As an astronomical field of study, celestial mechanics includes the sub-fields of orbital mechanics, which deals with the launching and orbitsartificial satellites, and lunar theory, a specialty which deals with the complications of the orbit of the Moon. Modern celestial mechanics tends to divide between five broad fields of study:
trajectories of artificial satellites (astrodynamics)
motions of major planets, minor planets, and natural satellites in
the Solar system and other stellar systems and widely spaced
multiple-star systems (planetary dynamics)
the motion of component stars and their planetary systems in closely
spaced multiple-star systems and globular clusters (astrodynamics and stellar dynamics)
flow of stars within and among the bodies of large galaxies, dwarf galaxies, and globular clusters (stellar dynamics and galactic dynamics)
All of the above fields overlap, but are sometimes treated as separate, especially the study of the motion of stars within galaxies and interactions between whole galaxies, which both tend to rely heavily on fluid mechanics (whole stars being particles of the “fluid”).
Modern analytic celestial mechanics started with Isaac Newton's Principia
of 1687. The name "celestial mechanics" is more recent than that.
Newton wrote that the field should be called "rational mechanics." The
term "dynamics" came in a little later with Gottfried Leibniz, and over a century after Newton, Pierre-Simon Laplace
introduced the term "celestial mechanics." Prior to Kepler there was
little connection between exact, quantitative prediction of planetary
positions, using geometrical or arithmetical techniques, and contemporary discussions of the physical causes of the planets' motion.
Isaac Newton (25 December 1642–31 March 1727) is credited with introducing the idea that the motion of objects in the heavens, such as planets, the Sun, and the Moon, and the motion of objects on the ground, like cannon balls and falling apples, could be described by the same set of physical laws. In this sense he unified celestial and terrestrial dynamics. Using Newton's law of universal gravitation,
proving Kepler's Laws for the case of a circular orbit is simple.
Elliptical orbits involve more complex calculations, which Newton
included in his Principia.
Joseph-Louis Lagrange
After Newton, Lagrange (25 January 1736–10 April 1813) attempted to solve the three-body problem, analyzed the stability of planetary orbits, and discovered the existence of the Lagrangian points. Lagrange also reformulated the principles of classical mechanics, emphasizing energy more than force and developing a method
to use a single polar coordinate equation to describe any orbit, even
those that are parabolic and hyperbolic. This is useful for calculating
the behaviour of planets and comets and such. More recently, it has also become useful to calculate spacecrafttrajectories.
Simon Newcomb
Simon Newcomb (12 March 1835–11 July 1909) was a Canadian-American astronomer who revised Peter Andreas Hansen's table of lunar positions. In 1877, assisted by George William Hill,
he recalculated all the major astronomical constants. After 1884, he
conceived with A. M. W. Downing a plan to resolve much international
confusion on the subject. By the time he attended a standardisation
conference in Paris,
France in May 1886, the international consensus was that all
ephemerides should be based on Newcomb's calculations. A further
conference as late as 1950 confirmed Newcomb's constants as the
international standard.
Albert Einstein
Albert Einstein (14 March 1879–18 April 1955) explained the anomalous precession of Mercury's perihelion in his 1916 paper The Foundation of the General Theory of Relativity. This led astronomers to recognize that Newtonian mechanics did not provide the highest accuracy. Binary pulsars have been observed, the first in 1974, whose orbits not only require the use of General Relativity for their explanation, but whose evolution proves the existence of gravitational radiation, a discovery that led to the 1993 Nobel Physics Prize.
Examples of problems
Celestial motion without additional forces such as thrust of a rocket, is governed by gravitational acceleration of masses due to other masses. A simplification is the n-body problem, where the problem assumes some number n
of spherically symmetric masses. In that case, the integration of the
accelerations can be well approximated by relatively simple summations.
Examples:
4-body problem: spaceflight to Mars (for parts of the flight the
influence of one or two bodies is very small, so that there we have a
2- or 3-body problem; see also the patched conic approximation)
In the case that n=2 (two-body problem), the situation is much simpler than for larger n.
