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| METHODS OF
CALCULATING CRESCENT LENGTH |
M. Shahid Qureshi1 and Nasiruddin Khan2
1 Institute
of Space & Planetary Astrophysics, 2Department of
Mathematics,
University of Karachi,
Karachi-75270, Pakistan
|
| ABSTRACT |
| A number of authors have described
the reasons for the shortening of the length of new lunar
crescent. McNally devised a mathematical technique to find the
shortened length of crescent using his formula for the width.
Recently Sultan has also developed a mathematical technique to
calculate the length of crescent on the basis of Blackwell
contrast threshold. In the present paper a technique for
calculating the “observed length” of the new lunar crescent
based on the lower limit on the visible width of crescent is
developed using q-value criterion of Yallop. This technique is
than used to calculate the crescent length for a number of
observations reported in literature since the time of Schmidt of
Athens. Finally a comparison of the observed crescent lengths is
done with the calculated lengths using our technique and the
calculated lengths on the basis of the formulas due to Sultan
and McNally. The results of this work are consistent with the
observed lengths whereas those due to others are generally
inconsistent. |
| Keywords:Moon, Surface of Moon, Lunar Crescent. |
| 1. INTRODUCTION |
The fact, that the new lunar
crescent appears shorter than 1800 in length, is
known for centuries. It was Danjon who first gave an explanation
for the phenomenon (Danjon, 1932 & 1936) and attributed it to
the lunar terrain close to the cusps. McNally attributed a
different reason with this phenomenon discarding Danjon’s
hypothesis (Mcnally, 1983). McNally proved that the length of
the shadows close to the lunar cusp and the departure of lunar
surface from being perfect sphere couldn’t diminish the
brightness of the regions of crescent close to cusps to the
level that they become invisible. Therefore he attributed the
length shortening of crescent to the “seeing affect” due to the
turbulence of the atmosphere. Schaeffer rejected McNally’s
explanation on the basis of his view that the shortening of the
crescent length is simply because of the sharp decline of the
brightness of the crescent close to the cusps (Schaeffer, 1991).
McNally has also developed formulas for calculating the length
of the crescent. Using the accurate model of Hapke (1984) for
calculating the surface brightness of the crescent Schaeffer
claims that Danjon’s collected observations and his own new data
fits the model. Lately Sultan (2005) has attributed the
shortening of length of crescent to the Blackwell Contrast
Threshold (1946) and has developed a formula to calculate
crescent’s length.
Most of the early description of
the p henomena concentrated on relating it to the phase (or
elongation) of the Moon. The description by Danjon was shown to
be incorrect mathematically by McNally. However his over
estimated limit on the minimum width of visible crescent (2 to 6
arc seconds) lead to very small values for Danjon Limit. The
description due to McNally is logically sound so is that of
Sultan and both resulted into techniques for calculating length
of crescent. However both McNally and Sultan have not reported
the application of their description on the recorded historical
data found in literature (Yallop, 1998, Schaeffer 1991 etc.).
According to Danjon, as described by Fatoohi et.al.
(1.1)
Where the arc PQ = α is the
deficiency arc in Fig. 1 (Fatoohi et. Al.. 1998), a is
the elongation and w is half the crescent length. It appears that Danjon used the Sine
formulae by assuming spherical angle at Q to be right angle.
McNally rejected Danjon’s argument and using four-part formula
arrives at:
(1.2)
Numerically, for small angles α
and a there is only a marginal difference between the two
results. Generally the elongation (a) can be calculated
and the crescent length (2ω) is observed, so the two formulas
can be used to find the deficiency arc. However, to calculate
the crescent length none of these can be used. McNally develops
a formula for angular separation φ from a cusp in terms of
crescent width R as:
(1.3)
where DR is the minimum visible width measured in
disc. Therefore the length of the
crescent he obtains is 1800 - 2φ.
Using the Blackwell threshold
contrast Sultan (2005) arrives at the minimum visible width (in
terms of diameter of the smallest equivalent Blackwell (1946)
disc) of crescent at perigee and apogee at his location of
observation. The formula that he developed for calculating the
crescent length is:
(1.4)
where r is the
semi-diameter of the Moon, and
(1.5)
with w is the diameter of
the smallest visible equivalent Blackwell disc and W is
central width of the crescent. Sultan considers minimum diameter
of Blackwell disc to be 0.14 arc minutes when the Moon is near
perigee and 0.16 arc minutes when the Moon is near apogee.
