Pub249Vol2 latitudes 0º-40º

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PUB. NO. 249

VOL. 2

SIGHT REDUCTION TABLES

FOR

AIR NAVIGATION

LATITUDES 0°−40°

DECLINATIONS 0°−29°



INTRODUCTION

FOREWORD

The Sight Reduction Tables for Air Navigation consist of three volumes of comprehensive tables of altitude and azi-

muth designed for the rapid reduction of astronomical sights in the air. This volume (Volume 2), for latitudes 0°–40°, and

Volume 3 for latitudes 39°–89°, provide for sights of the Sun, Moon, and planets; these tables are permanent. Volume 1

contains tables for selected stars for all latitudes, calculated for a specific epoch; it is intended for use for about 5 years,

when it will be replaced by a new edition based on a later epoch.

The National Imagery and Mapping Agency is responsible for the compilation of these tables. The Nautical Almanac

Office of the U.S. Naval Observatory and H. M. Nautical Almanac Office have cooperated in their design and preparation.

The tables are published in the United Kingdom as A.P. 3270, Sight Reduction Tables for Air Navigation.

The content and format of these three volumes may not be changed without the approval of Working Party 70 of the

Air Standardization Coordinating Committee.

In this 1992 reprint, the basic information and tabular data remain unchanged. Previous printings of this volume need

not be replaced by this reprint.

Users should refer corrections, additions, and comments for improving this product to:

MARINE NAVIGATION DEPARTMENT

ST D 44

NATIONAL IMAGERY AND MAPPING AGENCY

4600 SANGAMORE ROAD

BETHESDA MD 20816-5003



INTRODUCTION

DESCRIPTION OF THE TABLES

These tables, designated as Volume2 of the three-volume series of Pub.No. 249, Sight Reduction Tables forAir Nav-

igation, together with the similar Volume 3, supplement Volume 1 containing tabulations for selected stars. They togethercontain values of the altitude (to the nearest minute) and the azimuth angle (to the nearest degree) for integral degrees of

declination from 29° north to 29° south, for the complete range of latitude and for all hour angles at which the zenith dis-

tance is less than 95° (97° between latitudes 70° and the poles); provision is made for interpolation for declination. As in

Volume 1, no correction for refraction has been included in the tabulated altitudes; azimuth angle is given in contrast to the

azimuth for the selected stars. Volume 2 caters for latitudes 0°–40° and Volume 3 for latitudes 39°–89°; they are divided

purely for convenience in handling, and are otherwise similar in all respects.

The tables have been designed for use with the Air Almanac in the reduction of sights of the Sun, Moon and planets;they may also be used for stars with declinations less than 30° north or south. A list of the 57 navigational stars, with their

positions, is given on page (iii), as well as in the Air Almanac.

Their compact arrangement reflects the desire to include the maximum amount of data in the smallest practicable

space. The range of declination, and the extension to negative altitudes, explains the necessity for arranging the tables

across the length of the page.

ENTERING ARGUMENTS AND ARRANGEMENT

Latitude. Tabulations are given, in the two Volumes 2 and 3, for every whole degree of latitude from 0° to 89°; there

are four pages for latitude 0°, six pages for latitudes 1° to 47°, eight pages for latitudes 48° to 69°, four pages for latitudes

70° to 74° and six pages for latitudes 75° to 89°. Volume 2 covers latitudes 0° to 40° and Volume 3 latitudes 39° to 89°.

Declination. The full range of declination is divided into two groups of 15 values: 0° to 14° and 15° to 29°. One or

other of these groups is the horizontal argument on every page. Within the section (of 4, 6 or 8 pages) corresponding to

each degree of latitude, tabulations (of 2, 3 or 4 pages) for the first group of declinations, 0 ° to 14°, are given first; when

completed they are followed by precisely similar tabulations for the second group of declinations, 15° to 29°.

Local hour angle. The vertical argument on each page is the local hour angle of the body observed; it must be formed

in the usual way from the Air Almanac. The interval is 1° for latitudes 0° to 69°, but is increased to 2° for latitudes 70° to

89°. Within each sub-section of latitude and declination group, tabulations are first given for declination of the same name

as the latitude with LHA increasing on the left-hand side from 0° to 180°, or to some smaller limit depending on the alti-

tude; on the right-hand side the argument decreases from 360° to 180° (or some larger limit). Tabulations for declination

of the contrary name to the latitude follow after a break, and the order of LHA is reversed; the left-hand argument decreases

from 180°, or generally from some smaller limit, to 0°, while the right-hand argument increases from 180° (or some larger

limit) to 360°.

The tabulations for contrary name are seen to be arranged in the reverse way from those for same name; working

backwards (upwards instead of downwards) from the end of the sub-section, they appear precisely as those for the same

name when working forwards in the normal way.

Values of LHA between 0° and 180° are always found on the left; values between 180° and 360° are always found



INTRODUCTION

USE OF THE TABLES

The GHA and declination of the observed body are taken in the usual way from the Air Almanac for the actual time(GMT) of observation. The GHA is combined with an assumed longitude, close to the DR longitude, to make the LHA a

whole degree, or an even degree for latitudes above 69°. The tables are first entered with the whole degree of latitude, near-

est to the DR latitude, and the appropriate declination group; in this sub-section, they are then entered with the degree of

declination numerically less than that of the body observed, and with the value of LHA found above, taking particular care

to choose the portion of the table corresponding to the same or contrary name, as appropriate.

The tables give directly the tabulated altitude, Hc, the difference, d , and the azimuth angle, Z, for the whole degree

of declination chosen. The altitude must be interpolated to the true declination by means of Table 5, on page 248 or the

bookmark, applying to it the correct proportion of d , with the sign given (added if +, subtracted if −); the azimuth angle, Z,

must be converted to azimuth, Zn, by the rules given on each page, but, in general, need not be interpolated for declination.

For zenith distances greater than 90°, negative altitudes are tabulated; the correction from Table 5 must thus be applied

algebraically. In all cases it is recommended that values in neighboring columns be inspected to see whether the altitude

increases or decreases with declination.

The intercept is found in the usual way by comparing the corrected sextant altitude (Ho) with the tabulated altitude,

interpolated to the actual declination as above:

towards the body if the observed altitude is greater than the tabulated altitude;

away from the body if the observed altitude is less than the tabulated altitude.

The sextant reading must be corrected for instrument error, dome refraction (if applicable), refraction (from Table 6)

and parallax (for the Moon), before being compared with the tabulated altitude. The sight is plotted from the assumed po-

sition, defined by the whole degree of latitude and the assumed longitude. This assumed position may previously be ad-

justed for the effect of Coriolis acceleration (see Table 7) and advanced or retarded to another time; alternatively these cor-

rections may be made to the position line or, in the case of the corrections from Table7, to the fix. The application of these

corrections is considered separately below.

Example. On 1978 January 1, in DR position S 23° 42′, E 113° 25′, at height 37,000 ft., an observation of the Moon

is obtained with a bubble sextant at GMT 00h 53m 45s; the sextant reading is 31° 29′ and the correction for instrument error

and dome refraction is −5′.

From the Air Almanac, GMT GHA Dec. ° ′

h m s ° ′ ° ′ Sextant altitude 31 29

AM page for Jan. 1, Moon at 00 50 00 300 08 N 1 29 Instrument error, etc. −5flap, Moon, increment for 3 45 0 54 Parallax in altitude (P. in A.) +48

Refraction (Table 6) 0

Sum = GHA Moon at 00 53 45 301 02

Assumed longitude, added because east + 112 58 Corrected sextant altitude (Ho) 32 12

Sum = LHA Moon (less 360° if necessary) 54



INTRODUCTION

From these tables (pages 146), for Lat. 24°, Dec. 1° (Contrary), LHA 54°

The sign of the d -correction is the same as that of d , and a glance at the entries for the neighboring declination column

(2°) verifies that the altitude decreases with increasing declination.

The assumed latitude is S 24°, the assumed longitude is E 112° 58′, and the intercept of 26′ is plotted from this position

in the true bearing of 288°. The position line is drawn perpendicular to this direction.

A useful feature of these tables is the provision for low and even negative altitudes; this enables sights of the Sun, or

other bodies, to be reduced when actually below the horizon as seen from sea level. Refraction at such low altitudes is large

and variations from the standard values are too great to be ignored; provision is thus made in Table 6 for the application

of a temperature correction in such cases.

Example. On 1978 January 1, in DR position S 16° 47′, W 32° 19′, at height 32,000 ft., an observation of the Sun is

obtained at GMT 20h 57m 43s, the Sun being just above the visible horizon; the sextant reading is −2° 15′, the correction

for instrument error and dome refraction is −8′, and the external temperature is −70°C.

From these tables (pages 106), for Lat. 17°, Dec. 22° (Same), LHA 101°

Refraction is obtained from Table 6. The column headed 30,000 ft. (nearest to 32,000 ft.) is first chosen; in that

column the sextant altitude corrected for instrument error, etc., (−2° 23′) is seen to lie in the interval corresponding to

R0 = 45′. However, the temperature is here lower than normal for the height and the lower portion of the table indicates

that the correcting factor f , corresponding to a temperature of −70°C. at height 30,000 ft. is 1.1. The table on the right

immediately gives the refraction R as 50′.

