Kozai mechanism

In celestial mechanics, the Kozai mechanism or Lidov–Kozai mechanism or Kozai–Lidov mechanism, also known as the Kozai, Lidov–Kozai or Kozai–Lidov effect, oscillations, cycles or resonance, is a dynamical phenomenon affecting the orbit of a binary system perturbed by a distant third body under certain conditions, causing the orbit's argument of pericenter to oscillate about a constant value, which in turn leads to a periodic exchange between its eccentricity and inclination. The process occurs on timescales much longer than the orbital periods. It can drive an initially near-circular orbit to arbitrarily high eccentricity, and "flip" an initially moderately inclined orbit between a prograde and a retrograde motion.
The effect has been found to be an important factor shaping the orbits of irregular satellites of the planets, trans-Neptunian objects, extrasolar planets, and multiple star systems. It hypothetically promotes black hole mergers. It was first described in 1961 by Mikhail Lidov while analyzing the orbits of artificial and natural satellites of planets. In 1962, Yoshihide Kozai published this same result in application to the orbits of asteroids perturbed by Jupiter. The citations of the initial papers by Kozai and Lidov have risen sharply in the 21st century. As of 2017, the mechanism is among the most studied astrophysical phenomena.
Background.
Hamiltonian mechanics.
In Hamiltonian mechanics, a physical system is specified by a function, called "Hamiltonian" and denoted formula_1, of canonical coordinates in phase space. The canonical coordinates consist of the generalized coordinates formula_2 in configuration space and their conjugate momenta formula_3, for formula_4, for the bodies in the system (formula_5 for the Kozai-Lidov effect). The number of formula_6 pairs required to describe a given system is the number of its degrees of freedom.
The coordinate pairs are usually chosen in such a way as to simplify the calculations involved in solving a particular problem. One set of canonical coordinates can be changed to another by a canonical transformation. The equations of motion for the system are obtained from the Hamiltonian through "Hamilton's canonical equations", which relate time derivatives of the coordinates to partial derivatives of the Hamiltonian with respect to the conjugate momenta.
The three-body problem.
The dynamics of a system composed of three bodies system acting under their mutual gravitational attraction is complex. In general, the behaviour of a three-body system over long periods of time is enormously sensitive to any slight changes in the initial conditions, including even small uncertainties in determining the initial conditions, and rounding-errors in computer floating point arithmetic. The practical consequence is that, the three-body problem cannot be solved analytically for an indefinite amount of time, except in special cases. Instead, numerical methods are used for forecast-times limited by the available precision.
The Lidov-Kozai mechanism is a feature of "hierarchical" triple systems, that is systems in which one of the bodies, called the "perturber", is located far from the other two, which are said to comprise the inner binary. The perturber and the centre of mass of the inner binary comprise the outer binary. Such systems are often studied by using the methods of perturbation theory to write the Hamiltonian of a hierarchical three-body system as a sum of two terms responsible for the isolated evolution of the inner and the outer binary, and a third term coupling the two orbits,
The coupling term is then expanded in the orders of parameter formula_8, defined as the ratio of the semi-major axes of the inner and the outer binary and hence small in a hierarchical system. Since the perturbative series converges rapidly, the qualitative behaviour of a hierarchical three-body system is determined by the initial terms in the expansion, referred to as the "quadrupole"
(formula_9), "octupole" (formula_10) and "hexadecapole" (formula_11) order terms,
For many systems, a satisfactory description is found already at the lowest, quadrupole order in the perturbative expansion. The octupole term becomes dominant in certain regimes and is responsible for a long-term variation in the amplitude of the Lidov-Kozai oscillations.
Secular approximation.
The Lidov-Kozai mechanism is a "secular" effect, that is, it occurs on timescales much longer compared to the orbital periods of the inner and the outer binary. In order to simplify the problem and make it more tractable computationally, the hierarchical three-body Hamiltonian can be "secularised", that is, averaged over the rapidly varying mean anomalies of the two orbits. Through this process, the problem is reduced to that of two interacting massive wire loops.
Overview of the mechanism.
Test particle limit.
