Newton's laws of motion and his universal law of gravitation
described mathematically the motion of two bodies undergoing mutual
gravitational attraction. However, it is impossible to solve
analytically the equation of motion for three gravitationally
interacting bodies. This book discusses some techniques used to
obtain numerical solutions of the equations of motion for planets
and satellites, which are of fundamental importance to solar-system
dynamicists and to those involved in planning the orbits of
artificial satellites.
The first part introduces the classical two-body problem and
solves it by rigorously developing the six integrals of the motion,
starting from Newton's three laws of motion and his law of
gravitation and then using vector algebra to develop the integrals.
The various forms of the solution flow naturally from the
integrals. In the second part, several modern perturbation
techniques are developed and applied to cases of practical
importance. For example, the perturbed two-body problem for an
oblate planet or for a nonsymmetric rotating planet is considered,
as is the effect of drag on a satellite. The two-body problem is
regularized, and the nonlinear differential equation is thereby
transformed to a linear one by further embedding several of the
integrals. Finally, a brief sketch of numerical methods is given,
as the perturbation equations must be solved by numerical rather
than by analytical methods.
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