PRECESSION

AND

 THE OBLIQUITY OF THE ECLIPTIC

- Part One -

Haluk Akcam

Jan. 01, 2004

             

Summary

          

First, the expressions for the precession quantities since IAU 1976 resolutions are overviewed, compared, and their validity ranges are determined. Then, a long-term definition is proposed to work with the temporal search area round J2000 ± 100,000 years, for astrological purposes. Although the intend of this article is to seek reliable formulations for astrological researches, the scientific base of introduced expressions are strictly in accordance with recent astronomical concepts, and therefore may be safely used for astronomical computations for the given period.

            

Classical Definitions

              

In general, the term precession is used for the slow, periodic conical motion of the rotation axis of a spinning body. It is the uniformly progressing motion of  the pole rotation of a free rotating body undergoing torque from external gravitational forces. In the case of Earth, it is the slow gyration of the Earth's axis. The component of precession caused by the Sun and Moon acting on the Earth's equatorial bulge is called lunisolar precession, and the component caused by the action of the planets is called planetary precession. The sum of lunisolar and planetary precession is then called general precession.

Earth's axis of rotation is not perpendicular to the ecliptic but inclined about 23.5°, and thus affected by gravitational perturbations from other bodies in the solar system. The Sun and Moon pull harder on the nearest part of the Earth's equatorial bulge than the farthest part, and this causes a torque which precesses the Earth's rotational axis. This gravitational pull - mainly by the Sun and Moon on the Earth's equatorial bulge - causes the first point of Aries to move backward along the equator at about 50" per year, which produces the round 26,000 year canonical motion of the Earth's rotation axis.

While precessing, the Earth's axis wobbles due to the minutely greater gravitational effect of the Moon on the Earth's equatorial bulge, which is called nutation. It is a slight but recurrent oscillation of the axis of the Earth, due to lunar perturbations, and produces a small, irregular oscillation in the precessional motion of the Earth's rotational axis.

In general, obliquity is the angle between the equatorial and orbital planes of a body, which can be defined as the angular distance between the rotational and orbital poles. In the case of Earth, obliquity of the ecliptic is the angle between the planes of the equator and the ecliptic, and due to above summarized effects, the axial tilt of the Earth oscillates between round 22.0°-24.6°, with a period of round 41,000 years.

Further, the term eccentricity is applied for the extent to which an elliptical orbit departs from a circular one. It is the parameter that specifies the shape of a conic section. The eccentricity of an elliptical orbit is the amount by which the orbit deviates form circularity, as e=c/a, where c is the distance from the center to a focus, and a is the semimajor axis. The eccentricity of Earth's orbit also fluctuates with a cyclic period of about roughly 100,000 years, which is practically close to the minimum of its cycle at present. In connection with the precession quantities, these orbital parameters as well as the other four will be subject to some definitions, here in this article. Although the context of this article is simplified for the benefit of the laymen, the reader is expected to be aided at least with the basics of celestial dynamics.

                       

I - Expressions for Short-Interval Precession Quantities

                  

Since the definition of Simon Newcomb [1], in regard to the precise expression of the speed of general precession in longitude, remarkable progress has been achieved in one century. Some of the historical monuments are the works of Androyer, de Sitte, Brouwer, Woolard, Clemence, Lieske, and Fricke. Here, the expressions of Lieske (L77), which are adopted by the IAU (1976) General Assembly, are taken as the first sample of a series of its kind until the end of 2003. As a reminder, Saturn has almost completed one orbital period since that time.

Expressions, which do not include time series are not taken into account. Being a historical one, Newcomb's general precession value was p = 5025.64 arcseconds per tropical century at 1900.0.