When the altitude is very small or negative, special care must be exercised in applying the d -correction to the altitude

° ′ ′ ° ° ′

Tabulated Hc, d , and Z,d -correction (Table 5) for 29′

Hc 32 00 d −30 Z 108 Corrected sextant altitude (Ho) 32 12−14 Corrected tabulated altitude (Hc) 31 46

Corrected tabulated altitude (Hc) 31 46 Zn 288 Intercept 26 towards

From the Air Almanac, GMT GHA Dec.

h m s ° ′ ° ′ ° ′

PM page for Jan. 1, Sun atflap, Sun, increment for

20 50 00 131 35 S 22 59 Sextant altitude −2 15

7 43 1 56 Instrument error, etc. −8

Sum = GHA Sun at 20 57 43 133 31 Refraction (Table 6) −50

Assumed longitude, subtracted because west −32 31 Corrected sextant altitude (Ho) −3 13

Sum = LHA Sun (less 360° if necessary) 101

° ′ ′ ° ° ′

Tabulated Hc, d , and Z,

d -correction (Table 5) for 59′

Hc −3 25 d +20 Z 66 Corrected tabulated altitude (Ho) −3 05

+20 Intercept

plotted from assumed position:

latitude S 17°, longitude W 32° 31′

8 away

Corrected tabulated altitude (Hc) −3 05 Zn 246



INTRODUCTION

USE OF CORRECTING TABLES

As indicated above, corrections are required for the following, in addition to parallax (for the Moon) and refraction:

Coriolis acceleration. This correction, given in Table 7 on the inside back cover, may be applied either to each indi-

vidual observation or to the fix deduced from several observations. When applied to individual observations, either the po-

sition line or the assumed position from which it is constructed must be shifted by the distance Z miles perpendicular to the

track. The rule for applying this correction is given at the foot of Table 7.

Motion of the observer (MOO). If it is desired to get a fix from two or more observations, the resulting position lines

must be reduced to a common time, usually the time of one of them. This may be done in two ways: the position lines of

observations made earlier or later than this time may be transferred on the plotting chart by the motion of the aircraft in thetime-interval concerned, or the corrected sextant altitudes (or intercepts) may be adjusted to allow for the motion of the

aircraft.

In the first case, the shift may be applied to the position line or to the assumed position from which it is constructed.

In the second case, the adjustment to corrected sextant altitude may be taken from Table 1 on the inside front cover,

interpolating where necessary. Table 1 gives, in the upper part, the correction for a time-interval of 4 minutes, while the

lower part enables this to be extended to any time-interval. By reversing the sign of this correction, it may be applied to the

tabulated altitude instead of to the correctedsextant altitude, or it maybe applied directly to the intercept by the rules given.

Usually, sights of several stars will be taken in rapid succession to give a fix. The example below illustrates the use

of the tables for the reduction of a typical set of observations.

Example. On 1978 January 1, the following observations are obtained when flying at 385 knots on track 117°T. The

observations chosen are for illustration only and are not the most suitable for a fix.

The DR position at GMT 02h 30m is S 9° 42′, E 7° 28′, height 24,000 ft., temperature −47°C.

Body GMT Sextant altitude Instrument error, etc.h m s ° ′ ′

Moon 02 26 55 58 34 −6

Jupiter 02 30 55 26 25 −9

Adhara 02 35 17 45 55 −7

From the Air Almanac, GMTMoonGHA Dec. GMT

JupiterGHA Dec. GMT

Adhara(No.19)GHA Dec.

h m s ° ′ ° ′ h m s ° ′ ° ′ h m s ° ′ ° ′

AM page for Jan. 1 02 20 00 321 57 N 1 14 02 30 00 48 03 N 23 12 02 30 00 137 54flap, increment for 6 55 1 40 0 55 0 14 5 17 1 19

flap, SHA and Dec. of star — — — — — 255 33 S 28 57

Sum = GHA at 02 26 55 323 37 02 30 55 48 17 02 35 17 394 46

Assumed longitude, added because east +7 23 +7 43 +7 14

Sum = LHA (less 360° if necessary) 331 56 42



INTRODUCTION

From these tables (pages 62, 65, 63, respectively), with assumed latitude 10°

In this example, the assumed positions for all observations are taken as close as possible to the DR position at 02

h

30

m

;shorter intercepts can be obtained by relating the assumed positions to the DR position at the time of observation. The in-

tercepts are plotted from the assumed positions, latitude S 10°, respective longitudes E 7° 23′, E 7° 43′, and E 7° 14′, trans-

ferred on the chart for the motion of the aircraft between the time of observation and that of the fix, and for the effect of

Coriolis acceleration.

The corrections for motionof the aircraft may, however, be applied directly to the observed altitude or to the intercept.

Using Table 1 corrections are obtained as follows to the observations of the Moon and Adhara, so that the fix will be ob-

tained at the time of the Jupiter observation (02h 30m 55s).

The above table is largely self-explanatory; the value for the time-interval of 4m22s is found from the lower part of

Table 1 by doubling that for 2m11s.

The adjusted intercepts are plotted from the same assumed positions, latitude S 10°, respective longitudes E 7° 23′,E 7° 43′, and E 7° 14′. The correction for the effect of Coriolis acceleration is applied directly to the fix. From Table 7

(inside back cover) the Z correction is found to be 2′ and the fix (or the assumed positions or position lines) must be shifted

to a distance 2 miles to the left of track (southern hemisphere), i.e., in direction 027°.

Motion of the body (MOB). If the time of observation differs from that used to obtain the tabular value of LHA, the

entry may still be used if a correction for the motion of the body (due to the rotation of the Earth) in the time interval is

applied to the altitude (or intercept). Table 2, on page (i), provides for this correction. It enables observations made at dif-

ferent times to be reduced and plotted as if they were made simultaneously, and it thus facilitates precomputation from the

Air Almanac. Since the time used for reduction is normally the time at which the fix is desired, it is convenient to combine

the corrections for motion of the body with those for the motion of the observer, as the time intervals are the same.

When both corrections are used in this way, the quantities taken from the upper parts of Tables 1 and 2 should be

summed and the sum used to enter the lower parts of the tables. Alternative Tables 1 and 2, altitude corrections for change

in position respectively of the observer and body, for 1 minute of time, are included in this volume as an additional book-

mark.

h m

Dec. 1° (Contrary) Dec. 23° (Contrary) Dec. 28° (Same)

Hc d Z Hc d Z Hc d Z

Tabulated Hc, d , and Z

for

° ′ ′ ° ° ′ ′ ° ° ′ ′ °

LHA 331° 59 07 −23 109 LHA 56° 26 03 −26 122 LHA 42° 46 42 −17 60

d -correction (Table 5) for 14′ −5 12′ −5 57′ −16

Corrected tabulated altitude (Hc) 59 02 25 58 46 26

Corrected tabulated altitude (Ho) 58 57 26 15 45 48

Intercept 5 away Zn 071° 17 towards Zn 302° 38 away Zn 240°

Body AzimuthTrueTrack

RelativeAzimuth Table 1

TimeInterval

Correction from lowerPart of Table 1 to

Sext. Alt. Intercept

AdjustedCorr.

Sext. Alt.AdjustedIntercept

° ° ° ′ m s ′ ′ ° ′ ′

Moon 071 117 314 +18 +4 00 +28 18 towards 59 15 13 towards

Adhara 240 117 123 −14 −4 22 +15 15 towards 46 03 23 away



INTRODUCTION

From these tables (pages 62, 65, 63, respectively), with assumed latitude 10°

The adjustments to these intercepts, for motion of observer and motion of body, are found as follows:

SPECIAL TECHNIQUES

The arrangement of the tabulations in this volume, unlike that of Volume 1, does not lend itself to any particular tech-

nique of observation and reduction. Some special techniques may, however, still be used; the principles upon which they

are based are given below and users will doubtless develop methods to suit their own requirements.

1. By making the observations at predetermined times (“scheduled shooting”), the tabulated altitudes and azimuths

can be extracted beforehand and the same values used both for presetting the sextant and for the subsequent reduction of

the sights.

2. All corrections, normally applied to the sextant altitude, may be applied to the tabulated altitude (with reversed

signs), or to the assumed position, before an observation is made, thus enabling the position line to be drawn very quickly

after the observation. Care must be taken with refraction for low altitudes; the value from Table 6 may differ considerably

according to whether the sextant or tabulated altitude is used as argument.

Moon Jupiter Adhara (no. 19)

From the Air Almanac, GMT GHA Dec. GHA Dec. GHA Dec.

h m ° ′ ° ′ ° ′ ° ′ ° ′ ° ′

AM page for January 1 02 30 324 22 N 1 12 48 03 N 23 12 137 54

flap, SHA and Dec. of star — — — — — 255 33 S 28 57

Sum = GHA at 02 30 324 22 48 03 393 27

Assumed longitude, added because east +7 38 +7 57 +7 33

Sum = LHA (less 360° if necessary) 332 56 41

Dec. 1° (Contrary) Dec. 23° (Contrary) Dec. 28° (Same)Hc d Z Hc d Z Hc d Z

Tabulated Hc, d , and Z,

for

° ′ ′ ° ° ′ ′ ° ° ′ ′ °

LHA 332° 60 02 −23 110 LHA 56° 26 03 −26 122 LHA 41° 47 33 −18 59

d -correction (Table 5) for 12′ −5 12′ −5 57′ −17

Corrected tabulated altitude (Hc) 59 57 25 58 47 16

Corrected sextant altitude (Ho) 58 57 26 15 45 48

Intercept 1 00 away Zn 070° 17 towards Zn 302° 1 28 away Zn 239°

Body Azimuth

True

Track

Relative

Azimuth

Table

1

Table

2 Sum

Time

Interval

Corrections

to Intercept

Adjusted

Intercept

° ° ° ′ ′ ′ m s ′ ′

Moon 070 117 313 +17 +56 +73 +3 05 57 towards 3 away

Jupiter 302 117 185 −26 −50 −76 −0 55 18 towards 35 towards

Alpheratz 239 117 122 −13 −50 −63 −5 17 83 towards 5 away



TABLE 1.—Altitude Correction for Change in Position of Observer

Correction for 4 Minutes of Time

Rel.

