On The Cause Of Resonant Motions Of Celestial Bodies

Resonant motions are possible only in an inhomogeneous gravitational field. That’s the reason why in the beginning of the work we elucidate the principal differences between a homogeneous and an inhomogeneous field. We show that the resonant motions in closed orbits are consequences of the kinematical extrema conditions at perihelion and/or aphelion. Resonance ratios are determined and it is shown that resonance may take place after one, two and four revolutions. Finally, in the Appendix, we propose a simple criterion for ranking of the gravitational fields.

Introduction

Natural phenomenon that rotational and orbital periods of certain solid heavenly bodies moving along closed orbits are related as the rational fractions is denominated resonance in celestial mechanics. The first researchers in resonant effects were Euler, Lagrange and Laplace, more than two centuries ago. Their work was followed by numerous authors, among whom the most significant were, at the end of the nineteenth century, Bohlin and Poincare. During the last fifty years, along with the development of the artificial satellite and orbital station techniques, interest in the resonant motions was revived (see, e.g. [1], [2], [3]).

In the work [9] the second order differential equation of the relative rotation of a body in the closed orbit around the center of gravitation was derived and a hypothesis that the corresponding angular velocity must have an extremum at perihelion as the necessary resonance condition was proposed. Numerical simulations of the relative rotations (for different shapes of the body and different eccentricities of the orbit) corroborated this assumption: in the cases of resonance, as a rule, relative angular velocities were extreme at perihelion.

Since numerical results are less convincing as a rigorous proof, here we offer an evidence that stabilized (i.e. resonant) motion in closed orbit is possible only if one of the principal axes of inertia becomes coincident with direction connecting perihelion and aphelion (line of apsides), whenever body arrives at one or at both of these points. Consequences are the following: relative angular acceleration of the body has to be zero, so that an extremum or an inflexion must be present in the relative angular velocity function at the coincident point.

Motion of the Body and Frames of Reference

Consider a body of the mass m, moving in the orbit around the dominant center of gravitation of the mass m*. (Gravitational noise is excluded). Besides orbital motion, the body revolves around the principal axis (1) of its ellipsoid of inertia and this axis stays at a right angle with the orbital plane. Thus, we restrict our analysis to the planar motion of the body, only.

Motion of the Body and Frames of Reference

Fig. 1 – Motion of the Body and Frames of Reference

As usually, the orbit is defined in the polar system of coordinates R,\psi with the center of gravitation C* as the origin. Mass center c of the body is chosen to be the origin of two moving frames of reference Cxy and C\xi\eta. The first one (the translational along the radial direction displaced polar frame) is related to the geometry of orbit. The second one is related to the geometry of mass: C\xi is directed along the principal axis (3) and C\eta – along axis (2) of the ellipsoid of inertia.

Position of the second frame with respect to the first one is defined by the angle of relative rotation \varphi = \lhd xC\xi (Fig. 1).

Homogeneous and Inhomogeneous Gravitational Fields

Distinction between a homogeneous and an inhomogeneous gravitational field has nothing to do with its real nature, of course. The difference is only conceptual, that is, it’s related to the assumed model of the field and this model has to be restricted to active part of the field – to that part which is occupied by the body.

In a homogeneous field, intensities and directions of the elementary gravitational forces acting on the body particles depend on the position of the mass center in the gravitational field only. They are not functions of the position of the particles within the body, nor of the position of the body with respect to the direction C*C (Fig. 2). All the elementary forces are parallel to this direction and their sum, the “weight” of the body, coincides with that line, regardless relative rotation of the body in the frame of reference Cxy.

Resultant of the elementary forces in a homogeneous field always passes through the mass center, so the gravitational moment with respect to that point doesn’t exist. In fact, the mass center of a body in such a field represents the center of gravity, as conceived by Archimedes some 2.5 centuries B.C.

Homogeneous Gravitational Field

Fig. 2 – Homogeneous Gravitational Field

On the other hand, if the gravitational field is inhomogeneous one, intensities and directions of the elementary forces depend on positions of the mass center in the gravitational field, on positions of the corresponding particles within the body and on relative position of the body in the “orbital” frame of reference Cxy. All these forces converge toward the gravitational center and so does their resultant. Generally, this resultant doesn’t pass through the mass center, so it has to produce the gravitational moment at that point (Fig. 3). Hence we have a very important property of the inhomogeneous field: the existence of the gravitational moment with respect to the mass center.