Table 1.1 - Numerical Expressions for the General Accumulated Precession  pA

  t1 t2 t3 t4 t5 t6 t7 t8 t9 t10
L77 5029.0966 +1.11113 -6×10-6              
B81 5029.0966 +1.11370 +76×10-6              
La86 5029.0966 +1.111971 +7732×10-8 -235316×10-10 -18055×10-12 +17451×10-14 +13095×10-16 +2424×10-18 -4759×10-20 -866×10-22
B88 5029.0966 +1.111971 +7732×10-8 -235316×10-10 -18055×10-12 +17451×10-14        
S94 5028.8200 +1.112022 +773×10-7 -2353×10-8 -18×10-9 +2×10-10        
W94 5028.7700 +1.105407 +76×10-6 -24×10-6            
B97 5028.7700 +1.1124285 +7709×10-8 -23465×10-9 +182×10-10          
B98 5028.7700 +1.112433483 +77003×10-9 -234793×10-10 -17831×10-12          
IAU 5028.79695 +1.11113 -6×10-6              
B03 5028.792262 +1.1124406 +7699×10-8 -23479×10-9 -178×10-10 +18×10-11 +1×10-12      
F03i 5028.795765904 +1.105389809 -21763×10-9 +2×10-8 -5×10-9          
F03r 5028.795492447 +1.105410150 -21741×10-9 +128997×10-9 +3×10-9 -234×10-9        
C03 5028.796195 +1.1054348 +7964×10-8 -23857×10-9 -383×10-10          

            

Above expressions since Lieske are coded here for further reference, according to the leading scientist of the related paper and date of issue, which are: Lieske L77 [2], Bretagnon B81 [3], Laskar La86 [4], Bretagnon B88 [5], Simon S94 [6], Willams W94 [7], Bretagnon B97 [8][N1], Bretagnon B98 [9], IAU2000 IAU [10][N2], Bretagnon B03 [11], Fukushima F03i [12][N2], Fukushima F03r [12][N3], and Capitaine C03 [13]. Reader is referred to the issued papers for details on the corresponding model. [N4]

Cells colored with pink are denoting coefficients, which deviates from the median of its kind.  

Expressions are in arcseconds, and t is measured in Julian centuries of 36525 days as t = ( T - 2000 ) / 100, where T is the Julian date of the epoch. To compare the above thirteen expressions, accumulated precession figures may not be appropriate for the purpose. Therefore,  the first order derivatives of the polynomials are taken, and the graph below is accordingly:

Graph 1.1 - General Precession Rate According to Thirteen Models

precession rates

Ordinates are for the general precession rate in arcseconds per Julian year for the epoch, and the abscissae are for the epoch, each gray grid unit representing 1000 Julian years.

A quick glance at the table and the graph reveals that these thirteen models can be grouped in three structural categories:

  • Quasi-Linear Types: L77, B81, IAU, F03i

  • Classical Types:       La86, B88, S94, W94, B97, B98, B03, C03

  • Unusual Types:        F03r

A detailed examination of the interval J2000 ±3000 by applying these expressions give much clue about the similarities, which may help to define more clear classifications.

  • Similarities between L77 and IAU are obvious, for the latter is the modification of the former, simply by subtracting the proposed Dp value of MHB2000. Second and third terms of the polynomials are exactly the same [N1]. On the other hand, although the structure of B81 seems quite similar to L77, it emerges from an original work, which is the basis of the rotation matrix of VSOP82 by Bretagnon, and therefore cannot be regarded as a member to the same group. Finally, although a peculiar one, F03i is a unique sample of its kind, and must be handled apart from the others.

  • Among classical types, W94 and C03 are constituting a couple, C03 being the improved version of the theoretical W94, mainly by the aid of new VLBI and LLR results. But, the success of C03 is questionable. Therefore, this couple is slightly different than the next six models.

  • Evidently, La86, B88, S94, B98, and B03 are the successive improvements of the same model: B88, as a part of VSOP87, is a copy of La86 up to 6th power. S94 is also a rounded copy of La86, just with a new Dp application computed by Williams et al.(1991). B98, as the base of SMART97, is the revision of the formers. Finally, B03 is the modified version of B98. Yet, B97 in the original paper [8: p.316, tb.4] may possibly suffer a notation error with the 5th term's sign. In that case, it proves to be the successor of B88 or S94, and predecessor of B98. If there is no notation error, B97 is almost similar to B98 and B03, and quite similar to La86, B88, and S94. In any case, all these six expression variations seem to be from the same atelier. Although a relative primitive one, B81 can be placed at the beginning of these six successors.

  • The case with F03r is rather striking. The theory behind may be useful for further developments, but the model itself seems insufficient with the present status.

A comparison of thirteen polynomials in figures for the interval J2000±500 is given as a separate table.

Although these thirteen models are designed to produce accurate figures valid only for a few centuries, we will search for the incorporated arguments by scrutinizing critical areas of these models. For this purpose, the quasi-linear types are discarded due to incongruity. The classical types are found worthy to analyze. The unusual type F03r will be also included, but handled with care, since the model may be partly incomplete.