Zn

Ground Speed in Knots Rel.

Zn50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800 850 900

° ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ °

000 +3 +7 +10 +13 +17 +20 +23 +27 +30 +33 +37 +40 +43 +47 +50 +53 +57 +60 000005 3 7 10 13 17 20 23 27 30 33 37 40 43 46 50 53 56 60 355010 3 7 10 13 16 20 23 26 30 33 36 39 43 46 49 53 56 59 350015 3 6 10 13 16 19 23 26 29 32 35 39 42 45 48 52 55 58 345020 3 6 9 13 16 19 22 25 28 31 34 38 41 44 47 50 53 56 340025 3 6 9 12 15 18 21 24 27 30 33 36 39 42 45 48 51 54 335

030 +3 +6 +9 +12 +14 +17 +20 +23 +26 +29 +32 +35 +38 +40 +43 +46 +49 +52 330035 3 5 8 11 14 16 19 22 25 27 30 33 35 38 41 44 46 49 325040 3 5 8 10 13 15 18 20 23 26 28 31 33 36 38 41 43 46 320045 2 5 7 9 12 14 16 19 21 24 26 28 31 33 35 38 40 42 315050 2 4 6 9 11 13 15 17 19 21 24 26 28 30 32 34 36 39 310055 2 4 6 8 10 11 13 15 17 19 21 23 25 27 29 31 33 34 305

060 +2 +3 +5 +7 +8 +10 +12 +13 +15 +17 +18 +20 +22 +23 +25 +27 +28 +30 300

065 1 3 4 6 7 8 10 11 13 14 15 17 18 20 21 23 24 25 295070 1 2 3 5 6 7 8 9 10 11 13 14 15 16 17 18 19 21 290075 1 2 3 3 4 5 6 7 8 9 9 10 11 12 13 14 15 16 285080 1 1 2 2 3 3 4 5 5 6 6 7 8 8 9 9 10 10 280085 +0 +1 +1 +1 +1 +2 +2 +2 +3 +3 +3 +3 +4 +4 +4 +5 +5 +5 275

090 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 270

095 -0 -1 -1 -1 -1 -2 -2 -2 -3 -3 -3 -3 -4 -4 -4 -5 -5 -5 265100 1 1 2 2 3 3 4 5 5 6 6 7 8 8 9 9 10 10 260105 1 2 3 3 4 5 6 7 8 9 9 10 11 12 13 14 15 16 255110 1 2 3 5 6 7 8 9 10 11 13 14 15 16 17 18 19 21 250115 1 3 4 6 7 8 10 11 13 14 15 17 18 20 21 23 24 25 245120 2 3 5 7 8 10 12 13 15 17 18 20 22 23 25 27 28 30 240

125 -2 -4 -6 -8 -10 -11 -13 -15 -17 -19 -21 -23 -25 -27 -29 -31 -33 -34 235130 2 4 6 9 11 13 15 17 19 21 24 26 28 30 32 34 36 39 230135 2 5 7 9 12 14 16 19 21 24 26 28 31 33 35 38 40 42 225140 3 5 8 10 13 15 18 20 23 26 28 31 33 36 38 41 43 46 220145 3 5 8 11 14 16 19 22 25 27 30 33 35 38 41 44 46 49 215150 3 6 9 12 14 17 20 23 26 29 32 35 38 40 43 46 49 52 210

155 -3 -6 -9 -12 -15 -18 -21 -24 -27 -30 -33 -36 -39 -42 -45 -48 -51 -54 205160 3 6 9 13 16 19 22 25 28 31 34 38 41 44 47 50 53 56 200165 3 6 10 13 16 19 23 26 29 32 35 39 42 45 48 52 55 58 195170 3 7 10 13 16 20 23 26 30 33 36 39 43 46 49 53 56 59 190175 3 7 10 13 17 20 23 27 30 33 37 40 43 46 50 53 56 60 185180 -3 -7 -10 -13 -17 -20 -23 -27 -30 -33 -37 -40 -43 -47 -50 -53 -57 -60 180

Interpolation for Altitude Correction for Less Than 4 Minutes of TimeInterval

ofTime

Value from Tables 1 and 2 (For values greater than 60′ see opposite page) Intervalof

Time3 6 9 12 15 18 21 24 27 30 33 36 39 42 45 48 51 54 57 60

m s ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ m s0 00 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 00

10 0 0 0 1 1 1 1 1 1 1 1 2 2 2 2 2 2 2 2 3 1020 0 1 1 1 1 2 2 2 2 3 3 3 3 4 4 4 4 5 5 5 2030 0 1 1 2 2 2 3 3 3 4 4 5 5 5 6 6 6 7 7 8 3040 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 8 9 9 10 10 40

0 50 1 1 2 3 3 4 4 5 6 6 7 8 8 9 9 10 11 11 12 13 0 50

1 00 1 2 2 3 4 5 5 6 7 8 8 9 10 11 11 12 13 14 14 15 1 00

10 1 2 3 4 4 5 6 7 8 9 10 11 11 12 13 14 15 16 17 18 1020 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 2030 1 2 3 5 6 7 8 9 10 11 12 14 15 16 17 18 19 20 21 23 3040 1 3 4 5 6 8 9 10 11 13 14 15 16 18 19 20 21 23 24 25 40

1 50 1 3 4 6 7 8 10 11 12 14 15 17 18 19 21 22 23 25 26 28 1 50

2 00 2 3 5 6 8 9 11 12 14 15 17 18 20 21 23 24 26 27 29 30 2 0010 2 3 5 7 8 10 11 13 15 16 18 20 21 23 24 26 28 29 31 33 1020 2 4 5 7 9 11 12 14 16 18 19 21 23 25 26 28 30 32 33 35 2030 2 4 6 8 9 11 13 15 17 19 21 23 24 26 28 30 32 34 36 38 3040 2 4 6 8 10 12 14 16 18 20 22 24 26 28 30 32 34 36 38 40 40



TABLE 2.—Altitude Correction for Change in Position of Body

Correction for 4 Minutes of Time

True

Zn

Latitude in Degrees True

Zn0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85

° ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ °090 +60 +60 +59 +58 +56 +54 +52 +49 +46 +42 +39 +34 +30 +25 +21 +16 +10 +5 090095 60 60 59 58 56 54 52 49 46 42 38 34 30 25 20 15 10 5 085

100 59 59 58 57 56 54 51 48 45 42 38 34 30 25 20 15 10 5 080105 58 58 57 56 54 53 50 47 44 41 37 33 29 24 20 15 10 5 075110 56 56 56 54 53 51 49 46 43 40 36 32 28 24 19 15 10 5 070115 54 54 54 53 51 49 47 45 42 38 35 31 27 23 19 14 9 5 065

120 +52 +52 +51 +50 +49 +47 +45 +43 +40 +37 +33 +30 +26 +22 +18 +13 +9 +5 060125 49 49 48 47 46 45 43 40 38 35 32 28 25 21 17 13 9 4 055130 46 46 45 44 43 42 40 38 35 33 30 26 23 19 16 12 8 4 050

135 42 42 42 41 40 38 37 35 33 30 27 24 21 18 15 11 7 4 045140 39 38 38 37 36 35 33 32 30 27 25 22 19 16 13 10 7 3 040145 34 34 34 33 32 31 30 28 26 24 22 20 17 15 12 9 6 3 035

150 +30 +30 +30 +29 +28 +27 +26 +25 +23 +21 +19 +17 +15 +13 +10 +8 +5 +3 030155 25 25 25 24 24 23 22 21 19 18 16 15 13 11 9 7 4 2 025160 21 20 20 20 19 19 18 17 16 15 13 12 10 9 7 5 4 2 020165 16 15 15 15 15 14 13 13 12 11 10 9 8 7 5 4 3 1 015170 10 10 10 10 10 9 9 9 8 7 7 6 5 4 4 3 2 1 010175 +5 +5 +5 +5 +5 +5 +5 +4 +4 +4 +3 +3 +3 +2 +2 +1 +1 +0 005

180 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 180

185 -5 -5 -5 -5 -5 -5 -5 -4 -4 -4 -3 -3 -3 -2 -2 -1 -1 -0 355190 10 10 10 10 10 9 9 9 8 7 7 6 5 4 4 3 2 1 350195 16 15 15 15 15 14 13 13 12 11 10 9 8 7 5 4 3 1 345200 21 20 20 20 19 19 18 17 16 15 13 12 10 9 7 5 4 2 340

205 25 25 25 24 24 23 22 21 19 18 16 15 13 11 9 7 4 2 335210 30 30 30 29 28 27 26 25 23 21 19 17 15 13 10 8 5 3 330