Various explicit formulas apply, where in the more general case
typically only numerical solutions are possible. It is a useful
simplification that is often approximately valid.
A further simplification is based on the "standard assumptions in astrodynamics", which include that one body, the orbiting body, is much smaller than the other, the central body. This is also often approximately valid.
A spacecraft orbiting Earth, a moon, or a planet (in the latter
cases the approximation only applies after arrival at that orbit)
Perturbation theory
Perturbation theory
comprises mathematical methods that are used to find an approximate
solution to a problem which cannot be solved exactly. (It is closely
related to methods used in numerical analysis, which are ancient.) The earliest use of modern perturbation theory was to deal with the otherwise unsolveable mathematical problems of celestial mechanics: Newton's solution for the orbit of the Moon, which moves noticeably differently from a simple Keplerian ellipse because of the competing gravitation of the Earth and the Sun.
Perturbation methods
start with a simplified form of the original problem, which is
carefully chosen to be exactly solvable. In celestial mechanics, this is
usually a Keplerian ellipse, which is correct when there are only two gravitating bodies (say, the Earth and the Moon), or a circular orbit, which is only correct in special cases of two-body motion, but is often close enough for practical use.
The solved, but simplified problem is then "perturbed" to make its time-rate-of-change equations for the object's position closer to the values from the real problem, such as including the gravitational attraction of a third, more distant body (the Sun).
The slight changes that result from the terms in the equations – which
themselves may have been simplified yet again – are used as corrections
to the original solution. Because simplifications are made at every
step, the corrections are never perfect, but even one cycle of
corrections often provides a remarkably better approximate solution to
the real problem.
There is no requirement to stop at only one cycle of corrections.
A partially corrected solution can be re-used as the new starting point
for yet another cycle of perturbations and corrections. In principle,
for most problems the recycling and refining of prior solutions to
obtain a new generation of better solutions could continue indefinitely,
to any desired finite degree of accuracy.
The common difficulty with the method is that the corrections
usually progressively make the new solutions very much more complicated,
so each cycle is much more difficult to manage than the previous cycle
of corrections. Newton is reported to have said, regarding the problem of the Moon's orbit "It causeth my head to ache."
This general procedure – starting with a simplified problem and
gradually adding corrections that make the starting point of the
corrected problem closer to the real situation – is a widely used
mathematical tool in advanced sciences and engineering. It is the
natural extension of the "guess, check, and fix" method used anciently with numbers.
In celestial mechanics, an orbital resonance occurs when orbiting bodies exert a regular, periodic gravitational influence on each other, usually because their orbital periods are related by a ratio of small integers.
Most commonly this relationship is found for a pair of objects. The
physics principle behind orbital resonance is similar in concept to
pushing a child on a swing, where the orbit and the swing both have a natural frequency,
and the other body doing the "pushing" will act in periodic repetition
to have a cumulative effect on the motion. Orbital resonances greatly
enhance the mutual gravitational influence of the bodies, i.e. their
ability to alter or constrain each other's orbits. In most cases, this
results in an unstable interaction, in which the bodies exchange momentum
and shift orbits until the resonance no longer exists. Under some
circumstances, a resonant system can be stable and self-correcting, so
that the bodies remain in resonance. Examples are the 1:2:4 resonance of
Jupiter's moons Ganymede, Europa and Io, and the 2:3 resonance between Pluto and Neptune. Unstable resonances with Saturn's inner moons give rise to gaps in the rings of Saturn. The special case of 1:1 resonance between bodies with similar orbital radii causes large Solar System bodies to eject most other bodies sharing their orbits; this is part of the much more extensive process of clearing the neighbourhood, an effect that is used in the current definition of a planet.
A binary resonance ratio in this article should be interpreted as the ratio of number of orbits completed in the same time interval, rather than as the ratio of orbital periods,
which would be the inverse ratio. Thus the 2:3 ratio above means Pluto
completes two orbits in the time it takes Neptune to complete three. In
the case of resonance relationships among three or more bodies, either
type of ratio may be used (in such cases the smallest whole-integer
ratio sequences are not necessarily reversals of each other) and the
type of ratio will be specified.