Assuming that a fictitious sinus curve may serve as a prototype for the definition of general precession rate in time, with a certain amplitude and period, the primary asymptotic points of these polynomials may be taken into consideration. The table below is showing the results from second order derivatives of the polynomials: (figures are truncated!)

Table 1.2 - Critical Points of Nine Precession Curves

  Minimum Maximum  

Period

P

Amplitude

ap

Init.Epoch

t0

 

Mean

p0

Error

Dp0

Int.Const.

tc

 

Precession

Cycle (jy)

Operative

Interval

T1 pmin T2 pmax
La86 -8346.280 48.873090 11683.030 51.672820 40058.619 1.399865 1668.375 50.272955 +0.055681 1822.345 25779.269 -11221 to 14558 
B88 -9015.050 48.824715 11133.227 51.628111 40296.553 1.401698 1059.088 50.226413 +0.143719 1820.258 25803.157 -11842 to 13961
S94 -9741.497 48.793497 11262.697 51.635744 42008.387 1.421124 760.600 50.214620 +0.199945 1809.119 25809.216 -12144 to 13665
W94 -6682.719 49.013704 10841.052 51.596702 35047.543 1.291499 2079.167 50.305203 -0.000000 1856.809 25762.743 -10802 to 14961
B97 -6370.071 49.036732 11591.415 51.691755 35922.971 1.327512 2610.672 50.364244 -0.059196 1849.444 25732.542 -10256 to 15477
B98 -7372.872 48.927174 10517.154 51.572227 35780.052 1.322526 1572.141 50.249701 +0.057078 1850.061 25791.198 -11323 to 14468
B03 -7634.695 48.895346 12249.965 51.686451 39769.321 1.395552 2307.635 50.290899 -0.065464 1824.166 25770.070 -10577 to 15193
Mean -7880.455 48.909180 11325.506 51.640544 38411.921 1.365682 1722.525 50.274862 +0.047395 1833.172 25778.313 -11167 to 14612
C03 -8190.038 48.863134 10040.990 51.504969 36462.055 1.320918 925.476 50.184052 +0.132219 1847.050 25824.937 -11987 to 13838

Mean

-7919.153 48.903424 11164.941 51.623597 38168.188 1.360087 1622.894 50.263511 +0.057998 1834.907 25784.141 -11269 to 14515
F03r -612.395 49.788862 4611.280 50.786298 10447.349 0.498718 1999.442 50.287580 -0.000252 1983.510 25771.771 -10886 to 14885

The abscissa interval of two asymptotic points gives the half period (P/2), and the ordinate interval of the same points gives the double amplitude (2×a). Again the arithmetic mean of abscissa components gives the initial epoch t0, and the arithmetic mean of ordinate components gives the annual precession rate p0 for the initial epoch. Error Dp0 at the initial epoch for p0 is computed by applying the derivative of the polynomials. Integral constant tc is computed for J2000 by comparing to original polynomials. From these mean values, the prototype of the sinusoidal to define the general precession rate pt for the epoch t can be written approximately as:

pt = p0 - Dp0 cos g + ap sin g    where    g = 2 p ( t - t0 ) / P    and    t in Julian years.

It is obvious that the pt curve fits exactly to the original one at the critical points, but deviates slightly elsewhere. Below is the centennial error check ( value = prototype - original ) for the interval J2000±500, in which the original curve is expected to be most reliable:

Table 1.3 - Deviation of the Prototype Curve for General Precession Rate (in seconds of arc)

  J1500 J1600 J1700 J1800 J1900 J2000 J2100 J2200 J2300 J2400 J2500
La86 +0.000384 +0.000159 -0.000075 -0.000319 -0.000572 -0.000835 -0.001106 -0.001386 -0.001674 -0.001970 -0.002274
B88 -0.000621 -0.000820 -0.001039 -0.001280 -0.001540 -0.001821 -0.002122 -0.002442 -0.002782 -0.003140 -0.003517
S94 -0.004431 -0.005134 -0.005859 -0.006606 -0.007374 -0.008162 -0.008969 -0.009795 -0.010638 -0.011497 -0.012373
W94 -0.005989 -0.004969 -0.003941 -0.002907 -0.001868 -0.000826 +0.000217 +0.001260 +0.002301 +0.003339 +0.004371
B97 -0.010576 -0.009735 -0.008867 -0.007975 -0.007059 -0.006121 -0.005162 -0.004184 -0.003189 -0.002177 -0.001151
B98 -0.000758 +0.000291 +0.001329 +0.002354 +0.003364 +0.004358 +0.005334 +0.006291 +0.007227 +0.008142 +0.009032
B03 +0.001389 +0.001232 +0.001070 +0.000904 +0.000734 +0.000560 +0.000382 +0.000200 +0.000014 -0.000175 -0.000368
C03 +0.005445 +0.006290 +0.007102 +0.007878 +0.008618 +0.009321 +0.009986 +0.010611 +0.011196 +0.011739 +0.012241
F03r -0.036535 -0.030030 -0.022990 -0.015542 -0.007818 +0.000044 +0.007906 +0.015629 +0.023076 +0.030114 +0.036617

