Systematic computation algorithm to obtain osculating orbit elements from position and velocity vectors

Details Systematic computation algorithm to obtain osculating orbit elements from position and velocity vectors Systematic computation algorithm to obtain osculating orbit elements from position and velocity vectors

Sep 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989stin...9217854s&link_type=abstract

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Computation

Algorithms, Orbit Calculation, Orbital Elements, Orbital Mechanics, Orbital Position Estimation, Orbital Velocity, Position (Location), Celestial Mechanics, Orbit Perturbation, Perturbation Theory, Planetary Orbits, Spacecraft Orbits, Two Body Problem

Scientific paper

This report describes calculation algorithm and its systematic procedure of osculating orbital elements computation in each case of ecliptic, parabolic, hyperbolic and rectilinear orbit. The osculating orbital elements are those elements applied only in specific timing when position vector and velocity vector of a spacecraft or celestial body, such as comet, are input in the calculation.

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