History
Since the discovery of Newton's law of universal gravitation in the 17th century, the stability of the Solar System has preoccupied many mathematicians, starting with Laplace. The stable orbits that arise in a two-body approximation ignore the influence of other bodies. The effect of these added interactions on the stability of the Solar System
is very small, but at first it was not known whether they might add up
over longer periods to significantly change the orbital parameters and
lead to a completely different configuration, or whether some other
stabilising effects might maintain the configuration of the orbits of
the planets.
It was Laplace who found the first answers explaining the linked orbits of the Galilean moons
(see below). Before Newton, there was also consideration of ratios and
proportions in orbital motions, in what was called "the music of the
spheres", or Musica universalis.
A chart of the distribution of asteroid semimajor axes, showing the Kirkwood gaps where orbits are destabilized by resonances with Jupiter
Spiral density waves in Saturn's A Ring excited by resonances with inner moons.
Such waves propagate away from the planet (towards upper left). The
large set of waves just below center is due to the 6:5 resonance with Janus.
The eccentric Titan Ringlet in the Columbo Gap of Saturn's C Ring (center) and the inclined orbits of resonant particles in the bending wave just inside it have apsidal and nodal precessions, respectively, commensurate with Titan's mean motion.
In general, an orbital resonance may
involve one or any combination of the orbit parameters (e.g. eccentricity versus semimajor axis, or eccentricity versus orbital inclination).
act on any time scale from short term, commensurable with the orbit periods, to secular, measured in 104 to 106 years.
lead to either long-term stabilization of the orbits or be the cause of their destabilization.
A mean-motion orbital resonance occurs when two bodies have periods of revolution that are a simple integer ratio of each other. Depending on the details, this can either stabilize or destabilize the orbit.
Stabilization may occur when the two bodies move in such a synchronised fashion that they never closely approach. For instance:
The orbits of Pluto and the plutinos are stable, despite crossing that of the much larger Neptune,
because they are in a 2:3 resonance with it. The resonance ensures
that, when they approach perihelion and Neptune's orbit, Neptune is
consistently distant (averaging a quarter of its orbit away). Other
(much more numerous) Neptune-crossing bodies that were not in resonance
were ejected from that region by strong perturbations due to Neptune. There are also smaller but significant groups of resonant trans-Neptunian objects occupying the 1:1 (Neptune trojans), 3:5, 4:7, 1:2 (twotinos) and 2:5 resonances, among others, with respect to Neptune.
Orbital resonances can also destabilize one of the orbits. For small bodies, destabilization is actually far more likely. For instance:
In the asteroid belt within 3.5 AU from the Sun, the major mean-motion resonances with Jupiter are locations of gaps in the asteroid distribution, the Kirkwood gaps (most notably at the 4:1, 3:1, 5:2, 7:3 and 2:1 resonances). Asteroids
have been ejected from these almost empty lanes by repeated
perturbations. However, there are still populations of asteroids
temporarily present in or near these resonances. For example, asteroids
of the Alinda family
are in or close to the 3:1 resonance, with their orbital eccentricity
steadily increased by interactions with Jupiter until they eventually
have a close encounter with an inner planet that ejects them from the
resonance.
In the rings of Saturn, the Cassini Division is a gap between the inner B Ring and the outer A Ring that has been cleared by a 2:1 resonance with the moon Mimas. (More specifically, the site of the resonance is the Huygens Gap, which bounds the outer edge of the B Ring.)
In the rings of Saturn, the Encke and Keeler gaps within the A Ring are cleared by 1:1 resonances with the embedded moonlets Pan and Daphnis, respectively. The A Ring's outer edge is maintained by a destabilizing 7:6 resonance with the moon Janus.
Most bodies that are in resonance orbit in the same direction; however, the retrograde asteroid 2015 BZ509 appears to be in a stable (for a period of at least a million years) 1:−1 resonance with Jupiter. In addition, a few retrograde damocloids have been found that are temporarily captured in mean-motion resonance with Jupiter or Saturn. Such orbital interactions are weaker than the corresponding interactions between bodies orbiting in the same direction.
