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Advanced algorithm for orbit computationComputational 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.
Document ID
19860004632
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Szenbehely, V.
(Texas Univ. Austin, TX, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1983
Publication Information
Publication: NASA. Johnson (Lyndon B.) Space Center The 1983 NASA/ASEE Summer Faculty Fellowship Research Program Research Reports
Subject Category
Numerical Analysis
Accession Number
86N14101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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