The present work is based on the
observation of the last (old) crescent on February 26, 2006.
During this observation that started from the beginning of
morning twilight till well past sunrise, it was noticed that for
this –48 hours Moon, more than 27 degrees away from the sun the
crescent length started to decline with the rising sun. A
similar observation on March 28th when the age of
Moon was around –33 hours and around 18.5 degrees away from the
sun, the crescent length decreased more rapidly with decreasing
contrast. Two days later new crescent with age 27.6 hours at 15
degrees away from the sun was observed till setting. Close to
the horizon through thick humid atmosphere the crescent length
was again observed to be decreasing. These observations clearly
demonstrate that there is much more to be explored about the
phenomenon of shortening of crescent length apart from Hapke’s
accurate model that shows dependence of crescent length on
elongation alone.
Therefore, in this work, to begin
with we consider a simple geometrical model for the crescent.
The model describes the phenomenon of shortening of length that
depends on the actual semi-diameter of the Moon as well as the
relative altitude (ARCV) of the crescent over local sky. This is
derived from the single parameter (q-value) criterion of
earliest visibility of crescent due to Yallop (1998) and is
based on the fact that whenever the width (or brightness) of
crescent close to cusp is below the minimum visible central
width (or brightness) of the crescent the whole length of
crescent with smaller width would not be visible. Applying our
model on the recorded visibility and invisibility data available
the length of crescent in each case is calculated. The
calculated lengths of crescent are also compared with the
observed lengths and with the lengths calculated using formulas
(1.3) due to McNally and (1.4 & 1.5) due to Sultan. In case of
using McNally’s formula ΔR is considered from the
criterion used in this work and for Sultan’s formula the minimum
width of Blackwell disc (w) is also considered to be the
one we developed.
|
| 2. THE WIDTH OF CRESCENT |
Let O be the centre of the lunar
disc and the origin of coordinate system, x-axis be the
direction of the Earth, y-axis is along OB and the z-axis along
OC. C and D are the Cusps of the crescent. OS is the direction
of the Sun and the angle between OS and the negative x-axis is
the elongation E of the Moon from the Sun as seen from the
Earth. As shown in the Fig. 1 the disc of the Moon as seen from
the Earth is the circle ACBD that lies in the plane of the paper
(yz-plane), whereas the part of the lunar surface exposed to the
Sun is the hemisphere described by the semicircle CFD. Thus the
illuminated part of the surface of the Moon that is exposed to
view from the Earth is the region between the semicircle CFD and
the semi circle CBD.
Fig: 1
Geometry of Crescent.
If the
semi circle CFD that is above the plane of the paper (the octant
with positive x and y) is projected on to the plane of the paper
it forms a half ellipse. A point in the region between
semi-circle CBD and CFD is represented by:
(2.1)
where r is the radius of
the lunar disc, φ varies from 00 (along z-axis) to
1800 (along negative z-axis) and θ varies from 900 –E (plane of semi-circle DFC) to 900 (plane of
paper). If all these points are projected on the plane of the
paper we obtain the crescent that can be seen from the Earth.
The region is shown in Fig. 2 as the region enclosed between the
half ellipse CF’D and the half circle CBD. The outer limb is
described by a circle of radius equal to radius of the Moon
given parametrically by:
(2.2)
Fig. 2
Width of Crescent
The inner terminator CF’D is
described by:
(2.3)
which is an ellipse. The width of
the crescent along its length at any point is then the
difference between the y-coordinates for same values of
z:
(2.4)
This width of the crescent is
defined parallel to the plane containing the centers of the Sun,
the Moon and the observer (segment JK in fig. 2). The width
defined by McNally is in the radial direction (segment HK in
fig. 2). The reason that we have defined the width in this way
is that as the lunar phase increases JK increases from
zero at any j to rSinj (00 to 1800 along OB) whereas McNally’s model gives the width W in radial direction so that at 900 elongations ΔR is same as the semi-diameter R. According to our
definition (2.4) that considers the latitudinal width describes
the variation in width for all values of elongation. The
definition (2.4) shows that the width at the cusps (
and
)
geometrically vanishes. The width of the crescent at its center
(j = 900) is simply:
(2.5)
This agrees with the definition
of McNally:
(2.5a)
Which also yield the same central
width (at φ = 900) as given by (2.5).