As it is seen above, the error margins are quite satisfactory for a simple sinusoidal to substitute the polynomial for remote dates. Only F03r is an exception, yet it is not considered as a master for the prototype. The prototype with the mean parameters (Table 1.2) gives p = 50.2900027 for J2000, and when compared with the IAU proposal (50.2879695), the error is +0.0020332 arcseconds, which is acceptable with the present status of the prototype. The same prototype with the mean values of seven reliable models gives p = 50.2894799 for J2000 ( error = + 0.0015104).

It is possible to integrate pt for ( t - t0 ), to compare it to the original expressions. But, the significant period and the amplitude of the curve urge us to examine the polynomials for the obliquity of the ecliptic, before trying to improve the prototype. Examination of epsilon curves shows that model C03 must be also excluded next to F03 variants. In the end, we have only seven reliable models, and the above prototype can be integrated accordingly to compute the accumulated precession for remote dates as:

pA = p0 ( t - tc ) - ( P / 2 p ) ( Dp0 sin g + ap cos g )    where    g = 2 p ( t - t0 ) / P    and    t in Julian years.

The constants are mean values of the first seven models from Table 1.2, and the equation is to be considered as the preliminary version. Below is the centennial error check ( value = prototype - original ) for the interval J2000±500:

Table 1.4 - Deviation of the Prototype Curve for General Accumulated Precession (in seconds of arc)

  J1500 J1600 J1700 J1800 J1900 J2000 J2100 J2200 J2300 J2400 J2500
La86 +0.102901 +0.130155 +0.134441 +0.114800 +0.070293 0 -0.096977 -0.221511 -0.374451 -0.556614 -0.768789
B88 +0.589182 +0.517293 +0.424501 +0.308723 +0.167900 0 -0.196982 -0.425017 -0.686047 -0.981972 -1.314658
S94 +3.126105 +2.648024 +2.098543 +1.475453 +0.776623 0 -0.856384 -1.794413 -2.815885 -3.922506 -5.115889
W94 +1.709617 +1.161594 +0.715986 +0.373511 +0.134721 0 -0.030434 +0.043468 +0.221587 +0.503636 +0.889160
B97 +4.199532 +3.183750 +2.253416 +1.411088 +0.659189 0 -0.564339 -1.031836 -1.400648 -1.669083 -1.835605
B98 -0.914274 -0.937520 -0.856417 -0.672185 -0.386200 0 +0.484725 +1.066132 +1.742225 +2.510863 +3.369760
B03 -0.491694 -0.360634 -0.245506 -0.146741 -0.064767 0 +0.047151 +0.076292 +0.087043 +0.079040 +0.051939
C03 -3.728646 -3.141611 -2.471727 -1.722437 -0.897302 0 +0.965683 +1.995855 +3.086528 +4.233619 +5.432960
F03r +9.476581 +6.143405 +3.488487 +1.559039 +0.389297 0 +0.398083 +1.576569 +3.514677 +6.178130 +9.519677

As it is seen above, the error margins are quite satisfactory for a simple sinusoidal to substitute the polynomial for accumulated precession figures. F03r is an exception, yet it is not considered as a master for the prototype. S94, B97, and C03 are showing relatively rapid deviations, and need to be reconsidered. But, B03 is showing a perfect match, as well as La86. The rest; B88, W94, and B98 are not presenting huge deviations, yet supporting the prototype with less accuracy.   

