or quality of the resultant GPS location (B. Irwin, personal communication).

Statistics about time and distance between fixes, HDOP value, and ellipsoidal altitude are plotted at the end of each plot (mean, standard deviation, maximum and minimum values). Note that the standard deviations include the data gaps and may not be representative of the overall smoothness of the line (e.g., line 13). Line statistics are shown at the end of each line (i.e., on the final page for multiple page plots).

31

Page 32: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 33: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 34: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 35: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 101: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

APPENDIX 2

PLOTS OF SHOT-TIME CALIBRATION AND SHOT-DISTANCE INFORMATION

101

Page 102: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

DESCRIPTION OF SHOT-TIME CALIBRATION AND SHOT-DISTANCE PLOTS

This appendix gives four plots for each multichannel line from the 1992 Lake Baikal cruise. All plots utilize the same scales, except line 66/17A, which was shot with a different firing rate. Statistics (means and standard deviations) resulting from each step are plotted on each plot, together with a summary of the total shots per line (listed on the histogram plot). Some of the plots are continued on more than one page (lines 7, 11, 13, 15, 17, and 25).

Initial Shot-Time CalibrationThese plots show calculated firing rate versus shot point number. Shot-time calibration

was made at 15-minute intervals (about 35 shots) by logging shot number and a corresponding time. The firing rate was calculated by dividing the number of shots by the time. The locations of the calibration/control points are not labelled but can be extracted from most of the plots at the positions where the calculated firing rate changes, causing the boxy appearance of the plots. Initial shot time plots do not account for edits due to logging errors and missed shots. Logging of time to whole minutes is noted on the appropriate plots (Lines 1, 2, 3, 4, 6, 7, 8, 10, 16, 20, 22, 61/10A, 62/3A).

Final Shot-Time CalibrationThese plots are identical to initial shot-time calibration plots, except that edits for

incorrect logging and missed shots are included in the firing rate calculations. The positions of whole-minute logging are noted the same as for the initial shot-time calibration plots. Ideally, the plots of firing rate should be flat, because the airgun array was fired on even increments of time. Examples of reasonably flat final curves are lines 9, 11, 12, 13 (SP 1500 - 2500), 19, 25, 26, 32, 34, 52, 54, 56, 58, and 63. Examples of lines where editing provided major improvement in the calculated firing rate are lines 2, 11, 13, 19, 25, 34, 52, 54, 56, 58, and 66/17A. The boxiness of many of the "final" plots indicates poor final control on the firing rate (e.g., lines 4, 15, 17, 21, 42, 44, 46, 48, and 50).

Distance Between ShotsThese plots show the calculated distance between shots estimated after merging the raw

navigation with the final shot-time calibration files to produce an interpolated position and time for each shot point. Missing shots (i.e., pops) are included in this plot so that spikes that would otherwise be caused by missing shots do not show up. Pops are also included in the statistics (means and standard deviations).

Histogram of Distance Between ShotsThis plot shows the distribution of the scatter associated with the distance between shots.

The mean distance is plotted as a * on this plot. For lines that plot on multiple pages, the histogram plot is plotted only once, on the first page.

102

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Page 150: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 154: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

35In

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Page 156: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 157: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

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Page 158: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

APPENDIX 3

LINE CROSSING INFORMATION

158

Page 159: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

TABLE Al: LINE CROSSINGS

Line No.

2

2

3

3

4

4

4

4

6

6

6

6

6

6

7

7

7

7

7

7

7

7

7

7

7

7

7

7

7

7

7

Shot No.

199

462

166

345

96

271

539

540

80

231

280

814

822

946

45

147

321

453

639

763

901

995

1141

1200

1291

1337

1525

1552

1777

1899

2042

Line No.

3

7

2

4

7

26

3

62/3A

25

62/3A

26

28

7

L ll

24

22

20

18

16

14

12

25

61/10A

30

11

8

6

28

4

26

2

Shot No.

166

2042

199

539

1777

445

345

77

1329

238

189

161

1525

2137

40

378

17

354

39

367

89

154

897

108

1974

104

822

144

96

569

462

159

Page 160: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Line No.

8

8

8

8

8

8

9

10

11

11

11

11

11

11

11

11

11

11

11

11

11

11

11

11

12

12

12

13

13

13

13

Shot No.