A Laplace resonance is a three-body resonance with a 1:2:4 orbital period ratio (equivalent to a 4:2:1 ratio of orbits). The term arose because Pierre-Simon Laplace discovered that such a resonance governed the motions of Jupiter's moons Io, Europa, and Ganymede. It is now also often applied to other 3-body resonances with the same ratios, such as that between the extrasolar planetsGliese 876 c, b, and e. Three-body resonances involving other simple integer ratios have been termed "Laplace-like"[9] or "Laplace-type".
A secular resonance occurs when the precession of two orbits is synchronised (usually a precession of the perihelion or ascending node). A small body in secular resonance with a much larger one (e.g. a planet) will precess at the same rate as the large body. Over long times (a million years, or so) a secular resonance will change the eccentricity and inclination of the small body.
Several prominent examples of secular resonance involve Saturn. A
resonance between the precession of Saturn's rotational axis and that
of Neptune's orbital axis (both of which have periods of about 1.87
million years) has been identified as the likely source of Saturn's
large axial tilt (26.7°). Initially, Saturn probably had a tilt closer to that of Jupiter (3.1°).
The gradual depletion of the Kuiper belt would have decreased the
precession rate of Neptune's orbit; eventually, the frequencies matched,
and Saturn's axial precession was captured into the spin-orbit
resonance, leading to an increase in Saturn's obliquity. (The angular
momentum of Neptune's orbit is 104 times that of Saturn's spin, and thus dominates the interaction.)
The perihelion secular resonance between asteroids and Saturn (ν6 = g − g6)
helps shape the asteroid belt (the subscript "6" identifies Saturn as
the sixth planet from the Sun). Asteroids which approach it have their
eccentricity slowly increased until they become Mars-crossers, at which point they are usually ejected from the asteroid belt by a close pass to Mars. This resonance forms the inner and "side" boundaries of the asteroid belt around 2 AU, and at inclinations of about 20°.
Numerical simulations have suggested that the eventual formation of a perihelion secular resonance between Mercury and Jupiter (g1 = g5)
has the potential to greatly increase Mercury's eccentricity and
possibly destabilize the inner Solar System several billion years from
now.
The Titan Ringlet within Saturn's C Ring represents another type of resonance in which the rate of apsidal precession
of one orbit exactly matches the speed of revolution of another. The
outer end of this eccentric ringlet always points towards Saturn's major
moon Titan.
A Kozai resonance occurs when the inclination and eccentricity of a perturbed
orbit oscillate synchronously (increasing eccentricity while decreasing
inclination and vice versa). This resonance applies only to bodies on
highly inclined orbits; as a consequence, such orbits tend to be
unstable, since the growing eccentricity would result in small pericenters, typically leading to a collision or (for large moons) destruction by tidal forces.
In an example of another type of resonance involving orbital
eccentricity, the eccentricities of Ganymede and Callisto vary with a
common period of 181 years, although with opposite phases.
Mean-motion resonances in the Solar System
Depiction of Haumea's presumed 7:12 resonance with Neptune in a rotating frame,
with Neptune (blue dot at lower right) held stationary. Haumea's
shifting orbital alignment relative to Neptune periodically reverses (librates), preserving the resonance.
The Laplace resonance exhibited by three of the Galilean moons. The ratios in the figure are of orbital periods.
Conjunctions are highlighted by brief color changes. There are two
Io-Europa conjunctions (green) and three Io-Ganymede conjunctions (grey)
for each Europa-Ganymede conjunction (magenta).
Additionally, Haumea is believed to be in a 7:12 resonance with Neptune, and (225088) 2007 OR10 is believed to be in a 3:10 resonance with Neptune.
The simple integer ratios between periods hide more complex relations:
the point of conjunction can oscillate (librate) around an equilibrium point defined by the resonance.
given non-zero eccentricities, the nodes or periapsides can drift (a resonance related, short period, not secular precession).