215 -34 -34 -34 -33 -32 -31 -30 -28 -26 -24 -22 -20 -17 -15 -12 -9 -6 -3 325220 39 38 38 37 36 35 33 32 30 27 25 22 19 16 13 10 7 3 320225 42 42 42 41 40 38 37 35 33 30 27 24 21 18 15 11 7 4 315230 46 46 45 44 43 42 40 38 35 33 30 26 23 19 16 12 8 4 310235 49 49 48 47 46 45 43 40 38 35 32 28 25 21 17 13 9 4 305240 52 52 51 50 49 47 45 43 40 37 33 30 26 22 18 13 9 5 300

245 -54 -54 -54 -53 -51 -49 -47 -45 -42 -38 -35 -31 -27 -23 -19 -14 -9 -5 295250 56 56 56 54 53 51 49 46 43 40 36 32 28 24 19 15 10 5 290255 58 58 57 56 54 53 50 47 44 41 37 33 29 24 20 15 10 5 285260 59 59 58 57 56 54 51 48 45 42 38 34 30 25 20 15 10 5 280265 60 60 59 58 56 54 52 49 46 42 38 34 30 25 20 15 10 5 275270 -60 -60 -59 -58 -56 -54 -52 -49 -46 -42 -39 -34 -30 -25 -21 -16 -10 -5 270

Interpolation for Altitude Correction for Less Than 4 Minutes of Time

Intervalof

Time

Value from Tables 1 and 2 (For values less than 60 ′ see opposite page) Intervalof

Time63 66 69 72 75 78 81 84 87 90 93 96 99 102 105 108 111 114 117 120

m s ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ m s0 00 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 00

10 3 3 3 3 3 3 3 4 4 4 4 4 4 4 4 5 5 5 5 5 1020 5 6 6 6 6 7 7 7 7 8 8 8 8 9 9 9 9 10 10 10 2030 8 8 9 9 9 10 10 11 11 11 12 12 12 13 13 14 14 14 15 15 3040 11 11 12 12 13 13 14 14 15 15 16 16 17 17 18 18 19 19 20 20 40

0 50 13 14 14 15 16 16 17 18 18 19 19 20 21 21 22 23 23 24 24 25 0 50

1 00 16 17 17 18 19 20 20 21 22 23 23 24 25 26 26 27 28 29 29 30 1 0010 18 19 20 21 22 23 24 25 25 26 27 28 29 30 31 32 32 33 34 35 1020 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 20

30 24 25 26 27 28 29 30 32 33 34 35 36 37 38 39 41 42 43 44 45 3040 26 28 29 30 31 33 34 35 36 38 39 40 41 43 44 45 46 48 49 50 40

1 50 29 30 32 33 34 36 37 39 40 41 43 44 45 47 48 50 51 52 54 55 1 50

2 00 32 33 35 36 38 39 41 42 44 45 47 48 50 51 53 54 56 57 59 60 2 0010 34 36 37 39 41 42 44 46 47 49 50 52 54 55 57 59 60 62 63 65 1020 37 39 40 42 44 46 47 49 51 53 54 56 58 60 61 63 65 67 68 70 2030 39 41 43 45 47 49 51 53 54 56 58 60 62 64 66 68 69 71 73 75 3040 42 44 46 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76 78 80 40

2 50 45 47 49 51 53 55 57 60 62 64 66 68 70 72 74 77 79 81 83 85 2 50



TABLE 3.—Conversion of Arc to Time

° h m ° h m ° h m ° h m ° h m ° h m ′ m s ″ s

0 0 00 60 4 00 120 8 00 180 12 00 240 16 00 300 20 00 0 0 00 0 0.00

1 0 04 61 4 04 121 8 04 181 12 04 241 16 04 301 20 04 1 0 04 1 0.072 0 08 62 4 08 122 8 08 182 12 08 242 16 08 302 20 08 2 0 08 2 0.133 0 12 63 4 12 123 8 12 183 12 12 243 16 12 303 20 12 3 0 12 3 0.204 0 16 64 4 16 124 8 16 184 12 16 244 16 16 304 20 16 4 0 16 4 0.27

5 0 20 65 4 20 125 8 20 185 12 20 245 16 20 305 20 20 5 0 20 5 0.336 0 24 66 4 24 126 8 24 186 12 24 246 16 24 306 20 24 6 0 24 6 0.407 0 28 67 4 28 127 8 28 187 12 28 247 16 28 307 20 28 7 0 28 7 0.478 0 32 68 4 32 128 8 32 188 12 32 248 16 32 308 20 32 8 0 32 8 0.539 0 36 69 4 36 129 8 36 189 12 36 249 16 36 309 20 36 9 0 36 9 0.60

10 0 40 70 4 40 130 8 40 190 12 40 250 16 40 310 20 40 10 0 40 10 0.6711 0 44 71 4 44 131 8 44 191 12 44 251 16 44 311 20 44 11 0 44 11 0.7312 0 48 72 4 48 132 8 48 192 12 48 252 16 48 312 20 48 12 0 48 12 0.8013 0 52 73 4 52 133 8 52 193 12 52 253 16 52 313 20 52 13 0 52 13 0.87

14 0 56 74 4 56 134 8 56 194 12 56 254 16 56 314 20 56 14 0 56 14 0.93

15 1 00 75 5 0 135 9 00 195 13 0 255 17 00 315 21 00 15 1 00 15 1.0016 1 04 76 5 4 136 9 04 196 13 4 256 17 04 316 21 04 16 1 04 16 1.0717 1 08 77 5 8 137 9 08 197 13 8 257 17 08 317 21 08 17 1 08 17 1.1318 1 12 78 5 12 138 9 12 198 13 12 258 17 12 318 21 12 18 1 12 18 1.2019 1 16 79 5 16 139 9 16 199 13 16 259 17 16 319 21 16 19 1 16 19 1.27

20 1 20 80 5 20 140 9 20 200 13 20 260 17 20 320 21 20 20 1 20 20 1.3321 1 24 81 5 24 141 9 24 201 13 24 261 17 24 321 21 24 21 1 24 21 1.4022 1 28 82 5 28 142 9 28 202 13 28 262 17 28 322 21 28 22 1 28 22 1.4723 1 32 83 5 32 143 9 32 203 13 32 263 17 32 323 21 32 23 1 32 23 1.5324 1 36 84 5 36 144 9 36 204 13 36 264 17 36 324 21 36 24 1 36 24 1.60

25 1 40 85 5 40 145 9 40 205 13 40 265 17 40 325 21 40 25 1 40 25 1.67

26 1 44 86 5 44 146 9 44 206 13 44 266 17 44 326 21 44 26 1 44 26 1.7327 1 48 87 5 48 147 9 48 207 13 48 267 17 48 327 21 48 27 1 48 27 1.8028 1 52 88 5 52 148 9 52 208 13 52 268 17 52 328 21 52 28 1 52 28 1.8729 1 56 89 5 56 149 9 56 209 13 56 269 17 56 329 21 56 29 1 56 29 1.93

30 2 00 90 6 0 150 10 00 210 14 0 270 18 00 330 22 00 30 2 00 30 2.0031 2 04 91 6 4 151 10 04 211 14 4 271 18 04 331 22 04 31 2 04 31 2.0732 2 08 92 6 8 152 10 08 212 14 8 272 18 08 332 22 08 32 2 08 32 2.1333 2 12 93 6 12 153 10 12 213 14 12 273 18 12 333 22 12 33 2 12 33 2.2034 2 16 94 6 16 154 10 16 214 14 16 274 18 16 334 22 16 34 2 16 34 2.27

35 2 20 95 6 20 155 10 20 215 14 20 275 18 20 335 22 20 35 2 20 35 2.3336 2 24 96 6 24 156 10 24 216 14 24 276 18 24 336 22 24 36 2 24 36 2.4037 2 28 97 6 28 157 10 28 217 14 28 277 18 28 337 22 28 37 2 28 37 2.4738 2 32 98 6 32 158 10 32 218 14 32 278 18 32 338 22 32 38 2 32 38 2.5339 2 36 99 6 36 159 10 36 219 14 36 279 18 36 339 22 36 39 2 36 39 2.60

40 2 40 100 6 40 160 10 40 220 14 40 280 18 40 340 22 40 40 2 40 40 2.6741 2 44 101 6 44 161 10 44 221 14 44 281 18 44 341 22 44 41 2 44 41 2.7342 2 48 102 6 48 162 10 48 222 14 48 282 18 48 342 22 48 42 2 48 42 2.8043 2 52 103 6 52 163 10 52 223 14 52 283 18 52 343 22 52 43 2 52 43 2.8744 2 56 104 6 56 164 10 56 224 14 56 284 18 56 344 22 56 44 2 56 44 2.93

45 3 00 105 7 0 165 11 00 225 15 0 285 19 00 345 23 00 45 3 00 45 3.0046 3 04 106 7 4 166 11 04 226 15 4 286 19 04 346 23 04 46 3 04 46 3.0747 3 08 107 7 8 167 11 08 227 15 8 287 19 08 347 23 08 47 3 08 47 3.1348 3 12 108 7 12 168 11 12 228 15 12 288 19 12 348 23 12 48 3 12 48 3.2049 3 16 109 7 16 169 11 16 229 15 16 289 19 16 349 23 16 49 3 16 49 3.27

50 3 20 110 7 20 170 11 20 230 15 20 290 19 20 350 23 20 50 3 20 50 3.3351 3 24 111 7 24 171 11 24 231 15 24 291 19 24 351 23 24 51 3 24 51 3.4052 3 28 112 7 28 172 11 28 232 15 28 292 19 28 352 23 28 52 3 28 52 3.4753 3 32 113 7 32 173 11 32 233 15 32 293 19 32 353 23 32 53 3 32 53 3.5354 3 36 114 7 36 174 11 36 234 15 36 294 19 36 354 23 36 54 3 36 54 3.60

55 3 40 115 7 40 175 11 40 235 15 40 295 19 40 355 23 40 55 3 40 55 3.6756 3 44 116 7 44 176 11 44 236 15 44 296 19 44 356 23 44 56 3 44 56 3.7357 3 48 117 7 48 177 11 48 237 15 48 297 19 48 357 23 48 57 3 48 57 3.8058 3 52 118 7 52 178 11 52 238 15 52 298 19 52 358 23 52 58 3 52 58 3.8759 3 56 119 7 56 179 11 56 239 15 56 299 19 56 359 23 56 59 3 56 59 3.93









M O O



ALTERNATIVE TABLE 1—Altitude Correction for Change in Position of Observer M. O. O.