The Table
1 shows the widths of crescent for various elongations against
the displacement from the cusp to the center of crescent
according to (2.4). This describes the width of complete Moon at
every latitude of the lunar surface. Thereby for 900 elongations the crescent “width” goes from around 77 arc seconds
at 50 from cusp to the maximum “width” of 882 arc
seconds at 900 from the cusp. McNally has reported
this only up to elongation 90 0 in table II (pp 426,
1983). It shows the maximum width of illuminated lunar surface
to be 932 arc-sec for 900 for every point from cusp
to center of the crescent. Table 1 is generated for only the
minimum semi-diameter of lunar disc when the Moon is at the
greatest distance. Similar data can be generated for various
semi-diameters up to the maximum possible (when the Moon is
closest).
|
| 3. THE BRIGHTNESS OF CRESCENT |
A vector normal to the point
given by (2.1) is
and
the unit vector in the direction of the Sun at the
same point is
.
Therefore the solar flux received at any point of the
illuminated surface of the Moon is given by:
.
(3.1)
\Where Fm is the
maximum solar flux at the point on the lunar surface where the
Sun is at the zenith. In view of equation (3.1) as θ varies from
900 – E to 900 the flux received by
lunar surface decreases sharply for values of θ close to 900 – E. The total solar flux received by the visible
crescent, integrated over the whole region
that
defines the visible crescent, is then given by:
(3.2)
This total solar flux received by
the crescent is the measure of the brightness of the crescent.
It depends on the maximum possible solar flux Fm, received by the Moon that itself depend on the distance
between the Sun and the Moon, the semi diameter r and the
elongation E of the Moon from the Sun. Thus brightness
and consequently the visibility of the crescent must depend on
all these factors.
The actual brightness of the visible crescent depends on the
albedo “a” (reflectivity of lunar surface) and on the
distance R of the observer from the Moon. The intensity
Table 1: Width of crescent along
its length from cusp to the center according to Formula (2.4)
using smallest value 882 arc-sec for semi-diameter of lunar
disc.
Left most column =
angular distance from cusp, Top row shows the elongation
of Moon |
Ψ\E |
50 |
100 |
450 |
600 |
800 |
900 |
1200 |
1400 |
1600 |
1800 |
50 |
0.292 |
1.1678 |
22.515 |
38.436 |
63.523 |
76.871 |
115.31 |
135.76 |
149.11 |
153.74 |
100 |
0.582 |
2.3268 |
44.859 |
76.579 |
126.56 |
153.16 |
229.74 |
270.48 |
297.08 |
306.32 |
150 |
0.868 |
3.4681 |
66.861 |
114.14 |
188.64 |
228.28 |
342.42 |
403.15 |
442.79 |
456.56 |
200 |
1.147 |
4.5829 |
88.355 |
150.83 |
249.28 |
301.66 |
452.49 |
532.75 |
585.13 |
603.32 |
250 |
1.418 |
5.6629 |
109.18 |
186.37 |
308.02 |
372.75 |
559.12 |
658.29 |
723.02 |
745.5 |
300 |
1.678 |
6.6998 |
129.17 |
220.5 |
364.42 |
441 |
661.5 |
778.83 |
855.4 |
882 |
350 |
1.925 |
7.6857 |
148.17 |
252.95 |
418.05 |
505.89 |
758.84 |
893.43 |
981.28 |
1011.8 |
400 |
2.157 |
8.6131 |
166.05 |
283.47 |
468.49 |
566.94 |
850.41 |
1001.2 |
1099.7 |
1133.9 |
450 |
2.373 |
9.4749 |
182.67 |
311.83 |
515.37 |
623.67 |
935.5 |
1101.4 |
1209.7 |
1247.3 |
500 |
2.571 |
10.265 |
197.89 |
337.83 |
558.33 |
675.65 |
1013.5 |
1193.2 |
1310.6 |
1351.3 |
550 |
2.749 |
10.976 |
211.61 |
361.25 |
597.03 |
722.49 |
1083.7 |
1276 |
1401.4 |
1445 |
600 |
2.906 |
11.604 |
223.72 |
381.92 |
631.2 |
763.83 |
1145.8 |
1349 |
1481.6 |
1527.7 |
650 |
3.041 |
12.144 |
234.13 |
399.68 |
660.56 |
799.36 |
1199 |
1411.7 |
1550.5 |
1598.7 |
700 |
3.153 |
12.591 |
242.75 |
414.4 |
684.89 |
828.81 |
1243.2 |
1463.7 |
1607.6 |
1657.6 |
750 |
