Proceedings of the Fifth Conference on Mathematical Methods in Celestial Mechanics  Part I, II. Conference held at Oberwolfach, F.R. Germany, August 24  30, 1975.
Abstract
Attention is given to periodic solutions in the planar Nbody problem, to the use of the KS transformation in relation to the Lagrange equations of motion, to the numerical integration of nearparabolic orbits, and to trajectory optimization using a closed solution of constant thrustacceleration. Also considered are the decay of a highly eccentric satellite, an optimal Runge Kutta algorithm, and redundant variables for the global regularization of the three body problem. Individual items are announced in this issue.
 Publication:

Celestial Mechanics
 Pub Date:
 November 1976
 Bibcode:
 1976CeMec..14......
 Keywords:

 Applications Of Mathematics;
 Astrodynamics;
 Celestial Mechanics;
 Conferences;
 Boundary Value Problems;
 Calculus Of Variations;
 Conformal Mapping;
 Difference Equations;
 Linear Equations;
 Many Body Problem;
 Numerical Integration;
 Orbital Mechanics;
 RungeKutta Method;
 Satellite Orbits;
 Three Body Problem;
 Time Functions;
 Trajectory Optimization;
 Transformations (Mathematics);
 Astronomy