Correction for 1 Minute of Time

Rel.Zn

Ground Speed in KnotsRel.Zn

50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800 850 900

° ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ °

T o f a c i l i t a t e u

s e o f P u b .

N o .

2 4 9 ,

V o l u m e 1 ,

2 , a n d 3 .

000 +0.8 +1.7 +2.5 +3.3 +4.2 +5.0 +5.8 +6.7 +7.5 +8.3 +9.2 +10.0 +10.8 +11.7 +12.5 +13.3 +14.2 +15.0 000002 0.8 1.7 2.5 3.3 4.2 5.0 5.8 6.7 7.5 8.3 9.2 10.0 10.8 11.7 12.5 13.3 14.2 15.0 358004 0.8 1.7 2.5 3.3 4.2 5.0 5.8 6.7 7.5 8.3 9.1 10.0 10.8 11.6 12.5 13.3 14.1 15.0 356006 0.8 1.7 2.5 3.3 4.1 5.0 5.8 6.6 7.5 8.3 9.1 9.9 10.8 11.6 12.4 13.3 14.1 14.9 354008 0.8 1.7 2.5 3.3 4.1 5.0 5.8 6.6 7.4 8.3 9.1 9.9 10.7 11.6 12.4 13.2 14.0 14.9 352

010 +0.8 +1.6 +2.5 +3.3 +4.1 +4.9 +5.7 +6.6 +7.4 +8.2 +9.0 +9.8 +10.7 +11.5 +12.3 +13.1 +14.0 +14.8 350012 0.8 1.6 2.4 3.3 4.1 4.9 5.7 6.5 7.3 8.2 9.0 9.8 10.6 11.4 12.2 13.0 13.9 14.7 348014 0.8 1.6 2.4 3.2 4.0 4.9 5.7 6.5 7.3 8.1 8.9 9.7 10.5 11.3 12.1 12.9 13.7 14.6 346016 0.8 1.6 2.4 3.2 4.0 4.8 5.6 6.4 7.2 8.0 8.8 9.6 10.4 11.2 12.0 12.8 13.6 14.4 344018 0.8 1.6 2.4 3.2 4.0 4.8 5.5 6.3 7.1 7.9 8.7 9.5 10.3 11.1 11.9 12.7 13.5 14.3 342

020 +0.8 +1.6 +2.3 +3.1 +3.9 +4.7 +5.5 +6.3 +7.0 +7.8 +8.6 +9.4 +10.2 +11.0 +11.7 +12.5 +13.3 +14.1 340022 0.8 1.5 2.3 3.1 3.9 4.6 5.4 6.2 7.0 7.7 8.5 9.3 10.0 10.8 11.6 12.4 13.1 13.9 338024 0.8 1.5 2.3 3.0 3.8 4.6 5.3 6.1 6.9 7.6 8.4 9.1 9.9 10.7 11.4 12.2 12.9 13.7 336026 0.7 1.5 2.2 3.0 3.7 4.5 5.2 6.0 6.7 7.5 8.2 9.0 9.7 10.5 11.2 12.0 12.7 13.5 334028 0.7 1.5 2.2 2.9 3.7 4.4 5.2 5.9 6.6 7.4 8.1 8.8 9.6 10.3 11.0 11.8 12.5 13.2 332

030 +0.7 +1.4 +2.2 +2.9 +3.6 +4.3 +5.1 +5.8 +6.5 +7.2 +7.9 +8.7 +9.4 +10.1 +10.8 +11.5 +12.3 +13.0 330032 0.7 1.4 2.1 2.8 3.5 4.2 4.9 5.7 6.4 7.1 7.8 8.5 9.2 9.9 10.6 11.3 12.0 12.7 328034 0.7 1.4 2.1 2.8 3.5 4.1 4.8 5.5 6.2 6.9 7.6 8.3 9.0 9.7 10.4 11.1 11.7 12.4 326036 0.7 1.3 2.0 2.7 3.4 4.0 4.7 5.4 6.1 6.7 7.4 8.1 8.8 9.4 10.1 10.8 11.5 12.1 324038 0.7 1.3 2.0 2.6 3.3 3.9 4.6 5.3 5.9 6.6 7.2 7.9 8.5 9.2 9.9 10.5 11.2 11.8 322

040 +0.6 +1.3 +1.9 +2.6 +3.2 +3.8 +4.5 +5.1 +5.7 +6.4 +7.0 +7.7 +8.3 +8.9 +9.6 +10.2 +10.9 +11.5 320042 0.6 1.2 1.9 2.5 3.1 3.7 4.3 5.0 5.6 6.2 6.8 7.4 8.1 8.7 9.3 9.9 10.5 11.1 318044 0.6 1.2 1.8 2.4 3.0 3.6 4.2 4.8 5.4 6.0 6.6 7.2 7.8 8.4 9.0 9.6 10.2 10.8 316046 0.6 1.2 1.7 2.3 2.9 3.5 4.1 4.6 5.2 5.8 6.4 6.9 7.5 8.1 8.7 9.3 9.8 10.4 314048 0.6 1.1 1.7 2.2 2.8 3.3 3.9 4.5 5.0 5.6 6.1 6.7 7.2 7.8 8.4 8.9 9.5 10.0 312

050 +0.5 +1.1 +1.6 +2.1 +2.7 +3.2 +3.7 +4.3 +4.8 +5.4 +5.9 +6.4 +7.0 +7.5 +8.0 +8.6 +9.1 +9.6 310052 0.5 1.0 1.5 2.1 2.6 3.1 3.6 4.1 4.6 5.1 5.6 6.2 6.7 7.2 7.7 8.2 8.7 9.2 308054 0.5 1.0 1.5 2.0 2.4 2.9 3.4 3.9 4.4 4.9 5.4 5.9 6.4 6.9 7.3 7.8 8.3 8.8 306056 0.5 0.9 1.4 1.9 2.3 2.8 3.3 3.7 4.2 4.7 5.1 5.6 6.1 6.5 7.0 7.5 7.9 8.4 304058 0.4 0.9 1.3 1.8 2.2 2.6 3.1 3.5 4.0 4.4 4.9 5.3 5.7 6.2 6.6 7.1 7.5 7.9 302

060 +0.4 +0.8 +1.3 +1.7 +2.1 +2.5 +2.9 +3.3 +3.8 +4.2 +4.6 +5.0 +5.4 +5.8 +6.3 +6.7 +7.1 +7.5 300062 0.4 0.8 1.2 1.6 2.0 2.3 2.7 3.1 3.5 3.9 4.3 4.7 5.1 5.5 5.9 6.3 6.7 7.0 298064 0.4 0.7 1.1 1.5 1.8 2.2 2.6 2.9 3.3 3.7 4.0 4.4 4.7 5.1 5.5 5.8 6.2 6.6 296066 0.3 0.7 1.0 1.4 1.7 2.0 2.4 2.7 3.1 3.4 3.7 4.1 4.4 4.7 5.1 5.4 5.8 6.1 294068 0.3 0.6 0.9 1.2 1.6 1.9 2.2 2.5 2.8 3.1 3.4 3.7 4.1 4.4 4.7 5.0 5.3 5.6 292

070 +0.3 +0.6 +0.9 +1.1 +1.4 +1.7 +2.0 +2.3 +2.6 +2.9 +3.1 +3.4 +3.7 +4.0 +4.3 +4.6 +4.8 +5.1 290072 0.3 0.5 0.8 1.0 1.3 1.5 1.8 2.1 2.3 2.6 2.8 3.1 3.3 3.6 3.9 4.1 4.4 4.6 288074 0.2 0.5 0.7 0.9 1.1 1.4 1.6 1.8 2.1 2.3 2.5 2.8 3.0 3.2 3.4 3.7 3.9 4.1 286076 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 2.6 2.8 3.0 3.2 3.4 3.6 284078 0.2 0.3 0.5 0.7 0.9 1.0 1.2 1.4 1.6 1.7 1.9 2.1 2.3 2.4 2.6 2.8 2.9 3.1 282