As illustration of the latter, consider the well-known 2:1 resonance
of Io-Europa. If the orbiting periods were in this relation, the mean motions (inverse of periods, often expressed in degrees per day) would satisfy the following
Substituting the data (from Wikipedia) one will get −0.7395° day−1, a value substantially different from zero.
Actually, the resonance is perfect, but it involves also the precession of perijove (the point closest to Jupiter), . The correct equation (part of the Laplace equations) is:
In other words, the mean motion of Io is indeed double of that of
Europa taking into account the precession of the perijove. An observer
sitting on the (drifting) perijove will see the moons coming into
conjunction in the same place (elongation). The other pairs listed above
satisfy the same type of equation with the exception of Mimas-Tethys
resonance. In this case, the resonance satisfies the equation
The point of conjunctions librates around the midpoint between the nodes of the two moons.
Laplace resonance
Illustration of Io–Europa–Ganymede resonance. From the centre outwards: Io (yellow), Europa (gray) and Ganymede (dark)
The Laplace resonance involving Io–Europa–Ganymede includes the following relation locking the orbital phase of the moons:
where are mean longitudes of the moons (the second equals sign ignores libration).
This relation makes a triple conjunction impossible. (A Laplace resonance in the Gliese 876
system, in contrast, is associated with one triple conjunction per
orbit of the outermost planet, ignoring libration.) The graph
illustrates the positions of the moons after 1, 2 and 3 Io periods. librates about 180° with an amplitude of 0.03°.
Another "Laplace-like" resonance involves the moonsStyx, Nix and Hydra of Pluto:
This reflects orbital periods for Styx, Nix and Hydra, respectively,
that are close to a ratio of 18:22:33 (or, in terms of the near
resonances with Charon's period, 3+3/11:4:6; see below); the respective ratio of orbits is 11:9:6. Based on the ratios of synodic periods, there are 5 conjunctions of Styx and Hydra and 3 conjunctions of Nix and Hydra for every 2 conjunctions of Styx and Nix. As with the Galilean satellite resonance, triple conjunctions are forbidden. librates about 180° with an amplitude of at least 10°.
Sequence
of conjunctions of Hydra (blue),
Nix (red) and Styx (black) over one
third of their
resonance cycle. Movements are counterclockwise
and
orbits completed are tallied at upper right of
diagrams (click on image
to see the whole cycle).
Plutino resonances
The dwarf planet Pluto is following an orbit trapped in a web of resonances with Neptune. The resonances include:
The resonance of the longitude of the perihelion in relation to that of Neptune
One consequence of these resonances is that a separation of at least
30 AU is maintained when Pluto crosses Neptune's orbit. The minimum
separation between the two bodies overall is 17 AU, while the minimum
separation between Pluto and Uranus is just 11 AU.
The next largest body in a similar 2:3 resonance with Neptune, called a plutino, is the probable dwarf planet Orcus.
Orcus has an orbit similar in inclination and eccentricity to Pluto's.
However, the two are constrained by their mutual resonance with Neptune
to always be in opposite phases of their orbits; Orcus is thus sometimes
described as the "anti-Pluto".
Mean-motion resonances among extrasolar planets
While most extrasolar planetary systems discovered have not been found to have planets in mean-motion resonances, chains of up to five resonant planets and up to seven at least near resonant planets have been uncovered. Simulations have shown that during planetary system formation, the appearance of resonant chains of planetary embryos is favored by the presence of the primordial gas disc.
Once that gas dissipates, 90-95% of those chains must then become
unstable to match the low frequency of resonant chains observed.
As mentioned above, Gliese 876 e, b and c are in a Laplace resonance, with a 4:2:1 ratio of periods (124.3, 61.1 and 30.0 days). In this case, librates with an amplitude of 40° ± 13° and the resonance follows the time-averaged relation:
Kepler-223
has four planets in a resonance with an 8:6:4:3 orbit ratio, and a
3:4:6:8 ratio of periods (7.3845, 9.8456, 14.7887 and 19.7257 days). This represents the first confirmed 4-body orbital resonance.
The librations within this system are such that close encounters
between two planets occur only when the other planets are in distant
parts of their orbits. Simulations indicate that this system of
resonances must have formed via planetary migration.