The simplest treatment of the Lidov-Kozai mechanism assumes that one of the inner binary's components, the "secondary", is a test particle – an idealized point-like object with negligible mass compared to the other two bodies, the "primary" and the distant perturber. These assumptions are valid, for instance, in the case of an artificial satellite in a low-Earth orbit that is perturbed by the Moon, or a short-period comet that is perturbed by Jupiter.
Under these approximations, the orbit-averaged equations of motion for the secondary have a conserved quantity: the component of the secondary's orbital angular momentum parallel to the angular momentum of the primary / perturber angular momentum. This conserved quantity can be expressed in terms of the secondary's eccentricity and inclination relative to the plane of the outer binary:
Conservation of means that orbital eccentricity can be "traded for" inclination. Thus, near-circular, highly inclined orbits can become very eccentric. Since increasing eccentricity while keeping the semimajor axis constant reduces the distance between the objects at periapsis, this mechanism can cause comets (perturbed by Jupiter) to become sungrazing.
Lidov-Kozai oscillations will be present if is lower than a certain value. At the critical value of , a "fixed-point" orbit appears, with constant inclination given by
For values of less than this critical value, there is a one-parameter family of orbital solutions having the same but different amounts of variation in or . Remarkably, the degree of possible variation in is independent of the masses involved, which only set the timescale of the oscillations.
Timescale.
The basic timescale associated with Kozai oscillations is
where indicates the semimajor axis, is orbital period, is eccentricity and is mass; variables with subscript "2" refer to the outer (perturber) orbit and variables lacking subscripts refer to the inner orbit; is the mass of the primary. For example, with Moon's period of 27.3 days, eccentricity 0.055 and the Global Positioning System satellites period of half a (sidereal) day, the Kozai timescale is a little over 4 years; for geostationary orbits it is twice shorter.
The period of oscillation of all three variables (, , – the last being the argument of periapsis) is the same, but depends on how "far" the orbit is from the fixed-point orbit, becoming very long for the separatrix orbit that separates librating orbits from oscillating orbits.
Astrophysical implications.
Solar System.
The Lidov-Kozai mechanism causes the argument of pericenter () to librate about either 90° or 270°, which is to say that its periapse occurs when the body is farthest from the equatorial plane. This effect is part of the reason that Pluto is dynamically protected from close encounters with Neptune.
The Lidov-Kozai mechanism places restrictions on the orbits possible within a system, for example:
The mechanism has been invoked in searches for Planet Nine, a hypothetical planet orbiting the Sun far beyond the orbit of Neptune.
A number of moons have been found to be in the Lidov-Kozai resonance with their planet, including Jupiter's Carpo and Euporie, Saturn's Kiviuq and Ijiraq, Uranus's Margaret, and Neptune's Sao and Neso.
Some sources identify the Soviet space probe Luna 3 as the first example of an artificial satellite undergoing Lidov-Kozai oscillations. Launched in 1959 into a highly inclined, eccentric, geocentric orbit, it was the first mission to photograph the far side of the Moon. It burned in the Earth's atmosphere after completing eleven revolutions. However, according to Gkolias "et al.". (2016) a different mechanism must have driven the decay of the probe's orbit since the Lidov-Kozai oscillations would have been thwarted by effects of the Earth's oblateness.
Extrasolar planets.
The Lidov-Kozai mechanism, in combination with tidal friction, is able to produce Hot Jupiters, which are gas giant exoplanets orbiting their stars on tight orbits.
Black holes.
The mechanism is thought to affect the growth of central black holes in dense star clusters. It also drives the evolution of certain classes of binary black holes and may play a role in enabling black hole mergers.
History and development.
The effect was first described in 1961 by the Soviet space scientist Mikhail Lidov while analyzing the orbits of artificial and natural satellites of planets. Originally published in Russian, the result was translated into English in 1962.
Lidov first presented his work on artificial satellite orbits at the "Conference on General and Applied Problems of Theoretical Astronomy" held in Moscow on 20–25 November 1961. His paper was first published in a Russian-language journal in 1961. The Japanese astronomer Yoshihide Kozai was among the 1961 conference participants. Kozai published the same result in a widely read English-language journal in 1962, using the result to analyze orbits of asteroids perturbed by Jupiter. Since Lidov was the first to publish, many authors use the term Lidov–Kozai mechanism. Others, however, name it as the Kozai–Lidov or just the Kozai mechanism.