3.241 |
12.943 |
249.53 |
425.97 |
704.01 |
851.95 |
1277.9 |
1504.6 |
1652.5 |
1703.9 |
800 |
3.305 |
13.196 |
254.41 |
434.3 |
717.77 |
868.6 |
1302.9 |
1534 |
1684.8 |
1737.2 |
850 |
3.343 |
13.349 |
257.35 |
439.32 |
726.07 |
878.64 |
1318 |
1551.7 |
1704.3 |
1757.3 |
900 |
3.356 |
13.4 |
258.33 |
441 |
728.84 |
882 |
1323 |
1557.7 |
1710.8 |
1764 |
of light decreases as the square
of the distance, therefore the actual brightness of the visible
crescent is:
or
(3.3)
where S is the
semi-diameter,
of
the Moon and
is
the phase of the Moon. The equations (3.3) show that
the
brightness of the crescent varies as square of its
semi-diameter. Across the length of the crescent both the width W and the brightness B varies, being greatest at
the center and decreasing away from the centre. If (3.1) is
integrated only over θ then the expression for brightness along
a constant φ is:
(3.4)
(2.4) gives the width of the
crescent for fixed φ as:
(3.5)
Mathematically both the
brightness and the width vanish as φ approaches 00 or
1800 and both these expressions may be re-written as:
(3.6)
(3.7)
where ψ varies from 00 to 900 along the length of the crescent from centre
to a cusp respectively. The plot of the variations in the
brightness depending on y and E only is shown in Fig. 3 is in agreement with the Fig No 2 (pp
270) of Schaeffer (1991) in the sense that both exhibit a sharp
decline in the brightness close to the cusp. Fig. 4 shows the
variations in the magnitude of the crescent along its length
from center to the cusp for different elongation. Taking into
consideration the semi-diameter (r/R), the maximum solar flux Fm on the lunar surface (at any point of time)
and the albedo of the lunar surface more realistic brightness
values may be obtained.
|
| 4. THE LENGTH OF THE CRESCENT |
width of crescent is not only
dependent on the Elongation as treated by many authors that have
dealt with the problem of the length of lunar crescent and it’s
shortening but it also depends upon the actual radius,
semi-diameter, of the Moon that appeared in the expression
above. The minimum semi-diameter when the Moon is farthest from
us is 14.7 arc minutes and the maximum is 16.74 arc-minute. Thus
for the same elongation E, φ = 900, Wc may be 13.9% as
great as its minimum possible value and the total area of the lunar disc when closest
may be as large as 30% to that when it is farthest. Thus there
ought to be significant variations in the width and the
brightness of the crescent.
For the development of any model
that describes the minimum possible width that can be visible
through naked eye one requires to seek guidance from the actual
observations. In the history of scientifically reported
observation of the very young crescent Moon, the record is that
due to Pierce on February 25, 1990 (reported by Schaefer and
Yallop). The crescent he claims to have seen with naked eye was
just 14.8 hours and its width was 0.18 arc minute. Amongst all
the recorded observations the sighting of such a young and thin
crescent was never reported. In the model that is developed in
this work the lower limit of the width of visible crescent is
considered to be 0.18 arc minute. However this minimum is not
the absolute minimum for all crescents for all possible relative
altitudes (ARCV). In this work we consider this minimum of 0.18
arc-minutes of crescent width when the relative azimuth DAZ of
the Moon is zero and the relative altitude ARCV gives the
q-value of -0.22 according to Yallop’s criterion:
q = (ARCV - (11·8371 - 6·3226 W
+ 0·7319 W 2 - 0·1018 W 3 )) / 10 (4.1)
Fig. 3: Logarithmic Dependence of
Brightness of Crescent along its length on distance from
crescent’s center.
Fig. 4: Magnitude of Crescent along its length for various
Elongation
Thus for q = -2.2,
ARCV =9·6371 - 6·3226 W +
0·7319 W 2 - 0·1018 W 3 (4.2)
The
minimum ARCV according to this criterion giving the q-value
equal to -0.22 would yield a different lower limit on the
visible width of the crescent. This is caused by different
relative azimuths DAZ. For the least possible ARCV (zero) the
width of the invisible crescent would be around 108 arc-seconds
that occurs at a large value of DAZ. In view of this criterion
the minimum width of visible crescent for any ARCV is termed Wm and as the crescent is just invisible for this
width:
(4.3)
Where Wc is the
theoretical central width of the crescent given by (2.5) and
is
the reduced width at angle ψ from the center of the width. Wm is the width reduced by the relative altitude ARCV. In order
that some part of crescent is visible
at
some value ψ = ψm. Thus the effective visible width
of the crescent for ψ ranging from 00 to ψm is given by:
(4.4)
As mentioned earlier (equation
3.1) the brightness of crescent falls sharply as θ approaches 900 – E the actual visible width of crescent at any value of
ψ must be less than the geometric value of width given by
equation (3.7). Therefore the “effective visible width” given by
(4.4) is justified. Thus it is not only the length of crescent
that shortens but the visible width of crescent has to diminish
also. Whenever the crescent is invisible in view of (4.3) y m has to vanish so that:
(4.5)
In all other cases, i.e. whenever
the crescent is visible its width at some angle y m must vanish as the crescent is never seen a complete 1800 in length. Thus at ψ = ψm
(4.6)
Therefore in (4.6) y m is a measure of half the length of the crescent so that the
total length of the crescent is given by:
(4.7)
Thus the crescent length can be
evaluated whenever the theoretical width Wc exceeds the minimum width Wm visible according
to Yallop’s q-value criterion for the particular values of ARCV.
In the Fig. 5 the segment ED or AC is the minimum width Wm at any ARCV invisible according to Yallop’s criterion. The
segment AB is the theoretical width Wc at the
center of the crescent given by (2.5) or (2.5a). At angular
separation y m from the center of crescent ED equals
.
Therefore, the points on the outer limb of the crescent that has
angular separation from center greater than
should
not be visible. The visible crescent then extends from D to D’
and has length 2y m .
One should note that whenever Wm (minimum
visible width according to Yallop’s criterion) is greater than Wc (theoretical width) (4.6) can not be used
and the crescent is not visible, i.e. it has no length.
Fig. 5
The model developed in this work
to compute the length of the crescent has been applied to a
number of observations reported in literature (Schaeffer, 1984,
Yallop, 1998). The results are for the crescent length against
the elongation, are presented in Fig. 6. The chart shows that
the functional relation between crescent length and the
elongation is not smooth as reported by Schaeffer on the basis
of Hapke’s model. The main reasons for this is that the crescent
length has to be affected by the Earth-Moon distance as claimed
above and the atmospheric turbulence close to horizon as claimed
by McNally and Sultan. During this work the 70 observations of
Danjon (mentioned by Schaeffer and Fatoohi et. al.) could not be
accessed, however the pictorial data of crescent length is being
generated at the Astronomical Observatory at University of
Karachi. The observed crescent length from photographic records
is given in Table 2. This includes some observations made by
others during past few years and their pictures are available
from www.icproj.org maintained by Odeh.
Fig. 6:
Crescent Lengths vrs Variations due ARCV
Table 2.
Observed & Calculated Lengths of Crescents
Observe Date |
Location |
SD |
Wc |
Wm |
Length |
Reporter |
Length |
Y |
M |
D |
Lat |
Long |
arcmin |
Cal. |
Obs |
Sultan |
McNally |
1989 |
4 |
6 |
34 |
-107.2 |
33.8 |
0.51 |
0.18 |
128 |
123 |
Schaefer |
162 |
131 |
1989 |
5 |
5 |
39.7 |
-105.5 |
33.4 |
0.25 |
0.18 |
85 |
82 |
Schaefer |
171 |
106 |
1999 |
3 |
18 |
31.95 |
35.9 |
33.3 |
0.34 |
0.18 |
116 |
110 |
Odeh |
168 |
119 |
1999 |
4 |
16 |
33.17 |
-112.0 |
31.8 |
0.40 |
0.18 |
99 |
92 |
Omer |
165 |
124 |
1999 |
10 |
10 |
31.95 |
35.9 |
30.3 |
0.41 |
0.18 |
128 |
124 |
Odeh |
165 |
125 |
2001 |
2 |
24 |
32.68 |
51.68 |
30.2 |
0.44 |
0.18 |
131 |
122 |
Rahimi |
164 |
127 |
2001 |
11 |
16 |
32.68 |
51.68 |
31.6 |
0.59 |
0.18 |
124 |
117 |
Rahimi |
159 |
135 |
2006 |
1 |
1 |
24.88 |
67.05 |
33.4 |
0.93 |
0.18 |
137 |
127 |
Qureshi |
147 |