Kepler-80
d, e, b, c and g have periods in a ~ 1.000: 1.512: 2.296: 3.100: 4.767
ratio (3.0722, 4.6449, 7.0525, 9.5236 and 14.6456 days). However, in a
frame of reference that rotates with the conjunctions, this reduces to a
period ratio of 4:6:9:12:18 (an orbit ratio of 9:6:4:3:2). Conjunctions
of d and e, e and b, b and c, and c and g occur at relative intervals
of 2:3:6:6 (9.07, 13.61 and 27.21 days) in a pattern that repeats about
every 190.5 days (seven full cycles in the rotating frame) in the
inertial or nonrotating frame (equivalent to a 62:41:27:20:13 orbit
ratio resonance in the nonrotating frame, because the conjunctions
circulate in the direction opposite orbital motion). Librations of
possible three-body resonances have amplitudes of only about 3 degrees,
and modeling indicates the resonant system is stable to perturbations.
Triple conjunctions do not occur.
Kepler-29 has a pair of planets in a 7:9 resonance (ratio of 1/1.28587).
Kepler-36 has a pair of planets close to a 6:7 resonance.
Kepler-37
d, c and b are within one percent of a resonance with an 8:15:24 orbit
ratio and a 15:8:5 ratio of periods (39.792187, 21.301886 and 13.367308
days).
Of Kepler-90's
eight known planets, the period ratios b:c, c:i and i:d are close to
4:5, 3:5 and 1:4, respectively (4:4.977, 3:4.97 and 1:4.13) and d, e, f,
g and h are close to a 2:3:4:7:11 period ratio
(2:3.078:4.182:7.051:11.102; also 7:11.021). f, g and h are also close to a 3:5:8 period ratio (3:5.058:7.964). Relevant to systems like this and that of Kepler-36,
calculations suggest that the presence of an outer gas giant planet
facilitates the formation of closely packed resonances among inner
super-Earths.
TRAPPIST-1's
seven approximately Earth-sized planets are in a chain of near
resonances (the longest such chain known), having an orbit ratio of
approximately 24, 15, 9, 6, 4, 3 and 2, or nearest-neighbor period
ratios (proceeding outward) of about 8/5, 5/3, 3/2, 3/2, 4/3 and 3/2
(1.603, 1.672, 1.506, 1.509, 1.342 and 1.519). They are also configured
such that each triple of adjacent planets is in a Laplace resonance
(i.e., b, c and d in one such Laplace configuration; c, d and e in
another, etc.).
The resonant configuration is expected to be stable on a time scale of
billions of years, assuming it arose during planetary migration. A musical interpretation of the resonance has been provided.
Cases of extrasolar planets close to a 1:2 mean-motion resonance are fairly common. Sixteen percent of systems found by the transit method are reported to have an example of this (with period ratios in the range 1.83-2.18), as well as one sixth of planetary systems characterized by Doppler spectroscopy (with in this case a narrower period ratio range). Due to incomplete knowledge of the systems, the actual proportions are likely to be higher. Overall, about a third of radial velocity characterized systems appear to have a pair of planets close to a commensurability.
It is much more common for pairs of planets to have orbital period
ratios a few percent larger than a mean-motion resonance ratio than a
few percent smaller (particularly in the case of first order resonances,
in which the integers in the ratio differ by one). This was predicted to be true in cases where tidal interactions with the star are significant.
Coincidental 'near' ratios of mean motion
Depiction of asteroid Pallas' 18:7 near resonance with Jupiter in a rotating frame (click for animation).
Jupiter (pink loop at upper left) is held nearly stationary. The shift
in Pallas' orbital alignment relative to Jupiter increases steadily over
time; it never reverses course (i.e., there is no libration).
Depiction of the Earth:Venus 8:13 near resonance. With Earth held stationary at the center of a nonrotating frame, the successive inferior conjunctions of Venus over eight Earth years trace a pentagrammic pattern (reflecting the difference between the numbers in the ratio).