          

II - Expressions for Short-Interval Obliquity Quantities

            

Obliquity of the ecliptic was given as 23°27'08.26" for J1900.0, with the expressions of Newcomb:

e = 23.452294 - 0.0130125 T - 0.00000164 T2 + 0.000000503 T3

But, after reconsidering ancient and medieval measurements, as well as those of the recent ones, Newcomb's expressions became questionable, particularly in the late fifties. After two decades, IAU adopted the expressions of Lieske in 1976. The table below is listing the major contributions since then, until the end of 2003, in conformity with Table 1.1:

Table 2.1 - Numerical Expressions for the Obliquity of the Ecliptic  eA

  t0 t1 t2 t3 t4 t5 t6 t7 t8 t9 t10
L77 84381.448 -46.8150 -59×10-5 +1813×10-6              
B81 84381.448 -46.8093 -15×10-5 +2001×10-6              
La86 84381.448 -46.8093 -155×10-6 +199925×10-8 -5138×10-10 -24967×10-12 -3905×10-14 +712×10-16 +2787×10-18 +579×10-20 +245×10-22
B88 84381.448 -46.8093 -155×10-6 +199925×10-8 -5138×10-10 -24967×10-12 -3905×10-14        
S94 84381.412 -46.80927 -152×10-6 +19989×10-7 -51×10-8 -25×10-9          
W94 84381.409 -46.833960 -174×10-6 +2×10-3 -1×10-6            
B97 84381.412 -46.836057 -1664×10-7 +199906×10-8 -512×10-9 -259×10-10          
B98 84381.409 -46.836051020 -167238×10-9 +1999114×10-9 -5225×10-10 -24845×10-12          
IAU 84381.448 -46.84024 -59×10-5 +1813×10-6              
B03 84381.4088 -46.836051 -1667×10-7 +199911×10-8 -523×10-9 -248×10-10 -3×10-11        
F03i 84381.40621 -46.83460 -17×10-5 +2×10-3              
F03r 84381.409550617 -46.835355633 -170419×10-9 +2000054×10-9              
C03 84381.406 -46.836769 -1831×10-7 +20034×10-7 -576×10-9 -434×10-10          

Cells colored with pink are denoting coefficients, which deviates from the median of its kind.  

Graph 2.1 - Obliquity of the Ecliptic According to Thirteen Models

obliquity of the ecliptic

Graph for the obliquity of the ecliptic as proposed polynomials by thirteen sources is depicted above. The legends are similar to those of the previous graph (G1.1). Here the expression similarities are so close that it is almost impossible to discriminate the epsilon curves of B81, F03i, and F03r, as well as of S94 and B98. But, the similarity of IAU and L77 curves is not a surprise. The only problem, which cannot be understood easily, is the quasi-linearity of C03, in respect to others [N5]. A comparison of thirteen polynomials in figures for the interval J2000±500 is given as a separate table.

Applying the same method like before, critical points of the curves are computed by getting the first order derivatives, and tabulated here with truncated figures:

Table 2.2 - Critical Points of Twelve Epsilon Curves

  Maximum Minimum  

Period (jy)

Amplitude

ae

Init.Epoch

t0

 

Mean

e0

Error

De0

T2 emax T2 emin
La86 -7530.853 87246.833382 12032.440 81401.307366 39126.585 2922.763008 2250.794 84324.070374 59.986539
B88 -7412.099 87235.793369 12777.147 81343.986983 40378.491 2945.903193 2682.524 84289.890176 227.299888
S94 -7642.645 87265.798404 12223.222 81395.292549 39731.734 2935.252927 2290.289 84330.545477 84.967959
W94 -6589.629 87081.035864 11119.523 81556.625850 35418.305 2762.205007 2264.947 84318.830857 61.471118
B97 -7696.220 87275.541440 12309.857 81382.078660 40012.155 2946.731390 2306.818 84328.810050 91.043562
B98 -7630.439 87265.677162 12221.944 81392.986500 39704.766 2936.345331 2295.753 84329.331831 86.391552
B03 -7451.689 87242.687130 12608.172 81355.421632 40119.722 2943.632749 2578.242 84299.054381 188.090976
Mean -7421.939 87230.480964 12184.615 81403.957077 39213.108 2913.261944 2381.338 84317.219021 114.178799
L77 -7266.702 87271.896865 11288.397 81480.842535 37110.198 2895.527165 2010.848 84376.369700 0
B81 -6827.933 87135.920644 10832.930 81624.636061 35321.725 2755.642291 2002.499 84380.278352 0
IAU -7269.203 87274.236096 11290.898 81478.497828 37120.201 2897.869134 2010.848 84376.366962 0
F03i -6832.192 87138.645399 10837.859 81621.513060 35340.102 2758.566170 2002.833 84380.079230 0
F03r -6832.137 87138.675006 10837.818 81621.483622 35339.910 2758.595692 2002.840 84380.079314 0
Mean -7248.478 87214.395063 11698.351 81471.222720 37893.658 2871.586171 2224.936 84342.808892 66.604300

Calculation method is the same of Table 1.2. From these mean values, the prototype of the sinusoidal to define the obliquity of the ecliptic et for the epoch t can be written approximately as:

et = e0 - De0 cos g - ae sin g    where    g = 2 p ( t - t0 ) / P    and    t in Julian years.

