The so-called multi-revolution methods were introduced in celestial
mechanics as an efficient tool for the long-term numerical
integration
of orbits of artificial satellites. Multi-revolution methods attempt
to track the solution after a large number
of periods by using
the
one period map
at only a few suitable points. In this
talk
we will provide a theoretical background of such methods used in some
problems of celestial mechanics and in highly oscillatory problems of
other fields. For those problems it is assumed in advance that the
solutions of the differential equations for the initial conditions
under consideration are quasi periodic. We will give a general
presentation
and analysis of multi-revolution Runge-Kutta (MRRK) methods similar
to the
one
developed by John Butcher for standard RK methods applied to ordinary
differential equations. An
-stage multi-revolution Runge-Kutta
method
is
an algorithm that approximates the map
of N
quasi-periods
in terms of the one quasi-period Poincaré map
evaluated
at
suitable selected points. We assume that that the one
quasi-period map is a near identity map in some neighborhood of an
initial value and that the quasi-period T is known in advance.
Some order conditions, simplifying assumptions,
and order estimates will be presented. The construction of high order
MRIRK methods will be described based on some families of orthogonal
polynomials. Some references are given by
[1,2,3,4,5].