80

104

256

611

818

929

127

607

170

388

546

745

905

1034

1209

1373

1535

1638

1826

1879

1882

1974

2008

2137

15

89

292

282

411

668

883

Line No.

11

7

28

25

62/3A

26

61/10A

25

34

32

52

24

22

20

18

16

14

12

25

61/10A

30

7

8

6

25

7

11

65/50B

48

46

44

Shot No.

2008

1337

291

947

363

8

1070

486

183

370

133

281

153

259

105

299

99

292

317

815

63

1291

80

946

13

901

1638

409

136

208

907

160

Page 161: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Line No.

13

13

13

13

14

14

15

15

15

15

15

15

15

15

15

16

16

17

17

17

17

17

17

17

17

17

17

18

18

19

19

Shot No.

1078

1234

1413

2541

99

367

41

43

235

447

708

1002

1307

1743

1938

39

299

313

496

550

702

971

1278

1568

1871

2076

2245

105

354

63

328

Line No.

42

63/40A

38

36

11

7

21

42

44

46

48

50

54

56

58

7

11

42

44

21

46

48

50

54

56

58

60

11

7

32

34

Shot No.

460

334

561

59

1535

763

635

800

520

679

654

354

476

581

565

639

1373

1240

101

135

1068

990

58

226

793

389

64

1209

453

33

399

161

Page 162: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Line No.

19

20

20

21

21

21

21

21

22

22

23

24

24

25

25

25

25

25

25

25

25

25

25

25

26

26

26

26

26

26

28

Shot No.

566

17

259

133

135

248

631

635

153

378

103

40

281

13

154

317

376

486

490

563

947

1171

1185

1329

8

124

137

189

445

569

144

Line No.

36

7

11

66/1 7 A

17

44

42

15

11

7

40

7

11

12

7

11

30

10

61/1 OA

28

8

62/3A

26

6

8

25

62/3A

6

4

7

7

Shot No.

225

321

1034

550

550

202

804

41

905

147

102

45

745

15

995

1826

18

607

657

408

611

289

124

80

929

1185

276

280

271

1899

1552

162

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Line No.

28

28

28

30

30

30

30

32

32

34

34

36

36

38

40

42

42

42

42

42

44

44

44

44

44

46

46

46

46

48

48

Shot No.

161

291

408

18

60

63

108

33

370

183

399

59

225

561

102

460

800

804

1240

1240

99

101

202

520

907

208

679

1068

1069

136

654

Line No.

6

8

25

25

61/10A

11

7

19

11

11

19

13

19

13

23

13

15

21

17

66/17 A

66/17A

17

21

15

13

13

15

17

66/1 7 A

13

15

Shot No.

814

256

563

376

811

1882

1200

63

388

170

328

2541

566

1413

103

1078

43

631

313

599

561

496

248

235

883

668

447

702

517

411

708

163

Page 164: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Line No.

48

48

50

50

50

52

54

54

54

56

56

56

58

58

58

60

60

61/10A

61/10A

61/10A

61/10A

61/10A

62/3A

62/3A

62/3A

62/3A

62/3A

63/40A

65/50B

66/1 7 A

66/17A

Shot No.

990

992

58

58

354

133

226

226

476

581

791

793

389

390

565

64

65

657

811

815

897

1070

77

238

276

289

363

334

409

207

242

Line No.

17

66/17A

17

66/1 7 A

15

11

17

66/1 7 A

15

15

66/1 7 A

17

17

66/17A

15

17

66/17A

25

30

11

7

9

4

6

26

25

8

13

13

60

58

Shot No.

971

460

1278

401

1002

546

1568

343

1307

1743

285

1871

2076

242

1938

2245

207

490

60

1879

1141

127

540

231

137

1171

818

1234

282

65

390

164

Page 165: NAVIGATION QUALITY FROM LAKE BAIKAL 1992 …

Line No.

66/1 7 A

66/17A

66/17A

66/17A

66/17A

66/17A

66/17A

66/17A

Shot No.

285

343

401

460

517

550

561

599

Line No.

56

54

50

48

46

21

44

42

Shot No.

791

226

58

992

1069

133

99

1240

165