Conference on Mathematical Methods in Celestial Mechanics, 5th, Oberwolfach, West Germany, August 24-30, 1975, Proceedings. Parts 1 & 2

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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, Runge-Kutta Method, Satellite Orbits, Three Body Problem, Time Functions, Trajectory Optimization, Transformations (Mathematics)

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Attention is given to periodic solutions in the planar N-body problem, to the use of the KS transformation in relation to the Lagrange equations of motion, to the numerical integration of near-parabolic orbits, and to trajectory optimization using a closed solution of constant thrust-acceleration. 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.

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