Diagram of the orbits of Pluto's
small outer four moons, which follow a 3:4:5:6 sequence of near
resonances relative to the period of its large inner satellite Charon. The moons Styx, Nix and Hydra are also involved in a true 3-body resonance.
A number of near-integer-ratio
relationships between the orbital frequencies of the planets or major
moons are sometimes pointed out (see list below). However, these have no
dynamical significance because there is no appropriate precession of perihelion or other libration to make the resonance perfect (see the detailed discussion in the section above).
Such near resonances are dynamically insignificant even if the mismatch
is quite small because (unlike a true resonance), after each cycle the
relative position of the bodies shifts. When averaged over
astronomically short timescales, their relative position is random, just
like bodies that are nowhere near resonance. For example, consider the
orbits of Earth and Venus, which arrive at almost the same configuration
after 8 Earth orbits and 13 Venus orbits. The actual ratio is
0.61518624, which is only 0.032% away from exactly 8:13. The mismatch
after 8 years is only 1.5° of Venus' orbital movement. Still, this is
enough that Venus and Earth find themselves in the opposite relative
orientation to the original every 120 such cycles, which is 960 years.
Therefore, on timescales of thousands of years or more (still tiny by
astronomical standards), their relative position is effectively random.
The presence of a near resonance may reflect that a perfect
resonance existed in the past, or that the system is evolving towards
one in the future.
Mismatch
in orbital longitude of the inner body, as compared to its position at
the beginning of the cycle. Circular orbits are assumed (i.e., precession is ignored).
The
time needed for the mismatch from the initial relative longitudinal
orbital positions of the bodies to grow to 180°, rounded to the nearest
first significant digit.
The probability of obtaining an orbital coincidence of equal or smaller mismatch by chance at least once in n attempts, where n
is the integer number of orbits of the outer body per cycle, and the
mismatch is assumed to vary between 0° and 180° at random. The value is
calculated as 1- (1- mismatch/180°)^n. This is a crude calculation that only attempts to give a rough idea of relative probabilities.
The two near commensurabilities listed for Earth and Venus are reflected in the timing of transits of Venus, which occur in pairs 8 years apart, in a cycle that repeats every 243 years.
The near 1:12 resonance between Jupiter and Earth causes the Alinda asteroids, which occupy (or are close to) the 3:1 resonance with Jupiter, to be close to a 1:4 resonance with Earth.
This near resonance has been termed the Great Inequality. It was first described by Laplace in a series of papers published 1784–1789.
Resonances with a now-vanished inner moon are likely to have been involved in the formation of Phobos and Deimos.
Based on the proper orbital periods, 1684.869 and 1681.601 days, for Pallas and Ceres, respectively.
Based on the proper orbital period of Pallas, 1684.869 days, and 4332.59 days for Jupiter.
87 Sylvia is the first asteroid discovered to have more than one moon.
This resonance may have been occupied in the past.
This resonance may have been occupied in the past.
This resonance may have been occupied in the past.
The
results for the Haumea system aren't very meaningful because, contrary
to the assumptions implicit in the calculations, Namaka has an
eccentric, non-Keplerian orbit that precesses rapidly (see below). Hiʻiaka and Namaka are much closer to a 3:8 resonance than indicated, and may actually be in it.
The least probable orbital correlation in the list is that between Io
and Metis, followed by those between Rosalind and Cordelia, Pallas and
Ceres, Jupiter and Pallas, Callisto and Ganymede, and Hydra and Charon,
respectively.
Possible past mean-motion resonances
A past resonance between Jupiter and Saturn may have played a dramatic role in early Solar System history. A 2004 computer model by Alessandro Morbidelli of the Observatoire de la CƓte d'Azur in Nice suggested that the formation of a 1:2 resonance between Jupiter and Saturn (due to interactions with planetesimals
that caused them to migrate inward and outward, respectively) created a
gravitational push that propelled both Uranus and Neptune into higher
orbits, and in some scenarios caused them to switch places, which would
have doubled Neptune's distance from the Sun. The resultant expulsion of
objects from the proto-Kuiper belt as Neptune moved outwards could
explain the Late Heavy Bombardment 600 million years after the Solar System's formation and the origin of Jupiter's Trojan asteroids.
