NASA NTRS · 19860004632
Advanced algorithm for orbit computation
Abstract
Computational and analytical techniques which simplify the solution of complex problems in orbit mechanics, Astrodynamics and Celestial Mechanics were developed. The major tool of the simplification is the substitution of transformations in place of numerical or analytical integrations. In this way the rather complicated equations of orbit mechanics might sometimes be reduced to linear equations representing harmonic oscillators with constant coefficients.
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Szenbehely, V.. 1983-09-01. Advanced algorithm for orbit computation. https://ntrs.nasa.gov/citations/19860004632
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