Study on the perturbation of lunar and planetary orbiters

Details Study on the perturbation of lunar and planetary orbiters Study on the perturbation of lunar and planetary orbiters

Nov 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983stin...8433429h&link_type=abstract

Final Report MATRA Service Aerodynamique, Toulouse (France). Dept. d'Etudes et Avant Projets Systeme.

Computer Science

Software Engineering

Orbit Perturbation, Prediction Analysis Techniques, Software Engineering, Space Shuttle Orbiters, Computer Programs, Orbit Calculation, Orbital Mechanics, Three Body Problem

Scientific paper

A first order analytical orbit prediction software based on the stroboscopic method with equinoctial elements was developed. Only conservative disturbing forces are considered: the nonsphericity of the central body and the third body attraction. The first order equations of motion are analytically integrated over one revolution with a MACSYMA computerized algebraic utility. The obtained FORTRAN expressions are the foundations of the first version of the software which may be applied to the prediction of the orbit of lunar and planetary orbiters.

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