Inhomogeneous Gravitational Field

Fig. 3 – Inhomogeneous Gravitational Field

Another important point is the absence of the center of gravity, as we have emphasized that before [10]. “Conversion” of a homogeneous into an inhomogeneous gravitational field implies displacement of this point from the mass center C far away from the body, into the gravitational center C*. While the orbital motion of the body produces rotation of the radial direction C*C around C*, its relative rotation produces titling of the gravitational force around this direction.

GF(2): Components of Newton’s Gravitational Load and their Potential

Components of the gravitational load have the following forms in the gravitational field of the second rank (see Appendix):

for010203

In these expressions, F_0 is the gravitational force in a homogeneous field, G is the gravitational constant, while I_1, I_2, and I_3 are central principal moments of inertia of the body.

It is possible now to formulate the potential energy of this load. Clearly, it has to be an approximation, also, valid in the GF(2), only:

for04

Obviously, negative partial derivatives with respect to the related coordinates are the correspondent components of the gravitational load

for04a

Concerning the transversal component of the force, it may be obtained only indirectly, because it doesn’t perform work in motion of the body along the orbit.

Motion of the Body in an Inhomogeneous Gravitational Field

Differential equations of motion of the body in GF(2) may be written as follows

for050607

Dots over the symbols denote the first and the second derivatives of the corresponding variable with respect to time.

It is evident that in general case, if I_2 \neq I_2, relative rotation of the body affects all three components of the gravitational load, causing an appearance of the periodic forcing terms on the right-hand sides of the equations (5), (6) and (7). Although these terms have very small amplitudes (of the order \delta_2), they produce some immediate, but also, due to their long duration, some cumulative effects upon the motion of the body.

Let us enumerate some of them.

  • Taking into account that the right-hand side of the equation (6) is nonzero, the sectorial velocity is not constant in an inhomogeneous field, but “almost constant” wavy line, periodic in time (Fig. 4).

Sectorial Velocity in an Inhomogeneous Gravitational Field

Fig. 4 – Sectorial Velocity in an Inhomogeneous Gravitational Field

  • Forcing terms, appearing in (6) and (7) produce meander course of the mass center path around the corresponding Kepler’s orbit (Fig.5).

Path of the Mass Center in an Inhomogeneous Field

Fig. 5 – Path of the Mass Center in an Inhomogeneous Field

Discrepancies are negligible if the cross section of the ellipsoid of inertia with the orbital plane is an approximate circle, but if I_2 \gg I_3, they may be quite noticeable.

  • Radial coordinate and orbital angular velocity have extrema at perihelion (and aphelion, in a closed orbit), so that right-hand sides of (6) and (7) have to be equal zero there. In such a way, equations of transversal and rotational motions become zero identities at characteristic points of the orbit:

for0809

Since the gravitational force is maximal at perihelion and minimal at aphelion, it is plausible to suppose that dynamic characteristics of motion, kinetic and potential energies, must have their extrema at those points, also. It is obvious, from (4) that

for1011

Such a differentiation doesn’t follow consequentially from (8) and (9). This may be ascribed to the approximate expressions for the gravitational load and its potential, obtained in GF(2). It is more likely that only conditions (10) and (11) have to exist.

Extrema Conditions and Dispositions of the Body at Perihelion

Fig. 6 – Extrema Conditions and Dispositions of the Body at Perihelion

Regarding relative angular velocity, the form of this function at perihelion (and aphelion, in the case of closed orbit) depends on several factors. By use of the equation (7) the third derivative of \varphi with respect to time at apsides may be written in the form

for12

where

for12a

p is a parameter, e – eccentricity of the orbit, while P/A denotes perihelion/aphelion.

A close inspection of (12) shows that, depending on direction of the relative rotation, on the sign of cos2\varphi_{p/a} and on the relation

for12b

possibilities systematized in the Table 1 arise. Note that

for12c

while

for12d

Table 1. Relative Angular Velocity Function at Perihelion and Aphelion

Relative Angular Velocity Function at Perihelion and Aphelion

Possibility of the inflexion at apsides implies an asymmetrical form of the function \dot{\varphi}(t) there and, since relative and orbital motions are coupled, that fact may even indicate a kind of the orbital instability.

Resonance Condition and Resonance Ratios

As mentioned above, resonant motions are possible in the closed orbits only, and from now on we restrict our considerations to such orbits, with eccentricities 0 \le e < 1.

As shown before, the extrema conditions at perihelion and aphelion require that one of the principal axes \xi or \eta of the body becomes coincident with line of apsides AP every time when it arrives at those points. Fulfillment of this requirement during the motion results in a resonance.