080 +0.1 +0.3 +0.4 +0.6 +0.7 +0.9 +1.0 +1.2 +1.3 +1.4 +1.6 +1.7 +1.9 +2.0 +2.2 +2.3 +2.5 +2.6 280082 0.1 0.2 0.3 0.5 0.6 0.7 0.8 0.9 1.0 1.2 1.3 1.4 1.5 1.6 1.7 1.9 2.0 2.1 278084 0.1 0.2 0.3 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.0 1.1 1.2 1.3 1.4 1.5 1.6 276086 0.1 0.1 0.2 0.2 0.3 0.3 0.4 0.5 0.5 0.6 0.6 0.7 0.8 0.8 0.9 0.9 1.0 1.0 274088 0.0 0.1 0.1 0.1 0.1 0.2 0.2 0.2 0.3 0.3 0.3 0.3 0.4 0.4 0.4 0.5 0.5 0.5 272

090 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 270

092 -0.0 -0.1 -0.1 -0.1 -0.1 -0.2 -0.2 -0.2 -0.3 -0.3 -0.3 -0.3 -0.4 -0.4 -0.4 -0.5 -0.5 -0.5 268094 0.1 0.1 0.2 0.2 0.3 0.3 0.4 0.5 0.5 0.6 0.6 0.7 0.8 0.8 0.9 0.9 1.0 1.0 266096 0.1 0.2 0.3 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 1.0 1.1 1.2 1.3 1.4 1.5 1.6 264098 0.1 0.2 0.3 0.5 0.6 0.7 0.8 0.9 1.0 1.2 1.3 1.4 1.5 1.6 1.7 1.9 2.0 2.1 262100 0.1 0.3 0.4 0.6 0.7 0.9 1.0 1.2 1.3 1.4 1.6 1.7 1.9 2.0 2.2 2.3 2.5 2.6 260

102 -0.2 -0.3 -0.5 -0.7 -0.9 -1.0 -1.2 -1.4 -1.6 -1.7 -1.9 -2.1 -2.3 -2.4 -2.6 -2.8 -2.9 -3.1 258104 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 2.6 2.8 3.0 3.2 3.4 3.6 256106 0.2 0.5 0.7 0.9 1.1 1.4 1.6 1.8 2.1 2.3 2.5 2.8 3.0 3.2 3.4 3.7 3.9 4.1 254108 0.3 0.5 0.8 1.0 1.3 1.5 1.8 2.1 2.3 2.6 2.8 3.1 3.3 3.6 3.9 4.1 4.4 4.6 252110 0.3 0.6 0.9 1.1 1.4 1.7 2.0 2.3 2.6 2.9 3.1 3.4 3.7 4.0 4.3 4.6 4.8 5.1 250

112 -0.3 -0.6 -0.9 -1.2 -1.6 -1.9 -2.2 -2.5 -2.8 -3.1 -3.4 -3.7 -4.1 -4.4 -4.7 -5.0 -5.3 -5.6 248114 0.3 0.7 1.0 1.4 1.7 2.0 2.4 2.7 3.1 3.4 3.7 4.1 4.4 4.7 5.1 5.4 5.8 6.1 246116 0.4 0.7 1.1 1.5 1.8 2.2 2.6 2.9 3.3 3.7 4.0 4.4 4.7 5.1 5.5 5.8 6.2 6.6 244118 0.4 0.8 1.2 1.6 2.0 2.3 2.7 3.1 3.5 3.9 4.3 4.7 5.1 5.5 5.9 6.3 6.7 7.0 242120 0.4 0.8 1.3 1.7 2.1 2.5 2.9 3.3 3.8 4.2 4.6 5.0 5.4 5.8 6.3 6.7 7.1 7.5 240

122 -0.4 -0.9 -1.3 -1.8 -2.2 -2.6 -3.1 -3.5 -4.0 -4.4 -4.9 -5.3 -5.7 -6.2 -6.6 -7.1 -7.5 -7.9 238124 0.5 0.9 1.4 1.9 2.3 2.8 3.3 3.7 4.2 4.7 5.1 5.6 6.1 6.5 7.0 7.5 7.9 8.4 236126 0.5 1.0 1.5 2.0 2.4 2.9 3.4 3.9 4.4 4.9 5.4 5.9 6.4 6.9 7.3 7.8 8.3 8.8 234128 0.5 1.0 1.5 2.1 2.6 3.1 3.6 4.1 4.6 5.1 5.6 6.2 6.7 7.2 7.7 8.2 8.7 9.2 232130 0.5 1.1 1.6 2.1 2.7 3.2 3.7 4.3 4.8 5.4 5.9 6.4 7.0 7.5 8.0 8.6 9.1 9.6 230

132 -0.6 -1.1 -1.7 -2.2 -2.8 -3.3 -3.9 -4.5 -5.0 -5.6 -6.1 -6.7 -7.2 -7.8 -8.4 -8.9 -9.5 -10.0 228134 0.6 1.2 1.7 2.3 2.9 3.5 4.1 4.6 5.2 5.8 6.4 6.9 7.5 8.1 8.7 9.3 9.8 10.4 226136 0.6 1.2 1.8 2.4 3.0 3.6 4.2 4.8 5.4 6.0 6.6 7.2 7.8 8.4 9.0 9.6 10.2 10.8 224138 0.6 1.2 1.9 2.5 3.1 3.7 4.3 5.0 5.6 6.2 6.8 7.4 8.1 8.7 9.3 9.9 10.5 11.1 222140 0.6 1.3 1.9 2.6 3.2 3.8 4.5 5.1 5.7 6.4 7.0 7.7 8.3 8.9 9.6 10.2 10.9 11.5 220

142 -0.7 -1.3 -2.0 -2.6 -3.3 -3.9 -4.6 -5.3 -5.9 -6.6 -7.2 -7.9 -8.5 -9.2 -9.9 -10.5 -11.2 -11.8 218144 0.7 1.3 2.0 2.7 3.4 4.0 4.7 5.4 6.1 6.7 7.4 8.1 8.8 9.4 10.1 10.8 11.5 12.1 216146 0.7 1.4 2.1 2.8 3.5 4.1 4.8 5.5 6.2 6.9 7.6 8.3 9.0 9.7 10.4 11.1 11.7 12.4 214148 0.7 1.4 2.1 2.8 3.5 4.2 4.9 5.7 6.4 7.1 7.8 8.5 9.2 9.9 10.6 11.3 12.0 12.7 212150 0.7 1.4 2.2 2.9 3.6 4.3 5.1 5.8 6.5 7.2 7.9 8.7 9.4 10.1 10.8 11.5 12.3 13.0 210

ALTERNATIVE TABLE 2 Altit d C ti f Ch i P iti f B d M O B



ALTERNATIVE TABLE 2—Altitude Correction for Change in Position of Body M. O. B.

Correction for 1 Minute of Time

TRUEZn

Latitude in DegreesTRUE

Zn0 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85

° ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ ′ °

T o f a c i l i t a t e u

s e o f P u b .

N o .

2 4 9 ,

V o l u m e 1 ,

2 , a n d 3

.

090 +15.0 +14.9 +14.8 +14.5 +14.1 +13.6 +13.0 +12.3 +11.5 +10.6 +9.6 +8.6 +7.5 +6.3 +5.1 +3.9 +2.6 +1.3 090092 15.0 14.9 14.8 14.5 14.1 13.6 13.0 12.3 11.5 10.6 9.6 8.6 7.5 6.3 5.1 3.9 2.6 1.3 088094 15.0 14.9 14.7 14.5 14.1 13.6 13.0 12.3 11.5 10.6 9.6 8.6 7.5 6.3 5.1 3.9 2.6 1.3 086096 14.9 14.9 14.7 14.4 14.0 13.5 12.9 12.2 11.4 10.5 9.6 8.6 7.5 6.3 5.1 3.9 2.6 1.3 084098 14.9 14.8 14.6 14.3 14.0 13.5 12.9 12.2 11.4 10.5 9.5 8.5 7.4 6.3 5.1 3.8 2.6 1.3 082

100 +14.8 +14.7 +14.5 +14.3 +13.9 +13.4 +12.8 +12.1 +11.3 +10.4 +9.5 +8.5 +7.4 +6.2 +5.1 +3.8 +2.6 +1.3 080102 14.7 14.6 14.4 14.2 13.8 13.3 12.7 12.0 11.2 10.4 9.4 8.4 7.3 6.2 5.0 3.8 2.5 1.3 078104 14.6 14.5 14.3 14.1 13.7 13.2 12.6 11.9 11.1 10.3 9.4 8.3 7.3 6.2 5.0 3.8 2.5 1.3 076106 14.4 14.4 14.2 13.9 13.5 13.1 12.5 11.8 11.0 10.2 9.3 8.3 7.2 6.1 4.9 3.7 2.5 1.3 074108 14.3 14.2 14.0 13.8 13.4 12.9 12.4 11.7 10.9 10.1 9.2 8.2 7.1 6.0 4.9 3.7 2.5 1.2 072

110 +14.1 +14.0 +13.9 +13.6 +13.2 +12.8 +12.2 +11.5 +10.8 +10.0 +9.1 +8.1 +7.0 +6.0 +4.8 +3.6 +2.4 +1.2 070112 13.9 13.9 13.7 13.4 13.1 12.6 12.0 11.4 10.7 9.8 8.9 8.0 7.0 5.9 4.8 3.6 2.4 1.2 068114 13.7 13.7 13.5 13.2 12.9 12.4 11.9 11.2 10.5 9.7 8.8 7.9 6.9 5.8 4.7 3.5 2.4 1.2 066116 13.5 13.4 13.3 13.0 12.7 12.2 11.7 11.0 10.3 9.5 8.7 7.7 6.7 5.7 4.6 3.5 2.3 1.2 064118 13.2 13.2 13.0 12.8 12.4 12.0 11.5 10.8 10.1 9.4 8.5 7.6 6.6 5.6 4.5 3.4 2.3 1.2 062

120 +13.0 +12.9 +12.8 +12.5 +12.2 +11.8 +11.3 +10.6 +10.0 +9.2 +8.4 +7.5 +6.5 +5.5 +4.4 +3.4 +2.3 +1.1 060122 12.7 12.7 12.5 12.3 12.0 11.5 11.0 10.4 9.7 9.0 8.2 7.3 6.4 5.4 4.4 3.3 2.2 1.1 058124 12.4 12.4 12.2 12.0 11.7 11.3 10.8 10.2 9.5 8.8 8.0 7.1 6.2 5.3 4.3 3.2 2.2 1.1 056126 12.1 12.1 12.0 11.7 11.4 11.0 10.5 9.9 9.3 8.6 7.8 7.0 6.1 5.1 4.2 3.1 2.1 1.1 054128 11.8 11.8 11.6 11.4 11.1 10.7 10.2 9.7 9.1 8.4 7.6 6.8 5.9 5.0 4.0 3.1 2.1 1.0 052

130 +11.5 +11.4 +11.3 +11.1 +10.8 +10.4 +10.0 +9.4 +8.8 +8.1 +7.4 +6.6 +5.7 +4.9 +3.9 +3.0 +2.0 +1.0 050132 11.1 11.1 11.0 10.8 10.5 10.1 9.7 9.1 8.5 7.9 7.2 6.4 5.6 4.7 3.8 2.9 1.9 1.0 048134 10.8 10.8 10.6 10.4 10.1 9.8 9.3 8.8 8.3 7.6 6.9 6.2 5.4 4.6 3.7 2.8 1.9 0.9 046136 10.4 10.4 10.3 10.1 9.8 9.4 9.0 8.5 8.0 7.4 6.7 6.0 5.2 4.4 3.6 2.7 1.8 0.9 044138 10.0 10.0 9.9 9.7 9.4 9.1 8.7 8.2 7.7 7.1 6.5 5.8 5.0 4.2 3.4 2.6 1.7 0.9 042

140 +9.6 +9.6 +9.5 +9.3 +9.1 +8.7 +8.4 +7.9 +7.4 +6.8 +6.2 +5.5 +4.8 +4.1 +3.3 +2.5 +1.7 +0.8 040142 9.2 9.2 9.1 8.9 8.7 8.4 8.0 7.6 7.1 6.5 5.9 5.3 4.6 3.9 3.2 2.4 1.6 0.8 038144 8.8 8.8 8.7 8.5 8.3 8.0 7.6 7.2 6.8 6.2 5.7 5.1 4.4 3.7 3.0 2.3 1.5 0.8 036146 8.4 8.4 8.3 8.1 7.9 7.6 7.3 6.9 6.4 5.9 5.4 4.8 4.2 3.5 2.9 2.2 1.5 0.7 034148 7.9 7.9 7.8 7.7 7.5 7.2 6.9 6.5 6.1 5.6 5.1 4.6 4.0 3.4 2.7 2.1 1.4 0.7 032

150 +7.5 +7.5 +7.4 +7.2 +7.0 +6.8 +6.5 +6.1 +5.7 +5.3 +4.8 +4.3 +3.8 +3.2 +2.6 +1.9 +1.3 +0.7 030152 7.0 7.0 6.9 6.8 6.6 6.4 6.1 5.8 5.4 5.0 4.5 4.0 3.5 3.0 2.4 1.8 1.2 0.6 028154 6.6 6.6 6.5 6.4 6.2 6.0 5.7 5.4 5.0 4.6 4.2 3.8 3.3 2.8 2.2 1.7 1.1 0.6 026156 6.1 6.1 6.0 5.9 5.7 5.5 5.3 5.0 4.7 4.3 3.9 3.5 3.1 2.6 2.1 1.6 1.1 0.5 024158 5.6 5.6 5.5 5.4 5.3 5.1 4.9 4.6 4.3 4.0 3.6 3.2 2.8 2.4 1.9 1.5 1.0 0.5 022

160 +5.1 +5.1 +5.1 +5.0 +4.8 +4.6 +4.4 +4.2 +3.9 +3.6 +3.3 +2.9 +2.6 +2.2 +1.8 +1.3 +0.9 +0.4 020162 4.6 4.6 4.6 4.5 4.4 4.2 4.0 3.8 3.6 3.3 3.0 2.7 2.3 2.0 1.6 1.2 0.8 0.4 018164 4.1 4.1 4.1 4.0 3.9 3.7 3.6 3.4 3.2 2.9 2.7 2.4 2.1 1.7 1.4 1.1 0.7 0.4 016166 3.6 3.6 3.6 3.5 3.4 3.3 3.1 3.0 2.8 2.6 2.3 2.1 1.8 1.5 1.2 0.9 0.6 0.3 014168 3.1 3.1 3.1 3.0 2.9 2.8 2.7 2.6 2.4 2.2 2.0 1.8 1.6 1.3 1.1 0.8 0.5 0.3 012

170 +2.6 +2.6 +2.6 +2.5 +2.4 +2.4 +2.3 +2.1 +2.0 +1.8 +1.7 +1.5 +1.3 +1.1 +0.9 +0.7 +0.5 +0.2 010172 2.1 2.1 2.1 2.0 2.0 1.9 1.8 1.7 1.6 1.5 1.3 1.2 1.0 0.9 0.7 0.5 0.4 0.2 008174 1.6 1.6 1.5 1.5 1.5 1.4 1.4 1.3 1.2 1.1 1.0 0.9 0.8 0.7 0.5 0.4 0.3 0.1 006176 1.0 1.0 1.0 1.0 1.0 1.0 0.9 0.9 0.8 0.7 0.7 0.6 0.5 0.4 0.4 0.3 0.2 0.1 004178 0.5 0.5 0.5 0.5 0.5 0.5 0.5 0.4 0.4 0.4 0.3 0.3 0.3 0.2 0.2 0.1 0.1 0.0 002

180 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 000

182 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.5 -0.4 -0.4 -0.4 -0.3 -0.3 -0.3 -0.2 -0.2 -0.1 -0.1 -0.0 358184 1.0 1.0 1.0 1.0 1.0 1.0 0.9 0.9 0.8 0.7 0.7 0.6 0.5 0.4 0.4 0.3 0.2 0.1 356186 1.6 1.6 1.5 1.5 1.5 1.4 1.4 1.3 1.2 1.1 1.0 0.9 0.8 0.7 0.5 0.4 0.3 0.1 354188 2.1 2.1 2.1 2.0 2.0 1.9 1.8 1.7 1.6 1.5 1.3 1.2 1.0 0.9 0.7 0.5 0.4 0.2 352190 2.6 2.6 2.6 2.5 2.4 2.4 2.3 2.1 2.0 1.8 1.7 1.5 1.3 1.1 0.9 0.7 0.5 0.2 350

192 -3.1 -3.1 -3.1 -3.0 -2.9 -2.8 -2.7 -2.6 -2.4 -2.2 -2.0 -1.8 -1.6 -1.3 -1.1 -0.8 -0.5 -0.3 348194 3.6 3.6 3.6 3.5 3.4 3.3 3.1 3.0 2.8 2.6 2.3 2.1 1.8 1.5 1.2 0.9 0.6 0.3 346196 4.1 4.1 4.1 4.0 3.9 3.7 3.6 3.4 3.2 2.9 2.7 2.4 2.1 1.7 1.4 1.1 0.7 0.4 344198 4.6 4.6 4.6 4.5 4.4 4.2 4.0 3.8 3.6 3.3 3.0 2.7 2.3 2.0 1.6 1.2 0.8 0.4 342200 5.1 5.1 5.1 5.0 4.8 4.6 4.4 4.2 3.9 3.6 3.3 2.9 2.6 2.2 1.8 1.3 0.9 0.4 340

202 -5.6 -5.6 -5.5 -5.4 -5.3 -5.1 -4.9 -4.6 -4.3 -4.0 -3.6 -3.2 -2.8 -2.4 -1.9 -1.5 -1.0 -0.5 338204 6.1 6.1 6.0 5.9 5.7 5.5 5.3 5.0 4.7 4.3 3.9 3.5 3.1 2.6 2.1 1.6 1.1 0.5 336206 6.6 6.6 6.5 6.4 6.2 6.0 5.7 5.4 5.0 4.6 4.2 3.8 3.3 2.8 2.2 1.7 1.1 0.6 334208 7.0 7.0 6.9 6.8 6.6 6.4 6.1 5.8 5.4 5.0 4.5 4.0 3.5 3.0 2.4 1.8 1.2 0.6 332210 7.5 7.5 7.4 7.2 7.0 6.8 6.5 6.1 5.7 5.3 4.8 4.3 3.8 3.2 2.6 1.9 1.3 0.7 330