An outward migration of Neptune could also explain the current
occupancy of some of its resonances (particularly the 2:5 resonance)
within the Kuiper belt.
While Saturn's mid-sized moons Dione and Tethys are not close to
an exact resonance now, they may have been in a 2:3 resonance early in
the Solar System's history. This would have led to orbital eccentricity
and tidal heating
that may have warmed Tethys' interior enough to form a subsurface
ocean. Subsequent freezing of the ocean after the moons escaped from the
resonance may have generated the extensional stresses that created the
enormous graben system of Ithaca Chasma on Tethys.
The satellite system of Uranus is notably different from those of
Jupiter and Saturn in that it lacks precise resonances among the larger
moons, while the majority of the larger moons of Jupiter (3 of the 4
largest) and of Saturn (6 of the 8 largest) are in mean-motion
resonances. In all three satellite systems, moons were likely captured
into mean-motion resonances in the past as their orbits shifted due to tidal dissipation
(a process by which satellites gain orbital energy at the expense of
the primary's rotational energy, affecting inner moons
disproportionately). In the Uranian system, however, due to the planet's
lesser degree of oblateness,
and the larger relative size of its satellites, escape from a
mean-motion resonance is much easier. Lower oblateness of the primary
alters its gravitational field in such a way that different possible
resonances are spaced more closely together. A larger relative satellite
size increases the strength of their interactions. Both factors lead to
more chaotic orbital behavior at or near mean-motion resonances. Escape
from a resonance may be associated with capture into a secondary
resonance, and/or tidal evolution-driven increases in orbital eccentricity or inclination.
Mean-motion resonances that probably once existed in the Uranus
System include (3:5) Ariel-Miranda, (1:3) Umbriel-Miranda, (3:5)
Umbriel-Ariel, and (1:4) Titania-Ariel.Evidence for such past resonances includes the relatively high
eccentricities of the orbits of Uranus' inner satellites, and the
anomalously high orbital inclination of Miranda. High past orbital
eccentricities associated with the (1:3) Umbriel-Miranda and (1:4)
Titania-Ariel resonances may have led to tidal heating of the interiors
of Miranda and Ariel,
respectively. Miranda probably escaped from its resonance with Umbriel
via a secondary resonance, and the mechanism of this escape is believed
to explain why its orbital inclination is more than 10 times those of
the other regular Uranian moons (see Uranus' natural satellites).
Similar to the case of Miranda, the present inclinations of Jupiter's moonlets Amalthea and Thebe are thought to be indications of past passage through the 3:1 and 4:2 resonances with Io, respectively.
Neptune's regular moons Proteus and Larissa are thought to have
passed through a 1:2 resonance a few hundred million years ago; the
moons have drifted away from each other since then because Proteus is
outside a synchronous orbit
and Larissa is within one. Passage through the resonance is thought to
have excited both moons' eccentricities to a degree that has not since
been entirely damped out.
In the case of Pluto's
satellites, it has been proposed that the present near resonances are
relics of a previous precise resonance that was disrupted by tidal
damping of the eccentricity of Charon's orbit (see Pluto's natural satellites
for details). The near resonances may be maintained by a 15% local
fluctuation in the Pluto-Charon gravitational field. Thus, these near
resonances may not be coincidental.
The smaller inner moon of the dwarf planetHaumea, Namaka, is one tenth the mass of the larger outer moon, HiŹ»iaka. Namaka revolves around Haumea in 18 days in an eccentric, non-Keplerian orbit, and as of 2008 is inclined 13° from HiŹ»iaka.
Over the timescale of the system, it should have been tidally damped
into a more circular orbit. It appears that it has been disturbed by
resonances with the more massive Hiʻiaka,
due to converging orbits as it moved outward from Haumea because of
tidal dissipation. The moons may have been caught in and then escaped
from orbital resonance several times. They probably passed through the
3:1 resonance relatively recently, and currently are in or at least
close to an 8:3 resonance. Namaka's orbit is strongly perturbed, with a current precession of about −6.5° per year.