At a first impulse one would try to obtain the resonance condition by mere unification of the conditions (8) and (9), or (10) and (11). But it doesn’t seem to be a wise approach. In order to come to the correct condition producing all the possible resonance ratios, it is necessary to take into account the very beginning of the resonant motion. Genesis of such a motion depends on eccentricity of the orbit and on shape of the body, mainly.

In the case of great eccentricity and, especially if I_2 \gg I_3, influence of the orbit is very strong and the (maximal) gravitational force at perihelion will, acting like a magnet, oblige the body to take the proper position and thus produce the resonant motion. So, the capture into the resonance occurs immediately or soon after the capture into the orbit of the body. This doesn’t mean that the corresponding extrema condition is to be immediately fulfilled at the opposite point of the orbit, where the influence of the gravitational force is minimal.

Quite a different situation arises when the eccentricity is small, or I_2 \approx I_3. If that is the case, once captured into the orbit, the body generally resumes chaotic rotations. During such a motion there is a chance that once, at perihelion or aphelion, one of the principal axes and direction AP become coincident. After that, the body would periodically assume the same position, having the same angular velocity and angular acceleration zero. That event represents another scenario of the capture into the resonance. Again, it is not necessary that the extrema condition is fulfilled at the opposite point of the orbit.

Let us proceed now. We take perihelion for the more probable capture point, with the remark that result would be the same if aphelion was the choice. If we represent the angle of relative rotation as \varphi = \varphi(\psi) and assume the beginning of \psi at the line C*P, the resonance condition may be expressed in the form of an integer argument function

for13

  • i indicates the capture position of the body; it may take values 0 or 1;
  • m represents the single revolution average angular velocity, depending on the capture angular velocity; it is equal to one of the numbers 0,1,2,3,…;
  • n = 0,1,2,3,… denotes n-th passage through the capture point. Actually, it has the role of an argument in this equation.

The \pm sign in (13) designates progressive/retrograde rotation.

Resonance ratio represents the relation between angles of absolute and orbital rotation after one revolution

for14

Depending on the average angular velocity, resonant motions may have orbital periods of one, two and four revolutions

for14b

The middle term of this, in two directions infinite sequence is the so cold “ideal” resonance \frac {1} {1}, related to the zero average angular velocity. It separates ratios corresponding to the retrograde and to the progressive relative rotations.

In which resonance the body is to be captured depends on many factors. The most important are

  • shape of the orbit, that is, its eccentricity,
  • shape of the body, characterized by its shape factor s = \frac {I_2 - I_3} {I_1} and
  • initial, that is, capture relative angular velocity.

There is one more point we must discuss here. Dissipative forces were neglected in the equations of motion. It was entirely justified by the fact of their smallness as well as on their insignificance regarding solution of the posed problem. However, when motions of the heavenly bodies are in question, the time measures are millennia, even eons and the work of these damping forces gradually slows down orbital and rotational motions.

The effect of the friction with the cosmic dust is an increase of radius and reduction of eccentricity [7] of the orbit, while the tidal friction slows down relative rotation of the body. All that results in numerical diminution of the resonance ratio and in approach, either from the left or from the right, to the resonance situated in the middle of the sequence. As it was the case with beginning of the resonant motion, depending on shape of the orbit, as well as on shape of the body, passage from the higher into the lower resonance may occur suddenly, or gradually – through chaotic motion.

After this digression, we may continue now. As seen above, resonant motions with one, two and four revolutions orbital periods were obtained from the resonance condition (13), which corresponds to the extrema condition (8). Regarding satisfaction of the remaining conditions (9), (10) and (11) we show Table 2, in which the signs + and – mean that the related condition is/is not satisfied.

Like the other motions, resonant motions may be more or less stable. Using stability of the ball in a spherical cavity metaphor, it is possible to speak of the “shallow” and the “deep” resonance [1]. Capture into and escape from a shallow resonance should have to be relatively easy and so should have to be capture into a deep one. On the other hand, escape from a deep resonance should have to require a great amount of the energy consumption.

If one adopts the number of the fulfilled extrema conditions as a kind of the resonant motions stability criterion, one will reach to the expected outcome that the four – cycles resonant motions with the “wrong” capture position (\varphi_P = \frac {\pi} {2}) have the least stability: excepting this capture position, none of the other conditions is to be satisfied during such motions.

And now comes a somewhat surprising result: not the single – cycle, but the two – cycles resonant motions with “correct” capture position (\varphi_P = 0) satisfy all four extrema conditions. On the contrary, it is impossible that during the single–cycle resonant motions the energy extrema conditions were fulfilled at both characteristic points of the orbit.

Table 2. Resonant Motions: Fulfillment of the Extrema Conditions

Resonant Motions: Fulfillment of the Extrema Conditions

This result is possibly an explanation of the Mercury’s resonance. Rotational axis of this planet is almost perpendicular to the orbital plane and our model roughly corresponds to Mercury motion. For almost a hundred years it was considered that Mercury moves around Sun in the “ideal” \frac {1} {1} resonance. Subsequently, however, some forty years ago, it was established that its resonance ratio is, actually, \frac {3} {2}. From the standpoint of the here proposed criterion, if the capture position of this celestial body was correct, motion in \frac {3} {2} is more stable than motion in \frac {1} {1} resonance. Taking into consideration the outstanding eccentricity of its orbit (e = 0.206), chance that Mercury might escape the present and become captured into the “ideal” resonance appears insignificant. In general, \frac {1} {1} resonance is neither more nor less stable than any other single – cycle resonance.

It seems that the passage into the ideal resonance and the change in the shape of the orbit have to go together. As already mentioned, due to the continuous kinetic energy degradation, eccentricity of the orbit decreases and consequently, the orbital motion becomes uniform. Simultaneously, the relative rotation slows down and when it stops, in accordance with the minimal potential energy principle, the body assumes the stable position \varphi = 0, pointing its principal axis of the minimal moment of inertia toward the center of gravitation. This resonance \frac {1} {1} is the final one and, in our opinion, the term ideal should have to be reserved for such a motion only: uniform motion in a circular orbit, relative angular velocity – zero and position of the body – stable.

Earth’s Moon, as well as the numerous satellites orbiting around the other solar system planets, moves, approximately, in such a resonance.

Conclusion

It is not possible to speak about resonant motions in a gravitational field if an inhomogeneous field as a model for this field was not adopted.

Hence, in the beginning of this work the principal features of an inhomogeneous gravitational field were emphasized and after that, components of the gravitational load and their potential in such a field were given. Being the forcing terms in the differential equations of motions, these components produce appreciable dissimilarities between motions in a homogeneous and in an inhomogeneous gravitational field.

One of the most important differences is that an inhomogeneous field forces the body moving in a closed and stable orbit to revolve in resonance. We have shown in this work that fulfillment of the kinematical quantities extrema condition in perihelion and/or aphelion requires that one of the body’s principal axes of inertia coincides with the line of apsides whenever body arrives at one, or both these points. The result is a stable, that is, resonant motion.

We have also determined a sequence of the resonance ratios. It was shown that resonant motions may have orbital periods of one, two and four revolutions. An interesting conclusion is that generally, when eccentricity of the orbit differs from zero and the cross section of the ellipsoid of inertia with the orbital plane differs from circle, the two – cycles resonance is the most stable one.

Appendix

Ranking of the Gravitational Fields

Acording to the Figure 3, Newton’s gravitational force acting on the body in an unhomogeneous field may be represented in the form

for15

where \vec{r}(-R-x, -y) denotes position of the center of gravitation with respect to the body’s elementary mass.

The need for ranking of the fields follows from the fact that it is not possible to express this integral in finite form, by use of the elementary functions. Instead, it may be represented as the infinite functional series, only

for16

We propose the following form of the series representing components of this force

A1A2

In these expressions,

for17

and G is the gravitational constant.

Terms of the series are products of the dimensionless functions \bar{X_k} and \bar{Y_k} with the functional parameters \delta_k. Functions \bar{X_k} and \bar{Y_k} depend on the geometry of mass of the body, as well as on its relative rotation. The mass distribution is characterized by the moments of mass M_{ik} (i = 1,2,3) of the order k with respect to the adopted frame of reference. It’s convenient to take that the moments of the zero order determine mass of the body: M_{i0} = m, while the first moments define position of the center of mass C. Since this point was chosen to be the origin of our frames of reference, it’s obvious that these moments have to be zeros, identically: M_{i1} = 0 (i = 1,2,3).

The second moments M_{i2} are moments of inertia, of course. In the frame \xi\eta\zeta those are the principal moments: M_{i2} = I_i (i=1,2,3).