145 |
2006 |
3 |
30 |
24.88 |
67.05 |
33.3 |
0.57 |
0.18 |
143 |
138 |
Qureshi |
160 |
134 |
2006 |
4 |
28 |
21.5 |
39.16 |
31.7 |
0.28 |
0.18 |
90 |
75 |
Anwar |
170 |
112 |
2006 |
6 |
24 |
24.88 |
67.05 |
31.7 |
0.93 |
0.18 |
157 |
154 |
Qureshi |
147 |
145 |
2006 |
5 |
28 |
24.88 |
67.05 |
31.5 |
0.69 |
0.18 |
145 |
138 |
Qureshi |
156 |
139 |
|
| 5. DISCUSSION |
The model developed in this work
for both the brightness and the length of crescent is mainly
geometric supplemented by the Yallop’s criterion for the
earliest visibility of new lunar crescent. The model provides a
simple method of calculating length of lunar crescent and takes
into account the atmospheric affects indirectly through Yallop’s
q-value criterion. Whenever Wc < Wm the crescent length is not calculated and the crescent was not
seen according to recorded observation. Whenever Yallop’s
criteria indicates requirement of optical aid (ROA = require
optical aid and MROA = may require optical aid) the calculated
crescent length was less than 100 degrees. In case of visibility
under perfect condition (VUPC) as per q-value criterion the
crescent length was more than 100 degree. In all cases of easy
visibility (EV) the calculated crescent length varied from 120
degrees (for low values of elongation) to 170 degrees (for large
values of elongation).
The model has been tested in two
ways. First, for some of the recent observations whose
photographic records are available the calculated and observed
crescent lengths are found to be in close agreement shown as in
Table 2. The calculated values are slightly greater than the
observed values. In the calculations using formula due to Sultan
the maximum diameter of Blackwell disc is taken as Wm as defined in this work (if the maximum diameter is
considered to be from 0.14 arc minutes to 0.16 arc minutes the
results obtained are much larger). The crescent lengths obtained
are much greater than the observed values in general and in one
case smaller than the observed value. In calculations using the
formula of McNally ΔR = Wm and R = semi-diameter of lunar disc. The root mean square
deviation of our calculated results (2.2 degrees) from the
observed values is much smaller than those calculated using
the formula of McNally (18.05 degrees). The root mean square
deviation for the technique due to Sultan is much greater
(53.3 degrees). In case of use of our formula the error is
always positive in the sense that our results are just more
than the observations. In case of McNally’s techniques the
results are inconsistent in the sense that it has both
positive and the negative errors.
The second and indirect test of
the model is its comparison with the results of Danjon mentioned
in Fatoohi et. al. If the minimum visible width Wm for various ARCV according to Yallop’s criterion is replaced by
the minimum ever central visible width of 0.18 arc minutes that
is equivalent to ignoring the atmospheric affect for lower ARCV
then the relation between crescent length and elongation becomes
smooth as presented by Schaefer (1991). The same is shown in
Fig. 7. On the basis of the calculated lengths of crescent and
its elongation using our model the Danjon deficiency arcs are
calculated ignoring the affects of ARCV by formula given by
Danjon and that given by McNally (shown in Fig. 8 and 9
respectively). These results are in close agreement with the Fig
1 in Fatoohi et al (that is a reproduction of Danjon’s fig 2).
Fig.
7: Crescent Lengths against Elongation without variations due to
ARCV
Fig. 8: Deficiency
Arc against Elongation according to Danjon.
Fig.
9: Deficiency Arc against Elongation according to McNally.
The model for the calculation of
crescent length may be used as the earliest visibility criterion
much in the same way as Yallop’s criterion can be used. However,
our emphasis was not to develop an alternate criterion for the
same. This work was intended for a better understanding of the
geometry of the lunar crescent and to develop a method for
calculating its length. |
| ACKNOWLEDGEMENT |
1. The author is grateful to the organizers of www.icoproj.org and in particular Mr. Muhammad Shaukat Odeh
who have collected pictures of young crescents that were used
after seeking permission for calculating the crescent lengths.
2. The author specially acknowledges and express his
gratitude to the office of Dean Faculty of Science, University
of Karachi, who sponsored this research which a part of the
project entitled “Integrated Software Development for
Localized Study of Lunar Dynamics” approved and funded
by the office of the Dean. |
| REFERENCES |
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