212 -7.9 -7.9 -7.8 -7.7 -7.5 -7.2 -6.9 -6.5 -6.1 -5.6 -5.1 -4.6 -4.0 -3.4 -2.7 -2.1 -1.4 -0.7 328214 8.4 8.4 8.3 8.1 7.9 7.6 7.3 6.9 6.4 5.9 5.4 4.8 4.2 3.5 2.9 2.2 1.5 0.7 326216 8.8 8.8 8.7 8.5 8.3 8.0 7.6 7.2 6.8 6.2 5.7 5.1 4.4 3.7 3.0 2.3 1.5 0.8 324218 9.2 9.2 9.1 8.9 8.7 8.4 8.0 7.6 7.1 6.5 5.9 5.3 4.6 3.9 3.2 2.4 1.6 0.8 322220 9.6 9.6 9.5 9.3 9.1 8.7 8.4 7.9 7.4 6.8 6.2 5.5 4.8 4.1 3.3 2.5 1.7 0.8 320

222 -10.0 -10.0 -9.9 -9.7 -9.4 -9.1 -8.7 -8.2 -7.7 -7.1 -6.5 -5.8 -5.0 -4.2 -3.4 -2.6 -1.7 -0.9 318224 10.4 10.4 10.3 10.1 9.8 9.4 9.0 8.5 8.0 7.4 6.7 6.0 5.2 4.4 3.6 2.7 1.8 0.9 316226 10.8 10.8 10.6 10.4 10.1 9.8 9.3 8.8 8.3 7.6 6.9 6.2 5.4 4.6 3.7 2.8 1.9 0.9 314228 11.1 11.1 11.0 10.8 10.5 10.1 9.7 9.1 8.5 7.9 7.2 6.4 5.6 4.7 3.8 2.9 1.9 1.0 312230 11.5 11.4 11.3 11.1 10.8 10.4 10.0 9.4 8.8 8.1 7.4 6.6 5.7 4.9 3.9 3.0 2.0 1.0 310

232 -11.8 -11.8 -11.6 -11.4 -11.1 -10.7 -10.2 -9.7 -9.1 -8.4 -7.6 -6.8 -5.9 -5.0 -4.0 -3.1 -2.1 -1.0 308234 12.1 12.1 12.0 11.7 11.4 11.0 10.5 9.9 9.3 8.6 7.8 7.0 6.1 5.1 4.2 3.1 2.1 1.1 306236 12.4 12.4 12.2 12.0 11.7 11.3 10.8 10.2 9.5 8.8 8.0 7.1 6.2 5.3 4.3 3.2 2.2 1.1 304238 12.7 12.7 12.5 12.3 12.0 11.5 11.0 10.4 9.7 9.0 8.2 7.3 6.4 5.4 4.4 3.3 2.2 1.1 302240 13.0 12.9 12.8 12.5 12.2 11.8 11.3 10.6 10.0 9.2 8.4 7.5 6.5 5.5 4.4 3.4 2.3 1.1 300

NAVIGATIONAL STARS



G O S S

Alphabetical Order Order of SHA

Name No.

MagnitudeSHA

1985.0

Dec

1985.0Name No.

MagnitudeSHA

1985.0

Dec

1985.0Visual S-4 Visual S-4

° ′ ° ′ °′

°′Acamar 7 3.1 3.2 315 35 S 40 22 Markab* 57 2.6 2.3 14 00 N 15 07

ACHERNAR 5 0.6 0.1 335 43 S 57 19 FOMALHAUT 56 1.3 1.3 15 48 S 29 42ACRUX 30 1.1 0.5 173 34 S 63 01 Al Na’ir* 55 2.2 1.8 28 11 S 47 02Adhara* 19 1.6 1.2 255 29 S 28 57 Enif 54 2.5 4.8 34 08 N 9 48ALDEBARAN 10 1.1 3.1 291 14 N 16 29 DENEB 53 1.3 1.4 49 46 N 45 14

Alioth 32 1.7 1.5 166 39 N 56 02 Peacock 52 2.1 1.7 53 53 S 56 47Alkaid 34 1.9 1.5 153 16 N 49 23 ALTAIR 51 0.9 1.0 62 29 N 8 50Al Na’ir* 55 2.2 1.8 28 11 S 47 02 Nunki 50 2.1 1.9 76 25 S 26 19Alnilam* 15 1.8 1.3 276 08 S 1 13 VEGA 49 0.1 0.0 80 54 N 38 46Alphard 25 2.2 4.4 218 17 S 8 36 Kaus Australis* 48 2.0 2.0 84 12 S 34 24

Alphecca 41 2.3 2.1 126 29 N 26 46 Eltanin* 47 2.4 4.6 90 56 N 51 29Alpheratz 1 2.2 1.8 358 06 N 29 00 Rasalhague 46 2.1 2.2 96 26 N 12 34ALTAIR 51 0.9 1.0 62 29 N 8 50 Shaula 45 1.7 1.3 96 51 S 37 06Ankaa* 2 2.4 3.9 353 37 S 42 23 Sabik* 44 2.6 2.5 102 37 S 15 42ANTARES 42 1.2 3.7 112 53 S 26 24 Atria* 43 1.9 4.1 108 14 S 69 00

ARCTURUS 37 0.2 1.9 146 15 N 19 16 ANTARES 42 1.2 3.7 112 53 S 26 24Atria* 43 1.9 4.1 108 14 S 69 00 Alphecca 41 2.3 2.1 126 29 N 26 46Avior* 22 1.7 3.3 234 27 S 59 28 Kochab 40 2.2 4.3 137 19 N 74 13Bellatrix* 13 1.7 1.2 278 55 N 6 20 Zubenelgenubi* 39 2.9 3.2 137 29 S 15 59BETELGEUSE 16 0.1-1.2 2.5-3.6 271 25 N 7 24 RIGIL KENT. 38 0.1 0.9 140 21 S 60 46

CANOPUS 17 -0.9 -0.8 264 06 S 52 41 ARCTURUS 37 0.2 1.9 146 15 N 19 16CAPELLA 12 0.2 1.3 281 06 N 45 59 Menkent* 36 2.3 3.5 148 33 S 36 18DENEB 53 1.3 1.4 49 46 N 45 14 HADAR* 35 0.9 0.3 149 19 S 60 18Denebola 28 2.2 2.2 182 56 N 14 39 Alkaid 34 1.9 1.5 153 16 N 49 23Diphda 4 2.2 3.6 349 17 S 18 04 SPICA 33 1.2 0.7 158 54 S 11 05

Dubhe 27 2.0 3.4 194 18 N 61 50 Alioth 32 1.7 1.5 166 39 N 56 02Elnath* 14 1.8 1.4 278 40 N 28 36 Gacrux* 31 1.6 4.1 172 25 S 57 02Eltanin* 47 2.4 4.6 90 56 N 51 29 ACRUX 30 1.1 0.5 173 34 S 63 01Enif 54 2.5 4.8 34 08 N 9 48 Gienah 29 2.8 2.5 176 15 S 17 28FOMALHAUT 56 1.3 1.3 15 48 S 29 42 Denebola 28 2.2 2.2 182 56 N 14 39

Gacrux* 31

1.6 4.1 172 25 S 57 02 Dubhe 27

2.0 3.4 194 18 N 61 50Gienah 29 2.8 2.5 176 15 S 17 28 REGULUS 26 1.3 1.0 208 06 N 12 02HADAR* 35 0.9 0.3 149 19 S 60 18 Alphard 25 2.2 4.4 218 17 S 8 36Hamal 6 2.2 3.8 328 25 N 23 24 Miaplacidus 24 1.8 1.8 221 44 S 69 39Kaus Australis* 48 2.0 2.0 84 12 S 34 24 Suhail 23 2.2 4.6 223 08 S 43 22

Kochab 40 2.2 4.3 137 19 N 74 13 Avior* 22 1.7 3.3 234 27 S 59 28Markab* 57 2.6 2.3 14 00 N 15 07 POLLUX 21 1.2 2.5 243 54 N 28 04Menkar 8 2.8 5.3 314 38 N 4 02 PROCYON 20 0.5 0.8 245 22 N 5 16Menkent* 36 2.3 3.5 148 33 S 36 18 Adhara* 19 1.6 1.2 255 29 S 28 57Miaplacidus 24 1.8 1.8 221 44 S 69 39 SIRIUS 18 -1.6 -1.5 258 53 S 16 42

Mirfak 9 1.9 2.4 309 11 N 49 49 CANOPUS 17 -0.9 -0.8 264 06 S 52 41

Nunki 50 2.1 1.9 76 25 S 26 19 BETELGEUSE 16 0.1-1.2 2.5-3.6 271 25 N 7 24Peacock 52 2.1 1.7 53 53 S 56 47 Alnilam* 15 1.8 1.3 276 08 S 1 13POLLUX 21 1.2 2.5 243 54 N 28 04 Elnath* 14 1.8 1.4 278 40 N 28 36PROCYON 20 0.5 0.8 245 22 N 5 16 Bellatrix* 13 1.7 1.2 278 55 N 6 20

Rasalhague 46 2.1 2.2 96 26 N 12 34 CAPELLA 12 0.2 1.3 281 06 N 45 59REGULUS 26 1.3 1.0 208 06 N 12 02 RIGEL 11 0.3 0.0 281 33 S 8 13RIGEL 11 0.3 0.0 281 33 S 8 13 ALDEBARAN 10 1.1 3.1 291 14 N 16 29RIGIL KENT 38 0 1 0 9 140 21 S 60 46 Mi f k 9 1 9 2 4 309 11 N 49 49



SIGHT REDUCTION TABLES

FOR

AIR NAVIGATION

LATITUDES 0°−

40°

DECLINATIONS 0° − 29°









































































































































































































































































































































































































































































































Pub249Vol2 latitudes 0º-40º

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