Moments of mass of the higher order must have their meanings, also, but their definitions are not established, yet. Arguments S_k, denominated the shape factors in the work [9] may be defined in the following form

A3

 

Regarding parameters \delta_k, they may be represented as relations

A4

Obviously, \delta_0 = 1, while \delta_1 = 0. The other parameters are, as a rule, very small numbers in celestial mechanics, situated in the interval

A5

Note that min R = C*P (P – perihelion), while max R = \infty, for an open orbit and max R = C*A (A – aphelion), in the case of the closed one. As an illustration, for Earth in the gravitational field of Sun (considering small eccentricity of its orbit) one may adopt
that O(\delta_2) = 10^9. An effect of smallness of these parameters is a fast convergence of the sums of series toward the exact solutions.

Convenience of the forms (A1) and (A2) becomes evident. Parameters \delta_k in both expressions indicate terms of the comparable order, so that we may safely truncate series in these equations now and use the sums of the finite series as the approximate values of the force components. The term after which the series are to be truncated may be used as a criterion for ranking of the gravitational fields. The rule is quite simple:

  • rank of the field is K if the components of the gravitational force are approximated by the finite series with K terms. Such a field may be denominated GF(K).

If we put \bar{X_0} = -1 and \bar{Y_0} = 0 in (A1) and (A2) we shall get

X =F_0, Y = 0 and M^C = -RY = 0.

According to the given criterion, as well as to what was said about homogeneous and inhomogeneous fields, the GF(0) is obviously a homogeneous field. Since \delta_1 \equiv 0, GF(1) would be a homogeneous field, also. Actually, GF(1) \equiv GF(0).

All the other fields are inhomogeneous. If we take into account one more term, we “enter” into the GF(2) which has all the characteristics of an inhomogeneous field.

Here follow the components of the gravitational force in that field, written in the form (A1), (A2):

A6A7

and the gravitational moment with respect to the mass center is, of course

A8

Clearly,

a9

the shape factor corresponds to that one, obtained in the work [9] S_2 = \frac {I_2 - I_3} {I_1}, while the parameter \delta_2 = \frac {I_1} {mR^2}.

And that is all we have at this moment:

  • GF(0) = GF(1) – homogeneous gravitational field and
  • GF(2) – inhomogeneous gravitational field.

Gravitational fields of the higher rank will have to wait until definitions of the moments of mass of the higher order were established.

References

[1] B. Garfinkel: 1982, Celes. Mech., 28, pp. 275 – 290.
[2] R. Sergysels: 1989, Celes. Mech., 44, 155.
[3] R. A. Howland : 1989, Celes. Mech., 44, 209.
[4] R. V. de Moraes& P.A.F. da Silva: 1990, Celes. Mech., 47, 225.
[5] V. V. Beletskii: 1974, Resonance Phenomena at Rotations of Artificial and Natural Celestial Bodies, G. E.O. Giacaglia, Springer Verlag, Berlin, pp. 192 – 232.
[6] S. Hawking, W. Israel: 1989, 300 Years of Gravitation, Cambridge University Press.
[7] L. A. Pars: 1956, A Treatise of Analytical Dynamics, Heinemann, London.
[8] R. G. Strom: 1987, Mercury, Smitsonian Institution Press, London.
[9] M. Marjanov: 1997, Gravitational Resonances, Bull. Astron., Belgrade, 156, 9 – 19.
[10] M. Marjanov: 2001, Inhomogeneous Gravitational Field and the Body without Center of Gravity, XXIII JUMEH Congress, Belgrade.

O uzroku rezonantnih kretanja nebeskih tela. Fenomen gravitacionerezonance može se ispoljiti samo u nehomogenom gravitacionom polju. Stoga su na početku rada istaknute osnovne razlike između homogenog i nehomogenog polja. Izvedene su komponente gravitacionog opterećenja i njegov potencijal pri ravnom kretanju u nehomogenom polju. Pokazano je da su rezonantna kretanja (u zatvorenim orbitama) posledice postojanjaekstremuma kinematičkih i dinamičkih atributa kretanja u apsidama. Dat je beskrajni niz rezonantnih brojeva, to jest, razlomaka čiji su imenioci jedan, dva ili četiri. Naime, pokazalo se da su to brojevi orbitalnih revolucija u kojima se može uspostaviti rezonanca s rotacionim kretanjem. U prilogu je prikazan jednostavan kriterijum za razvrstavanje gravitacionih polja koji je korišćen u ovome radu.

Ključne reči: homogeno i nehomogeno gravitaciono polje, rezonanca, rezonantni broj

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