It is obvious that the et curve fits exactly to the original one at the critical points, but deviates slightly elsewhere. Below is the centennial error check ( value = prototype - original ) for the interval J2000±500, in which the original curve is expected to be most reliable:

Table 2.3 - Deviation of the Prototype Curve for Obliquity of the Ecliptic (in seconds of arc)

  J1500 J1600 J1700 J1800 J1900 J2000 J2100 J2200 J2300 J2400 J2500

La86

+0.814471

+0.753998

+0.678644

+0.588460

+0.483512

+0.363885

+0.229679

+0.081011

-0.081988

-0.259168

-0.450365

B88

-9.793283

-8.857501

-7.938689

-7.037773

-6.155664

-5.293255

-4.451422

-3.631025

-2.832904

-2.057882

-1.306765

S94

-3.080958

-2.652020

-2.233588

-1.826095

-1.429963

-1.045595

-0.673381

-0.313695

+0.033104

+0.366673

+0.686684

W94

+16.286017

+14.250991

+12.181416

+10.080574

+7.951793

+5.798441

+3.623921

+1.431667

-0.774861

-2.992180

-5.216795

B97

-4.500011

-3.903254

-3.316295

-2.739764

-2.174280

-1.620446

-1.078850

-0.550063

-0.034643

+0.466870

+0.953951

B98

-2.924845

-2.516636

-2.119337

-1.733359

-1.359095

-0.996924

-0.647209

-0.310297

+0.013480

+0.323808

+0.620387

B03

-6.980220

-6.243646

-5.523275

-4.819835

-4.134038

-3.466577

-2.818130

-2.189358

-1.580901

-0.993385

-0.427417

L77

+11.217024

+9.041244

+6.852465

+4.653836

+2.448519

+0.239683

-1.969498

-4.175848

-6.376197

-8.567381

-10.746247

B81

+11.027639

+8.854295

+6.666899

+4.468924

+2.263860

+0.055205

-2.153539

-4.358866

-6.557277

-8.745285

-10.919413

IAU

+11.223109

+9.046138

+6.856168

+4.656348

+2.449840

+0.239812

-1.970560

-4.178102

-6.379642

-8.572017

-10.752074

F03i

+11.040925

+8.866422

+6.677862

+4.478717

+2.272474

+0.062630

-2.147313

-4.353853

-6.553494

-8.742746

-10.918139

F03r

+11.041252

+8.866715

+6.678121

+4.478941

+2.272663

+0.062784

-2.147195

-4.353771

-6.553447

-8.742736

-10.918164

With the epsilon curve, the error margins are not very satisfactory even if it is a simple sinusoidal to substitute the polynomial for remote dates. The prototype with the mean parameters (Table 2.2) gives e = 84383.327 for J2000, and when compared with the old value kept by the IAU (84381.448), the error is +1.879 arcseconds, which is not quite acceptable even with the present status of the prototype. Yet, with the mean of seven reliable models, the value that the prototype gives is e = 84381.150 for J2000, and the error becomes -0.298 arcsec.

           

III - Congruence of Precession & Obliquity Expressions

         

The discord between the two prototypes is caused by the inconsistency of the master models. The maximal and minimal points of two curves are expected to fit respectively, on the horizontal axis. Namely, when the obliquity reaches its maximal/minimal value, the precession rate at the corresponding epoch is expected to reach its minimal/maximal value. Since the annual amount of the precession is inversely related to the obliqueness of the ecliptic plane, the derivatives of the two polynomials are expected to join at least at two abscissa points, when the ordinates are reduced to zero. But, this special case is not possible with any of these polynomial couples. Yet, we may consider the corresponding roots of the differential equation:

pA" = eA'

which is expected to give the approximated T1 and T2 values of mutual asymptotic points of both curves. In a similar way, a further differentiation: